diff --git a/Turbofan/.Turbofan.mdl.py.marks b/Turbofan/.Turbofan.mdl.py.marks new file mode 100644 index 0000000..5a325ea Binary files /dev/null and b/Turbofan/.Turbofan.mdl.py.marks differ diff --git a/Turbofan/JT9D.viewOut.GasTbl b/Turbofan/JT9D.viewOut.GasTbl new file mode 100644 index 0000000..c195510 --- /dev/null +++ b/Turbofan/JT9D.viewOut.GasTbl @@ -0,0 +1,33726 @@ + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:42 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 0 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 2/ 5/ 1/ 0 Run by: tlavelle + + SUsadfsdfsafMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 0.0 27.00 1539.20 49885.3 0.3583 17873.59 5.2751 0.00 20.218 2730.0 2661.4 2137.5 + core size:19.92 Q: 0.00 Maximum Thrust: 0.0 % Thrust: 0.0 Power code: 0.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1539.20 14.696 545.67 130.43 0.0000 1578.76 14.696 545.67 -----.- 0.0000 1.39999 +FS_2 Inlet.Fl_O 1539.20 14.578 545.67 130.43 0.0000 1591.49 12.015 516.31 5943.4 0.5329 1.39999 +FS_21 Fan.Fl_O 1539.20 23.370 632.71 151.34 0.0000 1069.03 20.339 608.15 4515.2 0.4500 1.39835 +FS_13 Splitter.Fl_O2 1293.91 23.370 632.71 151.34 0.0000 898.67 20.339 608.15 3795.6 0.4500 1.39835 +FS_22 Splitter.Fl_O1 245.29 23.370 632.71 151.34 0.0000 170.36 20.339 608.15 719.5 0.4500 1.39835 +FS_23 Duct1.Fl_O 245.29 23.312 632.71 151.34 0.0000 170.79 20.288 608.15 721.3 0.4500 1.39835 +FS_24 LPC.Fl_O 245.29 52.451 821.38 197.03 0.0000 86.49 45.682 790.04 366.0 0.4500 1.39092 +FS_25 Duct2.Fl_O 245.29 52.320 821.38 197.03 0.0000 86.70 45.568 790.04 366.9 0.4500 1.39092 +FS_3 HPC.Fl_O 245.29 297.127 1398.60 342.54 0.0000 19.92 279.648 1376.50 119.9 0.3000 1.35598 +FS_36 Bld3.Fl_O 223.21 297.127 1398.60 342.54 0.0000 18.13 279.648 1376.50 109.1 0.3000 1.35598 +FS_4 Burner.Fl_O 228.18 280.785 2730.00 733.17 0.0222 27.40 278.976 2725.99 483.4 0.1000 1.29378 +FS_45 HPT.Fl_O 250.25 104.013 2137.47 556.08 0.0202 71.78 98.103 2108.07 439.1 0.3000 1.30940 +FS_48 Duct3.Fl_O 250.25 103.493 2137.47 556.08 0.0202 72.14 97.612 2108.07 441.4 0.3000 1.30940 +FS_5 LPT.Fl_O 250.25 22.575 1522.73 382.68 0.0202 279.13 20.819 1492.01 1477.4 0.3500 1.33516 +FS_7 Duct4.Fl_O 250.25 22.350 1522.73 382.68 0.0202 281.95 21.441 1506.92 2018.9 0.2500 1.33516 +FS_9 Core_Nozz.Fl_O 250.25 22.350 1522.73 382.68 0.0202 281.95 14.696 1369.33 862.9 0.8111 1.33516 +FS_15 BypBld.Fl_O 1293.91 23.370 632.71 151.34 0.0000 898.67 20.339 608.15 3795.6 0.4500 1.39835 +FS_17 Duct5.Fl_O 1293.91 23.195 632.71 151.34 0.0000 905.46 20.187 608.15 3824.3 0.4500 1.39835 +FS_19 Byp_Nozz.Fl_O 1293.91 23.195 632.71 151.34 0.0000 905.46 14.696 555.46 2706.4 0.8345 1.39835 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1591.49 1.603 0.9038 3656.050 1.1595 0.9100 -45541.6 27.92 16.18 +LPC 170.79 2.250 0.8658 3395.283 1.2982 0.8800 -15855.2 30.00 22.36 +HPC 86.70 5.679 0.8625 6357.160 1.7027 0.8900 -50500.9 20.00 19.97 +HPT 27.40 2.700 0.9144 153.112 1.2300 0.9050 50500.9 +LPT 72.14 4.584 0.9288 81.111 1.4037 0.9150 61396.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3051.46 1.420 0.9337 0.927 2.0000 0.5215 1.4369 0.9679 3943.9586 +LPC 183.19 1.383 0.9018 0.927 1.7688 0.9323 3.2631 0.9600 3662.6571 +HPC 206.12 22.630 0.8508 1.000 2.0805 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 5.000 0.9328 100.000 5.0000 1.4085 0.4249 0.9803 1.5311 +LPT 149.90 6.000 0.9276 100.000 6.0000 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1028.00 247.96 88.184 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1028.00 247.96 88.184 +Duct1 0.0025 0.4500 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1028.00 247.96 88.184 +Duct2 0.0025 0.4500 365.99 +Duct3 0.0050 0.3000 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3500 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.5850 1398.60 342.54 297.127 +Duct5 0.0075 0.4500 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 13.4908 1398.60 342.54 297.127 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 632.71 151.34 23.370 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.2751 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 8000.0 33154.6 50500.9 +LP_Shaft 3750.0 85990.1 61396.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.00 0.9940 0.0550 4.96488 0.02224 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.578 0.9975 1.0000 0.9975 2706.36 0.835 961.7 38674.8 +Core_Nozz 1.521 0.9999 1.0000 0.9999 862.88 0.811 1441.3 11210.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:42 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 0 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 1/ 1/ 0/ 0 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 0.0 27.00 1539.20 49885.3 0.3583 17873.59 5.2751 0.00 20.218 2730.0 2661.4 2137.5 + core size:19.92 Q: 0.00 Maximum Thrust: 0.0 % Thrust: 0.0 Power code: 0.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1539.20 14.696 545.67 130.43 0.0000 1578.76 14.696 545.67 -----.- 0.0000 1.39999 +FS_2 Inlet.Fl_O 1539.20 14.578 545.67 130.43 0.0000 1591.49 12.014 516.31 5943.4 0.5330 1.39999 +FS_21 Fan.Fl_O 1539.20 23.370 632.71 151.34 0.0000 1069.03 20.340 608.15 4515.2 0.4500 1.39835 +FS_13 Splitter.Fl_O2 1293.91 23.370 632.71 151.34 0.0000 898.67 20.340 608.15 3795.6 0.4500 1.39835 +FS_22 Splitter.Fl_O1 245.29 23.370 632.71 151.34 0.0000 170.36 20.340 608.15 719.5 0.4500 1.39835 +FS_23 Duct1.Fl_O 245.29 23.312 632.71 151.34 0.0000 170.79 20.289 608.15 721.3 0.4500 1.39835 +FS_24 LPC.Fl_O 245.29 52.451 821.38 197.03 0.0000 86.49 45.676 790.02 366.0 0.4501 1.39092 +FS_25 Duct2.Fl_O 245.29 52.320 821.38 197.03 0.0000 86.70 45.562 790.02 366.9 0.4501 1.39092 +FS_3 HPC.Fl_O 245.29 297.127 1398.60 342.54 0.0000 19.92 279.657 1376.50 119.9 0.3000 1.35598 +FS_36 Bld3.Fl_O 223.21 297.127 1398.60 342.54 0.0000 18.13 279.657 1376.50 109.1 0.3000 1.35598 +FS_4 Burner.Fl_O 228.18 280.785 2730.00 733.17 0.0222 27.40 278.976 2725.99 483.4 0.1000 1.29378 +FS_45 HPT.Fl_O 250.25 104.013 2137.47 556.08 0.0202 71.78 98.096 2108.06 439.1 0.3000 1.30940 +FS_48 Duct3.Fl_O 250.25 103.493 2137.47 556.08 0.0202 72.14 97.605 2108.06 441.4 0.3000 1.30940 +FS_5 LPT.Fl_O 250.25 22.575 1522.73 382.68 0.0202 279.13 20.818 1492.00 1477.4 0.3500 1.33516 +FS_7 Duct4.Fl_O 250.25 22.350 1522.73 382.68 0.0202 281.95 21.440 1506.92 2018.9 0.2500 1.33516 +FS_9 Core_Nozz.Fl_O 250.25 22.350 1522.73 382.68 0.0202 281.95 14.696 1369.33 862.9 0.8111 1.33516 +FS_15 BypBld.Fl_O 1293.91 23.370 632.71 151.34 0.0000 898.67 20.340 608.15 3795.6 0.4500 1.39835 +FS_17 Duct5.Fl_O 1293.91 23.195 632.71 151.34 0.0000 905.46 20.187 608.15 3824.3 0.4500 1.39835 +FS_19 Byp_Nozz.Fl_O 1293.91 23.195 632.71 151.34 0.0000 905.46 14.696 555.46 2706.4 0.8345 1.39835 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1591.49 1.603 0.9038 3656.050 1.1595 0.9100 -45541.6 27.92 16.18 +LPC 170.79 2.250 0.8658 3395.283 1.2982 0.8800 -15855.2 30.00 22.36 +HPC 86.70 5.679 0.8625 6357.160 1.7027 0.8900 -50500.9 20.00 19.97 +HPT 27.40 2.700 0.9144 153.112 1.2300 0.9050 50500.9 +LPT 72.14 4.584 0.9288 81.111 1.4037 0.9150 61396.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3051.46 1.420 0.9337 0.927 2.0000 0.5215 1.4369 0.9679 3943.9586 +LPC 183.19 1.383 0.9018 0.927 1.7688 0.9323 3.2631 0.9600 3662.6571 +HPC 206.12 22.630 0.8508 1.000 2.0805 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 5.000 0.9328 100.000 5.0000 1.4085 0.4249 0.9803 1.5311 +LPT 149.90 6.000 0.9276 100.000 6.0000 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1028.00 247.96 88.184 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1028.00 247.96 88.184 +Duct1 0.0025 0.4500 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1028.00 247.96 88.184 +Duct2 0.0025 0.4501 365.99 +Duct3 0.0050 0.3000 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3500 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.5850 1398.60 342.54 297.127 +Duct5 0.0075 0.4500 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 13.4908 1398.60 342.54 297.127 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 632.71 151.34 23.370 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.2751 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 8000.0 33154.6 50500.9 +LP_Shaft 3750.0 85990.1 61396.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.00 0.9940 0.0550 4.96488 0.02224 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.578 0.9975 1.0000 0.9975 2706.36 0.835 961.7 38674.8 +Core_Nozz 1.521 0.9999 1.0000 0.9999 862.88 0.811 1441.3 11210.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:42 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 800 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 1/ 1/ 0/ 0 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 0.0 27.00 1539.20 49885.3 0.3583 17873.59 5.2751 0.00 20.218 2730.0 2661.4 2137.5 + core size:19.92 Q: 0.00 Maximum Thrust: 49885.3 % Thrust:100.0 Power code: 0.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1539.20 14.696 545.67 130.43 0.0000 1578.76 14.696 545.67 -----.- 0.0000 1.39999 +FS_2 Inlet.Fl_O 1539.20 14.578 545.67 130.43 0.0000 1591.49 12.014 516.31 5943.4 0.5330 1.39999 +FS_21 Fan.Fl_O 1539.20 23.370 632.71 151.34 0.0000 1069.03 20.340 608.15 4515.2 0.4500 1.39835 +FS_13 Splitter.Fl_O2 1293.91 23.370 632.71 151.34 0.0000 898.67 20.340 608.15 3795.6 0.4500 1.39835 +FS_22 Splitter.Fl_O1 245.29 23.370 632.71 151.34 0.0000 170.36 20.340 608.15 719.5 0.4500 1.39835 +FS_23 Duct1.Fl_O 245.29 23.312 632.71 151.34 0.0000 170.79 20.289 608.15 721.3 0.4500 1.39835 +FS_24 LPC.Fl_O 245.29 52.451 821.38 197.03 0.0000 86.49 45.676 790.02 366.0 0.4501 1.39092 +FS_25 Duct2.Fl_O 245.29 52.320 821.38 197.03 0.0000 86.70 45.562 790.02 366.9 0.4501 1.39092 +FS_3 HPC.Fl_O 245.29 297.127 1398.60 342.54 0.0000 19.92 279.657 1376.50 119.9 0.3000 1.35598 +FS_36 Bld3.Fl_O 223.21 297.127 1398.60 342.54 0.0000 18.13 279.657 1376.50 109.1 0.3000 1.35598 +FS_4 Burner.Fl_O 228.18 280.785 2730.00 733.17 0.0222 27.40 278.976 2725.99 483.4 0.1000 1.29378 +FS_45 HPT.Fl_O 250.25 104.013 2137.47 556.08 0.0202 71.78 98.096 2108.06 439.1 0.3000 1.30940 +FS_48 Duct3.Fl_O 250.25 103.493 2137.47 556.08 0.0202 72.14 97.605 2108.06 441.4 0.3000 1.30940 +FS_5 LPT.Fl_O 250.25 22.575 1522.73 382.68 0.0202 279.13 20.818 1492.00 1477.4 0.3500 1.33516 +FS_7 Duct4.Fl_O 250.25 22.350 1522.73 382.68 0.0202 281.95 21.440 1506.92 2018.9 0.2500 1.33516 +FS_9 Core_Nozz.Fl_O 250.25 22.350 1522.73 382.68 0.0202 281.95 14.696 1369.33 862.9 0.8111 1.33516 +FS_15 BypBld.Fl_O 1293.91 23.370 632.71 151.34 0.0000 898.67 20.340 608.15 3795.6 0.4500 1.39835 +FS_17 Duct5.Fl_O 1293.91 23.195 632.71 151.34 0.0000 905.46 20.187 608.15 3824.3 0.4500 1.39835 +FS_19 Byp_Nozz.Fl_O 1293.91 23.195 632.71 151.34 0.0000 905.46 14.696 555.46 2706.4 0.8345 1.39835 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1591.49 1.603 0.9038 3656.050 1.1595 0.9100 -45541.6 27.92 16.18 +LPC 170.79 2.250 0.8658 3395.283 1.2982 0.8800 -15855.2 30.00 22.36 +HPC 86.70 5.679 0.8625 6357.160 1.7027 0.8900 -50500.9 20.00 19.97 +HPT 27.40 2.700 0.9144 153.112 1.2300 0.9050 50500.9 +LPT 72.14 4.584 0.9288 81.111 1.4037 0.9150 61396.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3051.46 1.420 0.9337 0.927 2.0000 0.5215 1.4369 0.9679 3943.9586 +LPC 183.19 1.383 0.9018 0.927 1.7688 0.9323 3.2631 0.9600 3662.6571 +HPC 206.12 22.630 0.8508 1.000 2.0805 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 5.000 0.9328 100.000 5.0000 1.4085 0.4249 0.9803 1.5311 +LPT 149.90 6.000 0.9276 100.000 6.0000 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1028.00 247.96 88.184 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1028.00 247.96 88.184 +Duct1 0.0025 0.4500 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1028.00 247.96 88.184 +Duct2 0.0025 0.4501 365.99 +Duct3 0.0050 0.3000 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3500 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.5850 1398.60 342.54 297.127 +Duct5 0.0075 0.4500 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 13.4908 1398.60 342.54 297.127 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 632.71 151.34 23.370 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.2751 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 8000.0 33154.6 50500.9 +LP_Shaft 3750.0 85990.1 61396.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.00 0.9940 0.0550 4.96488 0.02224 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.578 0.9975 1.0000 0.9975 2706.36 0.835 961.7 38674.8 +Core_Nozz 1.521 0.9999 1.0000 0.9999 862.88 0.811 1441.3 11210.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:42 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 801 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 689.0 27.00 1549.51 40505.6 0.4407 17851.91 5.3129 228.51 20.172 2730.0 2661.5 2137.9 + core size:19.94 Q: 57.80 Maximum Thrust: 40505.6 % Thrust:100.0 Power code: 0.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1549.51 14.739 547.56 130.88 0.0000 1587.44 14.334 543.21 13710.1 0.2000 1.39995 +FS_2 Inlet.Fl_O 1549.51 14.650 547.56 130.88 0.0000 1597.03 12.050 517.81 5943.4 0.5357 1.39995 +FS_21 Fan.Fl_O 1549.51 23.408 634.33 151.73 0.0000 1075.82 20.327 609.32 4515.2 0.4537 1.39830 +FS_13 Splitter.Fl_O2 1304.06 23.408 634.33 151.73 0.0000 905.40 20.318 609.24 3795.6 0.4544 1.39830 +FS_22 Splitter.Fl_O1 245.45 23.408 634.33 151.73 0.0000 170.42 20.371 609.69 719.5 0.4502 1.39830 +FS_23 Duct1.Fl_O 245.45 23.349 634.33 151.73 0.0000 170.84 20.320 609.69 721.3 0.4502 1.39830 +FS_24 LPC.Fl_O 245.45 52.763 824.62 197.82 0.0000 86.20 46.000 793.40 366.0 0.4482 1.39077 +FS_25 Duct2.Fl_O 245.45 52.631 824.62 197.82 0.0000 86.42 45.885 793.40 366.9 0.4482 1.39077 +FS_3 HPC.Fl_O 245.45 297.320 1401.26 343.24 0.0000 19.94 279.802 1379.08 119.9 0.3003 1.35582 +FS_36 Bld3.Fl_O 223.36 297.320 1401.26 343.24 0.0000 18.15 279.802 1379.08 109.1 0.3003 1.35582 +FS_4 Burner.Fl_O 228.32 280.967 2730.00 733.13 0.0222 27.40 279.157 2725.99 483.4 0.1000 1.29381 +FS_45 HPT.Fl_O 250.41 104.158 2137.94 556.20 0.0202 71.73 98.241 2108.56 439.1 0.2998 1.30941 +FS_48 Duct3.Fl_O 250.41 103.637 2137.94 556.20 0.0202 72.09 97.750 2108.56 441.4 0.2998 1.30941 +FS_5 LPT.Fl_O 250.41 22.423 1520.33 382.01 0.0202 280.98 20.651 1489.17 1477.4 0.3527 1.33531 +FS_7 Duct4.Fl_O 250.41 22.199 1520.33 382.01 0.0202 283.82 21.283 1504.32 2018.9 0.2518 1.33531 +FS_9 Core_Nozz.Fl_O 250.41 22.199 1520.33 382.01 0.0202 283.82 14.334 1360.77 862.9 0.8294 1.33531 +FS_15 BypBld.Fl_O 1304.06 23.408 634.33 151.73 0.0000 905.40 20.318 609.24 3795.6 0.4544 1.39830 +FS_17 Duct5.Fl_O 1304.06 23.232 634.33 151.73 0.0000 912.25 20.166 609.24 3824.3 0.4544 1.39830 +FS_19 Byp_Nozz.Fl_O 1304.06 23.232 634.33 151.73 0.0000 912.25 14.334 552.68 2706.4 0.8601 1.39830 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1597.03 1.598 0.9029 3660.326 1.1585 0.9091 -45707.8 28.55 16.72 +LPC 170.84 2.260 0.8655 3400.782 1.3000 0.8799 -16004.8 29.65 22.13 +HPC 86.42 5.649 0.8630 6348.586 1.6993 0.8904 -50501.9 20.33 20.32 +HPT 27.40 2.698 0.9145 153.206 1.2299 0.9050 50502.0 +LPT 72.09 4.622 0.9287 81.338 1.4062 0.9148 61712.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3062.06 1.416 0.9328 0.928 2.0370 0.5215 1.4369 0.9679 3943.9586 +LPC 183.25 1.386 0.9016 0.929 1.7609 0.9323 3.2631 0.9600 3662.6571 +HPC 205.45 22.492 0.8514 0.999 2.0816 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 4.995 0.9328 100.062 4.9953 1.4085 0.4249 0.9803 1.5311 +LPT 149.80 6.052 0.9275 100.279 6.0524 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 13710.05 11005.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1031.03 248.71 88.478 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1031.03 248.71 88.478 +Duct1 0.0025 0.4502 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1031.03 248.71 88.478 +Duct2 0.0025 0.4482 365.99 +Duct3 0.0050 0.2998 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3527 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.5908 1401.26 343.24 297.320 +Duct5 0.0075 0.4544 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 13.4998 1401.26 343.24 297.320 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 634.33 151.73 23.408 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3129 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 8004.9 33134.8 50502.0 +LP_Shaft 3760.9 86182.0 61712.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.00 0.9940 0.0550 4.95886 0.02220 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.621 0.9975 1.0000 0.9975 2706.36 0.860 988.7 40074.4 +Core_Nozz 1.549 0.9999 1.0000 0.9999 862.88 0.829 1469.4 11436.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:42 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 802 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 0.0 27.00 1597.56 39310.2 0.4633 18211.53 5.3613 286.28 19.820 2730.0 2661.7 2137.9 + core size:19.97 Q: 92.58 Maximum Thrust: 39310.2 % Thrust:100.0 Power code: 0.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1597.56 15.349 552.49 132.06 0.0000 1578.70 14.696 545.67 11054.5 0.2500 1.39986 +FS_2 Inlet.Fl_O 1597.56 15.257 552.49 132.06 0.0000 1588.24 12.587 522.94 5943.4 0.5314 1.39986 +FS_21 Fan.Fl_O 1597.56 24.199 638.47 152.73 0.0000 1076.41 21.010 613.26 4515.2 0.4541 1.39818 +FS_13 Splitter.Fl_O2 1346.42 24.199 638.47 152.73 0.0000 907.20 20.990 613.10 3795.6 0.4556 1.39818 +FS_22 Splitter.Fl_O1 251.14 24.199 638.47 152.73 0.0000 169.21 21.112 614.11 719.5 0.4461 1.39818 +FS_23 Duct1.Fl_O 251.14 24.139 638.47 152.73 0.0000 169.64 21.059 614.11 721.3 0.4461 1.39818 +FS_24 LPC.Fl_O 251.14 54.277 828.76 198.83 0.0000 85.95 47.368 797.63 366.0 0.4465 1.39058 +FS_25 Duct2.Fl_O 251.14 54.141 828.76 198.83 0.0000 86.17 47.249 797.63 366.9 0.4465 1.39058 +FS_3 HPC.Fl_O 251.14 304.205 1405.43 344.33 0.0000 19.97 286.224 1383.12 119.9 0.3009 1.35558 +FS_36 Bld3.Fl_O 228.53 304.205 1405.43 344.33 0.0000 18.17 286.224 1383.12 109.1 0.3009 1.35558 +FS_4 Burner.Fl_O 233.59 287.474 2730.00 733.07 0.0221 27.40 285.622 2725.99 483.4 0.1000 1.29386 +FS_45 HPT.Fl_O 256.20 106.514 2137.92 556.15 0.0201 71.77 100.457 2108.51 439.1 0.3000 1.30945 +FS_48 Duct3.Fl_O 256.20 105.981 2137.92 556.15 0.0201 72.13 99.954 2108.51 441.4 0.3000 1.30945 +FS_5 LPT.Fl_O 256.20 22.956 1520.80 382.12 0.0201 280.84 21.144 1489.67 1477.4 0.3525 1.33532 +FS_7 Duct4.Fl_O 256.20 22.727 1520.80 382.12 0.0201 283.68 21.790 1504.79 2018.9 0.2516 1.33532 +FS_9 Core_Nozz.Fl_O 256.20 22.727 1520.80 382.12 0.0201 283.68 14.696 1361.70 862.9 0.8279 1.33532 +FS_15 BypBld.Fl_O 1346.42 24.199 638.47 152.73 0.0000 907.20 20.990 613.10 3795.6 0.4556 1.39818 +FS_17 Duct5.Fl_O 1346.42 24.018 638.47 152.73 0.0000 914.05 20.832 613.10 3824.3 0.4556 1.39818 +FS_19 Byp_Nozz.Fl_O 1346.42 24.018 638.47 152.73 0.0000 914.05 14.696 554.98 2706.4 0.8680 1.39818 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1588.24 1.586 0.9039 3636.605 1.1556 0.9099 -46702.7 29.43 17.01 +LPC 169.64 2.249 0.8650 3382.901 1.2981 0.8793 -16380.8 29.41 21.75 +HPC 86.17 5.619 0.8634 6341.382 1.6958 0.8906 -51699.1 20.72 20.74 +HPT 27.40 2.699 0.9145 153.417 1.2301 0.9050 51699.1 +LPT 72.13 4.617 0.9285 81.174 1.4058 0.9145 63083.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3045.22 1.408 0.9338 0.922 2.0364 0.5215 1.4369 0.9679 3943.9586 +LPC 181.96 1.383 0.9010 0.924 1.7523 0.9323 3.2631 0.9600 3662.6571 +HPC 204.85 22.352 0.8518 0.998 2.0867 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 4.999 0.9328 100.199 4.9986 1.4085 0.4249 0.9803 1.5311 +LPT 149.87 6.045 0.9273 100.077 6.0451 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 11054.52 14214.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1035.19 249.75 90.775 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1035.19 249.75 90.775 +Duct1 0.0025 0.4461 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1035.19 249.75 90.775 +Duct2 0.0025 0.4465 365.99 +Duct3 0.0050 0.3000 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3525 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.7898 1405.43 344.33 304.205 +Duct5 0.0075 0.4556 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 13.8125 1405.43 344.33 304.205 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 638.47 152.73 24.199 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3613 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 8015.9 33873.7 51699.1 +LP_Shaft 3753.3 88274.9 63083.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.00 0.9940 0.0550 5.05876 0.02214 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.634 0.9975 1.0000 0.9975 2706.36 0.868 999.8 41841.2 +Core_Nozz 1.546 0.9999 1.0000 0.9999 862.88 0.828 1467.3 11683.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:42 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 803 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 4/ 14/ 1/ 2 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 5000.0 27.00 1463.74 31920.9 0.5270 16823.53 5.3232 450.56 20.538 2730.0 2661.6 2139.4 + core size:19.95 Q: 197.26 Maximum Thrust: 31920.9 % Thrust:100.0 Power code: 0.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1463.74 13.653 544.74 130.20 0.0000 1614.72 12.228 527.84 7481.9 0.4000 1.40001 +FS_2 Inlet.Fl_O 1463.74 13.584 544.74 130.20 0.0000 1622.84 11.069 513.76 5943.4 0.5488 1.40001 +FS_21 Fan.Fl_O 1463.74 21.763 632.26 151.23 0.0000 1091.30 18.798 606.42 4515.2 0.4624 1.39836 +FS_13 Splitter.Fl_O2 1232.25 21.763 632.26 151.23 0.0000 918.71 18.788 606.32 3795.6 0.4632 1.39836 +FS_22 Splitter.Fl_O1 231.49 21.763 632.26 151.23 0.0000 172.59 18.852 606.91 719.5 0.4577 1.39836 +FS_23 Duct1.Fl_O 231.49 21.709 632.26 151.23 0.0000 173.02 18.805 606.91 721.3 0.4577 1.39836 +FS_24 LPC.Fl_O 231.49 50.111 827.45 198.51 0.0000 85.75 43.769 796.55 366.0 0.4451 1.39064 +FS_25 Duct2.Fl_O 231.49 49.986 827.45 198.51 0.0000 85.96 43.660 796.55 366.9 0.4451 1.39064 +FS_3 HPC.Fl_O 231.49 280.393 1402.33 343.52 0.0000 19.95 263.857 1380.11 119.9 0.3005 1.35576 +FS_36 Bld3.Fl_O 210.65 280.393 1402.33 343.52 0.0000 18.15 263.857 1380.11 109.1 0.3005 1.35576 +FS_4 Burner.Fl_O 215.33 264.971 2729.99 733.12 0.0222 27.40 263.263 2725.99 483.4 0.1000 1.29382 +FS_45 HPT.Fl_O 236.16 98.534 2139.38 556.60 0.0202 71.53 92.969 2110.16 439.1 0.2989 1.30937 +FS_48 Duct3.Fl_O 236.16 98.041 2139.38 556.60 0.0202 71.89 92.504 2110.16 441.4 0.2989 1.30937 +FS_5 LPT.Fl_O 236.16 20.688 1512.75 379.94 0.0202 286.50 18.981 1480.30 1477.4 0.3608 1.33572 +FS_7 Duct4.Fl_O 236.16 20.481 1512.75 379.94 0.0202 289.40 19.601 1496.12 2018.9 0.2571 1.33572 +FS_9 Core_Nozz.Fl_O 236.16 20.481 1512.75 379.94 0.0202 289.40 12.228 1326.86 862.9 0.9047 1.33572 +FS_15 BypBld.Fl_O 1232.25 21.763 632.26 151.23 0.0000 918.71 18.788 606.32 3795.6 0.4632 1.39836 +FS_17 Duct5.Fl_O 1232.25 21.600 632.26 151.23 0.0000 925.66 18.647 606.32 3824.3 0.4632 1.39836 +FS_19 Byp_Nozz.Fl_O 1232.25 21.600 632.26 151.23 0.0000 925.66 12.228 537.49 2706.4 0.9395 1.39836 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1622.84 1.602 0.8960 3713.846 1.1607 0.9027 -43550.4 28.58 17.60 +LPC 173.02 2.308 0.8657 3447.224 1.3087 0.8805 -15483.3 29.02 22.06 +HPC 85.96 5.609 0.8640 6335.717 1.6947 0.8910 -47493.2 20.65 20.68 +HPT 27.40 2.689 0.9144 153.159 1.2291 0.9050 47494.8 +LPT 71.89 4.739 0.9288 82.287 1.4142 0.9146 59029.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3111.44 1.419 0.9257 0.942 2.1385 0.5215 1.4369 0.9679 3943.9586 +LPC 185.59 1.401 0.9018 0.941 1.7518 0.9323 3.2631 0.9600 3662.6571 +HPC 204.35 22.308 0.8523 0.997 2.0762 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 4.976 0.9328 100.031 4.9756 1.4085 0.4249 0.9803 1.5311 +LPT 149.38 6.216 0.9276 101.449 6.2159 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 7481.90 20497.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1033.22 249.26 83.741 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1033.22 249.26 83.741 +Duct1 0.0025 0.4577 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1033.22 249.26 83.741 +Duct2 0.0025 0.4451 365.99 +Duct3 0.0050 0.2989 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3608 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.1021 1402.33 343.52 280.393 +Duct5 0.0075 0.4632 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.7318 1402.33 343.52 280.393 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 632.26 151.23 21.763 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3232 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 8002.4 31171.5 47494.8 +LP_Shaft 3806.0 81457.0 59029.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2729.99 0.9940 0.0550 4.67320 0.02218 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.766 0.9975 1.0000 0.9975 2706.36 0.939 1065.1 40792.5 +Core_Nozz 1.675 0.9999 1.0000 0.9999 862.88 0.905 1584.0 11626.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:42 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 804 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 9/ 19/ 1/ 7 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 20000.0 0.00 1016.12 19469.4 0.5732 11159.70 5.0408 622.40 22.702 2527.7 2463.5 1977.7 + core size:19.92 Q: 245.29 Maximum Thrust: 19469.4 % Thrust:100.0 Power code: 0.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1016.12 8.616 479.66 114.61 0.0000 1666.72 6.753 447.35 5769.7 0.6000 1.40110 +FS_2 Inlet.Fl_O 1016.12 8.573 479.66 114.61 0.0000 1675.11 6.843 449.69 5943.4 0.5763 1.40110 +FS_21 Fan.Fl_O 1016.12 14.097 564.19 134.87 0.0000 1104.76 12.120 540.34 4515.2 0.4697 1.39964 +FS_13 Splitter.Fl_O2 847.91 14.097 564.19 134.87 0.0000 921.88 12.155 540.79 3795.6 0.4651 1.39964 +FS_22 Splitter.Fl_O1 168.21 14.097 564.19 134.87 0.0000 182.88 11.925 537.86 719.5 0.4947 1.39964 +FS_23 Duct1.Fl_O 168.21 14.062 564.19 134.87 0.0000 183.34 11.896 537.86 721.3 0.4947 1.39964 +FS_24 LPC.Fl_O 168.21 34.999 756.56 181.26 0.0000 85.30 30.624 728.52 366.0 0.4416 1.39399 +FS_25 Duct2.Fl_O 168.21 34.911 756.56 181.26 0.0000 85.52 30.548 728.52 366.9 0.4416 1.39399 +FS_3 HPC.Fl_O 168.21 195.598 1288.02 313.86 0.0000 19.92 184.110 1267.41 119.9 0.2991 1.36263 +FS_36 Bld3.Fl_O 153.07 195.598 1288.02 313.86 0.0000 18.12 184.110 1267.41 109.1 0.2991 1.36263 +FS_4 Burner.Fl_O 156.17 184.841 2527.67 670.78 0.0203 27.41 183.648 2523.90 483.4 0.0998 1.29933 +FS_45 HPT.Fl_O 171.31 69.337 1977.75 509.04 0.0184 70.90 65.496 1950.84 439.1 0.2952 1.31596 +FS_48 Duct3.Fl_O 171.31 68.990 1977.75 509.04 0.0184 71.26 65.169 1950.84 441.4 0.2952 1.31596 +FS_5 LPT.Fl_O 171.31 14.181 1379.26 343.29 0.0184 289.50 12.984 1348.40 1477.4 0.3639 1.34440 +FS_7 Duct4.Fl_O 171.31 14.039 1379.26 343.29 0.0184 292.43 13.422 1363.46 2018.9 0.2591 1.34440 +FS_9 Core_Nozz.Fl_O 171.31 14.039 1379.26 343.29 0.0184 292.43 7.514 1172.59 862.9 1.0000 1.34440 +FS_15 BypBld.Fl_O 847.91 14.097 564.19 134.87 0.0000 921.88 12.155 540.79 3795.6 0.4651 1.39964 +FS_17 Duct5.Fl_O 847.91 13.992 564.19 134.87 0.0000 928.85 12.063 540.79 3824.3 0.4651 1.39964 +FS_19 Byp_Nozz.Fl_O 847.91 13.992 564.19 134.87 0.0000 928.85 7.389 470.01 2706.4 1.0000 1.39964 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.644 0.8675 3944.235 1.1762 0.8765 -29134.9 24.72 17.46 +LPC 183.34 2.489 0.8683 3636.786 1.3410 0.8838 -11039.8 28.36 23.27 +HPC 85.52 5.603 0.8652 6324.778 1.7025 0.8922 -31558.5 20.18 20.24 +HPT 27.41 2.666 0.9135 151.936 1.2304 0.9037 31558.7 +LPT 71.26 4.865 0.9327 85.290 1.4339 0.9187 40173.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.448 0.8962 1.000 2.3712 0.5215 1.4369 0.9679 3943.9586 +LPC 196.66 1.456 0.9045 0.993 1.7659 0.9323 3.2631 0.9600 3662.6571 +HPC 203.31 22.278 0.8535 0.995 2.0438 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.921 0.9319 99.232 4.9207 1.4085 0.4249 0.9803 1.5311 +LPT 148.07 6.392 0.9315 105.152 6.3916 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5769.68 19656.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 946.28 227.67 58.452 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 946.28 227.67 58.452 +Duct1 0.0025 0.4947 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 946.28 227.67 58.452 +Duct2 0.0025 0.4416 365.99 +Duct3 0.0050 0.2952 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3639 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.8873 1288.02 313.86 195.598 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.2515 1288.02 313.86 195.598 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 564.19 134.87 14.097 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0408 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7638.7 21698.6 31558.7 +LP_Shaft 3793.0 55627.9 40173.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2527.67 0.9940 0.0550 3.09992 0.02025 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.072 0.9976 1.0000 0.9975 2706.36 1.000 1060.6 29670.7 +Core_Nozz 2.079 0.9998 1.0000 0.9999 862.88 1.000 1652.6 9455.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:42 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 805 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 10/ 20/ 1/ 8 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.780 35000.0 18.00 621.16 10588.8 0.6168 6530.68 5.0414 776.33 22.712 2442.5 2380.4 1908.1 + core size:19.93 Q: 212.25 Maximum Thrust: 10588.8 % Thrust:100.0 Power code: 0.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 621.16 5.170 462.14 110.41 0.0000 1666.72 3.458 411.85 5084.3 0.7800 1.40126 +FS_2 Inlet.Fl_O 621.16 5.144 462.14 110.41 0.0000 1675.11 4.106 433.26 5943.4 0.5763 1.40126 +FS_21 Fan.Fl_O 621.16 8.459 543.62 129.94 0.0000 1104.74 7.273 520.63 4515.2 0.4697 1.40003 +FS_13 Splitter.Fl_O2 518.34 8.459 543.62 129.94 0.0000 921.88 7.294 521.06 3795.6 0.4651 1.40003 +FS_22 Splitter.Fl_O1 102.82 8.459 543.62 129.94 0.0000 182.86 7.156 518.24 719.5 0.4946 1.40003 +FS_23 Duct1.Fl_O 102.82 8.438 543.62 129.94 0.0000 183.32 7.139 518.24 721.3 0.4946 1.40003 +FS_24 LPC.Fl_O 102.82 21.002 729.26 174.64 0.0000 85.31 18.378 702.18 366.0 0.4415 1.39504 +FS_25 Duct2.Fl_O 102.82 20.950 729.26 174.64 0.0000 85.52 18.332 702.18 366.9 0.4415 1.39504 +FS_3 HPC.Fl_O 102.82 117.417 1244.21 302.61 0.0000 19.93 110.509 1224.16 119.9 0.2991 1.36537 +FS_36 Bld3.Fl_O 93.56 117.417 1244.21 302.61 0.0000 18.14 110.509 1224.16 109.1 0.2991 1.36537 +FS_4 Burner.Fl_O 95.38 110.959 2442.48 644.83 0.0194 27.41 110.243 2438.82 483.4 0.0997 1.30182 +FS_45 HPT.Fl_O 104.63 41.589 1908.13 488.81 0.0176 70.91 39.285 1881.97 439.1 0.2948 1.31912 +FS_48 Duct3.Fl_O 104.63 41.381 1908.13 488.81 0.0176 71.27 39.089 1881.97 441.4 0.2948 1.31912 +FS_5 LPT.Fl_O 104.63 8.487 1326.41 328.97 0.0176 289.73 7.770 1296.46 1477.4 0.3637 1.34812 +FS_7 Duct4.Fl_O 104.63 8.402 1326.41 328.97 0.0176 292.66 8.033 1311.08 2018.9 0.2590 1.34812 +FS_9 Core_Nozz.Fl_O 104.63 8.402 1326.41 328.97 0.0176 292.66 4.491 1125.93 862.9 1.0000 1.34812 +FS_15 BypBld.Fl_O 518.34 8.459 543.62 129.94 0.0000 921.88 7.294 521.06 3795.6 0.4651 1.40003 +FS_17 Duct5.Fl_O 518.34 8.396 543.62 129.94 0.0000 928.85 7.239 521.06 3824.3 0.4651 1.40003 +FS_19 Byp_Nozz.Fl_O 518.34 8.396 543.62 129.94 0.0000 928.85 4.433 452.83 2706.4 1.0000 1.40003 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.645 0.8675 3944.235 1.1763 0.8765 -17159.1 24.71 17.45 +LPC 183.32 2.489 0.8683 3636.641 1.3415 0.8839 -6503.7 28.34 23.26 +HPC 85.52 5.605 0.8652 6324.831 1.7061 0.8922 -18615.0 20.13 20.19 +HPT 27.41 2.668 0.9134 151.750 1.2322 0.9036 18615.3 +LPT 71.27 4.876 0.9324 85.231 1.4386 0.9183 23662.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8963 1.000 2.3708 0.5215 1.4369 0.9679 3943.9586 +LPC 196.64 1.456 0.9044 0.993 1.7655 0.9323 3.2631 0.9600 3662.6571 +HPC 203.31 22.286 0.8535 0.995 2.0422 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.926 0.9317 99.110 4.9257 1.4085 0.4249 0.9803 1.5311 +LPT 148.09 6.407 0.9312 105.079 6.4066 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5084.34 14987.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 912.86 219.43 35.082 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 912.86 219.43 35.082 +Duct1 0.0025 0.4946 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 912.86 219.43 35.082 +Duct2 0.0025 0.4415 365.99 +Duct3 0.0050 0.2948 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3637 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.5986 1244.21 302.61 117.417 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.6549 1244.21 302.61 117.417 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 543.62 129.94 8.459 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0414 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7499.7 13036.5 18615.3 +LP_Shaft 3723.1 33380.4 23662.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2442.48 0.9940 0.0550 1.81408 0.01939 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.428 0.9965 1.0000 0.9975 2706.36 1.000 1041.0 19412.2 +Core_Nozz 2.430 0.9981 1.0000 0.9999 862.88 1.000 1621.5 6164.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:42 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 806 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 4/ 14/ 1/ 2 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 34000.0 0.00 674.22 11194.4 0.6113 6842.60 5.0408 782.15 22.723 2375.3 2314.8 1853.1 + core size:19.94 Q: 234.10 Maximum Thrust: 11194.4 % Thrust:100.0 Power code: 0.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 674.22 5.528 448.46 107.14 0.0000 1666.72 3.626 397.42 5041.1 0.8000 1.40133 +FS_2 Inlet.Fl_O 674.22 5.500 448.46 107.14 0.0000 1675.11 4.391 420.44 5943.4 0.5763 1.40133 +FS_21 Fan.Fl_O 674.22 9.045 527.55 126.08 0.0000 1104.74 7.776 505.23 4515.2 0.4696 1.40035 +FS_13 Splitter.Fl_O2 562.61 9.045 527.55 126.08 0.0000 921.86 7.799 505.65 3795.6 0.4650 1.40035 +FS_22 Splitter.Fl_O1 111.61 9.045 527.55 126.08 0.0000 182.88 7.652 502.91 719.5 0.4946 1.40035 +FS_23 Duct1.Fl_O 111.61 9.023 527.55 126.08 0.0000 183.34 7.633 502.91 721.3 0.4946 1.40035 +FS_24 LPC.Fl_O 111.61 22.451 707.81 169.45 0.0000 85.35 19.643 681.47 366.0 0.4416 1.39575 +FS_25 Duct2.Fl_O 111.61 22.395 707.81 169.45 0.0000 85.56 19.594 681.47 366.9 0.4416 1.39575 +FS_3 HPC.Fl_O 111.61 125.611 1209.83 293.82 0.0000 19.94 118.213 1190.23 119.9 0.2990 1.36753 +FS_36 Bld3.Fl_O 101.57 125.611 1209.83 293.82 0.0000 18.15 118.213 1190.23 109.1 0.2990 1.36753 +FS_4 Burner.Fl_O 103.47 118.702 2375.33 624.51 0.0187 27.41 117.936 2371.75 483.4 0.0997 1.30391 +FS_45 HPT.Fl_O 113.51 44.462 1853.12 472.96 0.0170 70.92 41.999 1827.56 439.1 0.2946 1.32175 +FS_48 Duct3.Fl_O 113.51 44.240 1853.12 472.96 0.0170 71.27 41.789 1827.56 441.4 0.2946 1.32175 +FS_5 LPT.Fl_O 113.51 9.055 1284.79 317.78 0.0170 289.95 8.289 1255.55 1477.4 0.3636 1.35110 +FS_7 Duct4.Fl_O 113.51 8.965 1284.79 317.78 0.0170 292.88 8.570 1269.82 2018.9 0.2589 1.35110 +FS_9 Core_Nozz.Fl_O 113.51 8.965 1284.79 317.78 0.0170 292.88 4.788 1089.27 862.8 1.0000 1.35110 +FS_15 BypBld.Fl_O 562.61 9.045 527.55 126.08 0.0000 921.86 7.799 505.65 3795.6 0.4650 1.40035 +FS_17 Duct5.Fl_O 562.61 8.978 527.55 126.08 0.0000 928.83 7.740 505.65 3824.3 0.4650 1.40035 +FS_19 Byp_Nozz.Fl_O 562.61 8.978 527.55 126.08 0.0000 928.83 4.740 439.42 2706.4 1.0000 1.40035 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.645 0.8675 3944.235 1.1764 0.8766 -18072.7 24.71 17.45 +LPC 183.34 2.488 0.8683 3636.556 1.3417 0.8840 -6849.2 28.37 23.29 +HPC 85.56 5.609 0.8651 6326.001 1.7093 0.8923 -19639.2 20.09 20.15 +HPT 27.41 2.670 0.9133 151.628 1.2338 0.9035 19639.8 +LPT 71.27 4.886 0.9323 85.197 1.4424 0.9179 24921.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8963 1.000 2.3706 0.5215 1.4369 0.9679 3943.9586 +LPC 196.66 1.456 0.9045 0.993 1.7664 0.9323 3.2631 0.9600 3662.6571 +HPC 203.42 22.306 0.8535 0.995 2.0424 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.930 0.9316 99.031 4.9299 1.4085 0.4249 0.9803 1.5311 +LPT 148.11 6.420 0.9311 105.038 6.4203 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5041.09 16390.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 886.61 212.98 37.516 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 886.61 212.98 37.516 +Duct1 0.0025 0.4946 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 886.61 212.98 37.516 +Duct2 0.0025 0.4416 365.99 +Duct3 0.0050 0.2946 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.9064 1209.83 293.82 125.611 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.1386 1209.83 293.82 125.611 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 527.55 126.08 9.045 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0408 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7390.0 13958.2 19639.8 +LP_Shaft 3667.6 35688.5 24921.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2375.33 0.9940 0.0550 1.90072 0.01871 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.476 0.9962 1.0000 0.9975 2706.36 1.000 1025.5 20949.7 +Core_Nozz 2.473 0.9978 1.0000 0.9999 862.88 1.000 1596.5 6635.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:42 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 807 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 2/ 12/ 1/ 0 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 35000.0 0.00 674.69 10979.8 0.6277 6892.42 5.0406 827.30 22.721 2387.6 2326.8 1863.2 + core size:19.94 Q: 252.05 Maximum Thrust: 10979.8 % Thrust:100.0 Power code: 0.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 674.69 5.547 450.95 107.73 0.0000 1666.73 3.458 393.85 4955.8 0.8500 1.40132 +FS_2 Inlet.Fl_O 674.69 5.519 450.95 107.73 0.0000 1675.12 4.406 422.78 5943.4 0.5763 1.40132 +FS_21 Fan.Fl_O 674.69 9.077 530.49 126.78 0.0000 1104.75 7.803 508.04 4515.2 0.4696 1.40030 +FS_13 Splitter.Fl_O2 563.00 9.077 530.49 126.78 0.0000 921.86 7.826 508.46 3795.6 0.4650 1.40030 +FS_22 Splitter.Fl_O1 111.69 9.077 530.49 126.78 0.0000 182.89 7.678 505.70 719.5 0.4946 1.40030 +FS_23 Duct1.Fl_O 111.69 9.054 530.49 126.78 0.0000 183.35 7.659 505.70 721.3 0.4946 1.40030 +FS_24 LPC.Fl_O 111.69 22.530 711.72 170.40 0.0000 85.34 19.711 685.24 366.0 0.4416 1.39562 +FS_25 Duct2.Fl_O 111.69 22.473 711.72 170.40 0.0000 85.56 19.662 685.24 366.9 0.4416 1.39562 +FS_3 HPC.Fl_O 111.69 126.036 1216.12 295.42 0.0000 19.94 118.613 1196.43 119.9 0.2990 1.36713 +FS_36 Bld3.Fl_O 101.64 126.036 1216.12 295.42 0.0000 18.15 118.613 1196.43 109.1 0.2990 1.36713 +FS_4 Burner.Fl_O 103.56 119.104 2387.59 628.21 0.0188 27.41 118.335 2383.99 483.4 0.0997 1.30351 +FS_45 HPT.Fl_O 113.61 44.618 1863.17 475.85 0.0171 70.92 42.146 1837.49 439.1 0.2946 1.32126 +FS_48 Duct3.Fl_O 113.61 44.395 1863.17 475.85 0.0171 71.28 41.935 1837.49 441.4 0.2946 1.32126 +FS_5 LPT.Fl_O 113.61 9.091 1292.40 319.82 0.0171 289.90 8.322 1263.03 1477.4 0.3636 1.35055 +FS_7 Duct4.Fl_O 113.61 9.000 1292.40 319.82 0.0171 292.83 8.604 1277.37 2018.9 0.2589 1.35055 +FS_9 Core_Nozz.Fl_O 113.61 9.000 1292.40 319.82 0.0171 292.83 4.807 1095.97 862.8 1.0000 1.35055 +FS_15 BypBld.Fl_O 563.00 9.077 530.49 126.78 0.0000 921.86 7.826 508.46 3795.6 0.4650 1.40030 +FS_17 Duct5.Fl_O 563.00 9.009 530.49 126.78 0.0000 928.83 7.767 508.46 3824.3 0.4650 1.40030 +FS_19 Byp_Nozz.Fl_O 563.00 9.009 530.49 126.78 0.0000 928.83 4.757 441.87 2706.4 1.0000 1.40030 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.12 1.645 0.8675 3944.235 1.1764 0.8766 -18186.1 24.71 17.45 +LPC 183.35 2.488 0.8683 3636.571 1.3416 0.8840 -6892.4 28.37 23.29 +HPC 85.56 5.608 0.8651 6325.800 1.7087 0.8922 -19757.7 20.10 20.15 +HPT 27.41 2.669 0.9133 151.650 1.2335 0.9035 19757.5 +LPT 71.28 4.883 0.9323 85.203 1.4416 0.9180 25078.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8963 1.000 2.3706 0.5215 1.4369 0.9679 3943.9586 +LPC 196.66 1.456 0.9045 0.993 1.7663 0.9323 3.2631 0.9600 3662.6571 +HPC 203.40 22.303 0.8535 0.995 2.0422 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.929 0.9316 99.046 4.9291 1.4085 0.4249 0.9803 1.5311 +LPT 148.11 6.417 0.9311 105.045 6.4172 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4955.84 17348.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 891.40 214.16 37.645 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 891.40 214.16 37.645 +Duct1 0.0025 0.4946 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 891.40 214.16 37.645 +Duct2 0.0025 0.4416 365.99 +Duct3 0.0050 0.2946 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.9093 1216.12 295.42 126.036 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.1431 1216.12 295.42 126.036 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 530.49 126.78 9.077 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0406 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7410.1 14003.7 19757.5 +LP_Shaft 3677.8 35814.0 25078.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2387.59 0.9940 0.0550 1.91456 0.01884 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.605 0.9953 1.0000 0.9975 2706.36 1.000 1028.4 21510.7 +Core_Nozz 2.603 0.9968 1.0000 0.9999 862.88 1.000 1601.1 6817.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:42 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 808 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 0.0 27.00 1539.20 49885.7 0.3583 17873.61 5.2751 0.00 20.219 2730.0 2661.4 2137.5 + core size:19.92 Q: 0.00 Maximum Thrust: 49885.7 % Thrust:100.0 Power code: 0.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1539.20 14.696 545.67 130.43 0.0000 1578.76 14.696 545.67 -----.- 0.0000 1.39999 +FS_2 Inlet.Fl_O 1539.20 14.578 545.67 130.43 0.0000 1591.49 12.014 516.31 5943.4 0.5330 1.39999 +FS_21 Fan.Fl_O 1539.20 23.370 632.71 151.34 0.0000 1069.03 20.340 608.15 4515.2 0.4500 1.39835 +FS_13 Splitter.Fl_O2 1293.92 23.370 632.71 151.34 0.0000 898.67 20.340 608.15 3795.6 0.4500 1.39835 +FS_22 Splitter.Fl_O1 245.29 23.370 632.71 151.34 0.0000 170.36 20.340 608.15 719.5 0.4500 1.39835 +FS_23 Duct1.Fl_O 245.29 23.312 632.71 151.34 0.0000 170.79 20.289 608.15 721.3 0.4500 1.39835 +FS_24 LPC.Fl_O 245.29 52.452 821.39 197.03 0.0000 86.48 45.677 790.03 366.0 0.4501 1.39092 +FS_25 Duct2.Fl_O 245.29 52.321 821.39 197.03 0.0000 86.70 45.563 790.03 366.9 0.4501 1.39092 +FS_3 HPC.Fl_O 245.29 297.130 1398.61 342.54 0.0000 19.92 279.660 1376.50 119.9 0.3000 1.35598 +FS_36 Bld3.Fl_O 223.21 297.130 1398.61 342.54 0.0000 18.13 279.660 1376.50 109.1 0.3000 1.35598 +FS_4 Burner.Fl_O 228.18 280.788 2730.00 733.17 0.0222 27.40 278.979 2725.99 483.4 0.1000 1.29378 +FS_45 HPT.Fl_O 250.25 104.014 2137.47 556.08 0.0202 71.78 98.097 2108.06 439.1 0.3000 1.30940 +FS_48 Duct3.Fl_O 250.25 103.494 2137.47 556.08 0.0202 72.14 97.607 2108.06 441.4 0.3000 1.30940 +FS_5 LPT.Fl_O 250.25 22.575 1522.73 382.68 0.0202 279.13 20.818 1492.00 1477.4 0.3500 1.33516 +FS_7 Duct4.Fl_O 250.25 22.350 1522.73 382.68 0.0202 281.95 21.440 1506.92 2018.9 0.2500 1.33516 +FS_9 Core_Nozz.Fl_O 250.25 22.350 1522.73 382.68 0.0202 281.95 14.696 1369.33 862.9 0.8111 1.33516 +FS_15 BypBld.Fl_O 1293.92 23.370 632.71 151.34 0.0000 898.67 20.340 608.15 3795.6 0.4500 1.39835 +FS_17 Duct5.Fl_O 1293.92 23.195 632.71 151.34 0.0000 905.46 20.187 608.15 3824.3 0.4500 1.39835 +FS_19 Byp_Nozz.Fl_O 1293.92 23.195 632.71 151.34 0.0000 905.46 14.696 555.46 2706.3 0.8345 1.39835 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1591.49 1.603 0.9038 3656.082 1.1595 0.9100 -45542.3 27.92 16.18 +LPC 170.79 2.250 0.8657 3395.310 1.2982 0.8800 -15855.7 30.00 22.36 +HPC 86.70 5.679 0.8625 6357.146 1.7027 0.8900 -50501.2 20.00 19.97 +HPT 27.40 2.700 0.9145 153.112 1.2300 0.9050 50501.1 +LPT 72.14 4.584 0.9288 81.112 1.4037 0.9150 61397.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3051.49 1.420 0.9337 0.927 2.0000 0.5215 1.4369 0.9679 3943.9586 +LPC 183.19 1.383 0.9018 0.927 1.7688 0.9323 3.2631 0.9600 3662.6571 +HPC 206.12 22.630 0.8508 1.000 2.0805 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.000 0.9328 100.000 5.0000 1.4085 0.4249 0.9803 1.5311 +LPT 149.90 6.000 0.9276 100.001 6.0001 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1028.00 247.96 88.185 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1028.00 247.96 88.185 +Duct1 0.0025 0.4500 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1028.00 247.96 88.185 +Duct2 0.0025 0.4501 365.99 +Duct3 0.0050 0.3000 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3500 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.5851 1398.61 342.54 297.130 +Duct5 0.0075 0.4500 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 13.4908 1398.61 342.54 297.130 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 632.71 151.34 23.370 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.2751 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 8000.0 33154.6 50501.1 +LP_Shaft 3750.0 85990.6 61397.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.00 0.9940 0.0550 4.96489 0.02224 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.578 0.9975 1.0000 0.9975 2706.36 0.835 961.7 38675.1 +Core_Nozz 1.521 0.9999 1.0000 0.9999 862.88 0.811 1441.3 11210.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:42 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 1 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 1/ 1/ 0/ 0 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 0.0 27.00 1539.20 49885.7 0.3583 17873.61 5.2751 0.00 20.219 2730.0 2661.4 2137.5 + core size:19.92 Q: 0.00 Maximum Thrust: 49885.7 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1539.20 14.696 545.67 130.43 0.0000 1578.76 14.696 545.67 -----.- 0.0000 1.39999 +FS_2 Inlet.Fl_O 1539.20 14.578 545.67 130.43 0.0000 1591.49 12.014 516.31 5943.4 0.5330 1.39999 +FS_21 Fan.Fl_O 1539.20 23.370 632.71 151.34 0.0000 1069.03 20.340 608.15 4515.2 0.4500 1.39835 +FS_13 Splitter.Fl_O2 1293.92 23.370 632.71 151.34 0.0000 898.67 20.340 608.15 3795.6 0.4500 1.39835 +FS_22 Splitter.Fl_O1 245.29 23.370 632.71 151.34 0.0000 170.36 20.340 608.15 719.5 0.4500 1.39835 +FS_23 Duct1.Fl_O 245.29 23.312 632.71 151.34 0.0000 170.79 20.289 608.15 721.3 0.4500 1.39835 +FS_24 LPC.Fl_O 245.29 52.452 821.39 197.03 0.0000 86.48 45.677 790.03 366.0 0.4501 1.39092 +FS_25 Duct2.Fl_O 245.29 52.321 821.39 197.03 0.0000 86.70 45.563 790.03 366.9 0.4501 1.39092 +FS_3 HPC.Fl_O 245.29 297.130 1398.61 342.54 0.0000 19.92 279.660 1376.50 119.9 0.3000 1.35598 +FS_36 Bld3.Fl_O 223.21 297.130 1398.61 342.54 0.0000 18.13 279.660 1376.50 109.1 0.3000 1.35598 +FS_4 Burner.Fl_O 228.18 280.788 2730.00 733.17 0.0222 27.40 278.979 2725.99 483.4 0.1000 1.29378 +FS_45 HPT.Fl_O 250.25 104.014 2137.47 556.08 0.0202 71.78 98.097 2108.06 439.1 0.3000 1.30940 +FS_48 Duct3.Fl_O 250.25 103.494 2137.47 556.08 0.0202 72.14 97.607 2108.06 441.4 0.3000 1.30940 +FS_5 LPT.Fl_O 250.25 22.575 1522.73 382.68 0.0202 279.13 20.818 1492.00 1477.4 0.3500 1.33516 +FS_7 Duct4.Fl_O 250.25 22.350 1522.73 382.68 0.0202 281.95 21.440 1506.92 2018.9 0.2500 1.33516 +FS_9 Core_Nozz.Fl_O 250.25 22.350 1522.73 382.68 0.0202 281.95 14.696 1369.33 862.9 0.8111 1.33516 +FS_15 BypBld.Fl_O 1293.92 23.370 632.71 151.34 0.0000 898.67 20.340 608.15 3795.6 0.4500 1.39835 +FS_17 Duct5.Fl_O 1293.92 23.195 632.71 151.34 0.0000 905.46 20.187 608.15 3824.3 0.4500 1.39835 +FS_19 Byp_Nozz.Fl_O 1293.92 23.195 632.71 151.34 0.0000 905.46 14.696 555.46 2706.3 0.8345 1.39835 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1591.49 1.603 0.9038 3656.082 1.1595 0.9100 -45542.3 27.92 16.18 +LPC 170.79 2.250 0.8657 3395.310 1.2982 0.8800 -15855.7 30.00 22.36 +HPC 86.70 5.679 0.8625 6357.146 1.7027 0.8900 -50501.2 20.00 19.97 +HPT 27.40 2.700 0.9145 153.112 1.2300 0.9050 50501.1 +LPT 72.14 4.584 0.9288 81.112 1.4037 0.9150 61397.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3051.49 1.420 0.9337 0.927 2.0000 0.5215 1.4369 0.9679 3943.9586 +LPC 183.19 1.383 0.9018 0.927 1.7688 0.9323 3.2631 0.9600 3662.6571 +HPC 206.12 22.630 0.8508 1.000 2.0805 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.000 0.9328 100.000 5.0000 1.4085 0.4249 0.9803 1.5311 +LPT 149.90 6.000 0.9276 100.001 6.0001 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1028.00 247.96 88.185 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1028.00 247.96 88.185 +Duct1 0.0025 0.4500 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1028.00 247.96 88.185 +Duct2 0.0025 0.4501 365.99 +Duct3 0.0050 0.3000 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3500 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.5851 1398.61 342.54 297.130 +Duct5 0.0075 0.4500 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 13.4908 1398.61 342.54 297.130 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 632.71 151.34 23.370 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.2751 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 8000.0 33154.6 50501.1 +LP_Shaft 3750.0 85990.6 61397.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.00 0.9940 0.0550 4.96489 0.02224 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.578 0.9975 1.0000 0.9975 2706.36 0.835 961.7 38675.1 +Core_Nozz 1.521 0.9999 1.0000 0.9999 862.88 0.811 1441.3 11210.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:42 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 2 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 0.0 27.00 1467.35 44898.1 0.3482 15633.30 5.4331 0.00 18.420 2626.0 2560.6 2051.7 + core size:20.06 Q: 0.00 Maximum Thrust: 49885.7 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1467.35 14.696 545.67 130.43 0.0000 1505.06 14.696 545.67 -----.- 0.0000 1.39999 +FS_2 Inlet.Fl_O 1467.35 14.578 545.67 130.43 0.0000 1517.20 12.308 519.89 5943.4 0.4977 1.39999 +FS_21 Fan.Fl_O 1467.35 22.538 625.19 149.53 0.0000 1050.44 19.735 601.96 4515.2 0.4399 1.39855 +FS_13 Splitter.Fl_O2 1239.26 22.538 625.19 149.53 0.0000 887.15 19.704 601.69 3795.6 0.4425 1.39855 +FS_22 Splitter.Fl_O1 228.09 22.538 625.19 149.53 0.0000 163.29 19.894 603.34 719.5 0.4261 1.39855 +FS_23 Duct1.Fl_O 228.09 22.482 625.19 149.53 0.0000 163.69 19.845 603.34 721.3 0.4261 1.39855 +FS_24 LPC.Fl_O 228.09 48.621 802.22 192.36 0.0000 85.74 42.470 772.20 366.0 0.4449 1.39184 +FS_25 Duct2.Fl_O 228.09 48.500 802.22 192.36 0.0000 85.96 42.364 772.20 366.9 0.4449 1.39184 +FS_3 HPC.Fl_O 228.09 270.694 1360.51 332.62 0.0000 20.06 254.550 1338.60 119.9 0.3020 1.35823 +FS_36 Bld3.Fl_O 207.57 270.694 1360.51 332.62 0.0000 18.25 254.550 1338.60 109.1 0.3020 1.35823 +FS_4 Burner.Fl_O 211.91 255.806 2626.04 700.72 0.0209 27.39 254.158 2622.16 483.4 0.0999 1.29671 +FS_45 HPT.Fl_O 232.44 94.402 2051.69 530.57 0.0190 71.97 89.002 2023.05 439.1 0.3005 1.31296 +FS_48 Duct3.Fl_O 232.44 93.930 2051.69 530.57 0.0190 72.33 88.557 2023.05 441.4 0.3005 1.31296 +FS_5 LPT.Fl_O 232.44 21.219 1470.14 367.95 0.0190 271.02 19.671 1442.18 1477.4 0.3378 1.33877 +FS_7 Duct4.Fl_O 232.44 21.007 1470.14 367.95 0.0190 273.76 20.204 1455.69 2018.9 0.2419 1.33877 +FS_9 Core_Nozz.Fl_O 232.44 21.007 1470.14 367.95 0.0190 273.76 14.696 1342.14 862.8 0.7452 1.33877 +FS_15 BypBld.Fl_O 1239.26 22.538 625.19 149.53 0.0000 887.15 19.704 601.69 3795.6 0.4425 1.39855 +FS_17 Duct5.Fl_O 1239.26 22.369 625.19 149.53 0.0000 893.85 19.557 601.69 3824.3 0.4425 1.39855 +FS_19 Byp_Nozz.Fl_O 1239.26 22.369 625.19 149.53 0.0000 893.85 14.696 554.55 2706.4 0.7986 1.39855 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1517.20 1.546 0.9086 3508.341 1.1457 0.9141 -39660.5 31.20 16.19 +LPC 163.69 2.163 0.8631 3277.641 1.2832 0.8770 -13820.5 29.51 20.75 +HPC 85.96 5.581 0.8635 6335.349 1.6959 0.8907 -45266.0 21.36 21.38 +HPT 27.39 2.710 0.9146 153.752 1.2332 0.9049 45264.4 +LPT 72.33 4.427 0.9266 79.445 1.3956 0.9125 53479.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2908.79 1.380 0.9387 0.890 1.9124 0.5215 1.4369 0.9679 3943.9586 +LPC 175.58 1.356 0.8990 0.895 1.7403 0.9323 3.2631 0.9600 3662.6571 +HPC 204.36 22.179 0.8519 0.997 2.1016 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.024 0.9329 100.418 5.0241 1.4085 0.4249 0.9803 1.5311 +LPT 150.30 5.780 0.9254 97.945 5.7800 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1001.86 241.45 81.051 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1001.86 241.45 81.051 +Duct1 0.0025 0.4261 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1001.86 241.45 81.051 +Duct2 0.0025 0.4449 365.99 +Duct3 0.0050 0.3005 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3378 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.9833 1360.51 332.62 270.694 +Duct5 0.0075 0.4425 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.5451 1360.51 332.62 270.694 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 625.19 149.53 22.538 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.4331 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7879.0 30173.1 45264.4 +LP_Shaft 3598.5 78054.5 53479.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2626.04 0.9940 0.0550 4.34258 0.02092 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.522 0.9975 1.0000 0.9975 2706.36 0.799 919.6 35418.5 +Core_Nozz 1.429 0.9999 1.0000 0.9999 862.88 0.745 1312.2 9479.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:42 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 3 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 0.0 27.00 1389.01 39908.4 0.3402 13576.41 5.5949 0.00 16.657 2524.5 2462.0 1968.0 + core size:20.18 Q: 0.00 Maximum Thrust: 49885.7 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1389.01 14.696 545.67 130.43 0.0000 1424.70 14.696 545.67 -----.- 0.0000 1.39999 +FS_2 Inlet.Fl_O 1389.01 14.578 545.67 130.43 0.0000 1436.19 12.594 523.32 5943.4 0.4619 1.39999 +FS_21 Fan.Fl_O 1389.01 21.687 617.81 147.76 0.0000 1027.25 19.128 596.08 4515.2 0.4275 1.39872 +FS_13 Splitter.Fl_O2 1178.39 21.687 617.81 147.76 0.0000 871.49 19.073 595.58 3795.6 0.4325 1.39872 +FS_22 Splitter.Fl_O1 210.62 21.687 617.81 147.76 0.0000 155.76 19.406 598.53 719.5 0.4017 1.39872 +FS_23 Duct1.Fl_O 210.62 21.633 617.81 147.76 0.0000 156.15 19.358 598.53 721.3 0.4017 1.39872 +FS_24 LPC.Fl_O 210.62 44.699 782.04 187.45 0.0000 85.03 39.155 753.34 366.0 0.4399 1.39282 +FS_25 Duct2.Fl_O 210.62 44.588 782.04 187.45 0.0000 85.24 39.057 753.34 366.9 0.4399 1.39282 +FS_3 HPC.Fl_O 210.62 244.796 1321.64 322.54 0.0000 20.18 229.997 1299.95 119.9 0.3039 1.36057 +FS_36 Bld3.Fl_O 191.66 244.796 1321.64 322.54 0.0000 18.37 229.997 1299.95 109.1 0.3039 1.36057 +FS_4 Burner.Fl_O 195.43 231.332 2524.45 669.35 0.0197 27.39 229.842 2520.69 483.4 0.0997 1.29980 +FS_45 HPT.Fl_O 214.39 85.001 1968.02 505.97 0.0179 72.20 80.106 1940.11 439.1 0.3011 1.31667 +FS_48 Duct3.Fl_O 214.39 84.576 1968.02 505.97 0.0179 72.56 79.705 1940.11 441.4 0.3011 1.31667 +FS_5 LPT.Fl_O 214.39 20.042 1422.47 354.71 0.0179 260.34 18.703 1397.57 1477.4 0.3222 1.34220 +FS_7 Duct4.Fl_O 214.39 19.841 1422.47 354.71 0.0179 262.97 19.144 1409.54 2018.9 0.2314 1.34220 +FS_9 Core_Nozz.Fl_O 214.39 19.841 1422.47 354.71 0.0179 262.97 14.696 1316.97 862.9 0.6803 1.34220 +FS_15 BypBld.Fl_O 1178.39 21.687 617.81 147.76 0.0000 871.49 19.073 595.58 3795.6 0.4325 1.39872 +FS_17 Duct5.Fl_O 1178.39 21.525 617.81 147.76 0.0000 878.07 18.930 595.58 3824.3 0.4325 1.39872 +FS_19 Byp_Nozz.Fl_O 1178.39 21.525 617.81 147.76 0.0000 878.07 14.696 554.05 2706.4 0.7590 1.39872 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1436.19 1.488 0.9082 3348.520 1.1322 0.9132 -34054.0 34.07 15.93 +LPC 156.15 2.066 0.8601 3146.962 1.2658 0.8735 -11827.8 29.16 19.30 +HPC 85.24 5.490 0.8641 6316.573 1.6900 0.8911 -40256.7 22.63 22.74 +HPT 27.39 2.722 0.9147 154.372 1.2364 0.9047 40256.7 +LPT 72.56 4.220 0.9245 77.421 1.3835 0.9105 45881.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2753.68 1.339 0.9382 0.849 1.8598 0.5215 1.4369 0.9679 3943.9586 +LPC 167.50 1.327 0.8959 0.859 1.7161 0.9323 3.2631 0.9600 3662.6571 +HPC 202.65 21.757 0.8525 0.994 2.1192 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.052 0.9330 100.823 5.0518 1.4085 0.4249 0.9803 1.5311 +LPT 150.78 5.492 0.9233 95.450 5.4918 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 974.80 234.73 73.918 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 974.80 234.73 73.918 +Duct1 0.0025 0.4017 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 974.80 234.73 73.918 +Duct2 0.0025 0.4399 365.99 +Duct3 0.0050 0.3011 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3222 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.3716 1321.64 322.54 244.796 +Duct5 0.0075 0.4325 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.5839 1321.64 322.54 244.796 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 617.81 147.76 21.687 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5949 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7756.2 27259.7 40256.7 +LP_Shaft 3434.6 70161.6 45881.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2524.45 0.9940 0.0550 3.77122 0.01968 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.465 0.9975 1.0000 0.9975 2706.36 0.759 873.6 31995.4 +Core_Nozz 1.350 0.9999 1.0000 0.9999 862.88 0.680 1187.6 7913.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:42 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 4 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 0.0 27.00 1211.50 29931.4 0.3276 9806.91 5.9189 0.00 13.207 2305.9 2250.0 1787.8 + core size:20.47 Q: 0.00 Maximum Thrust: 49885.7 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1211.50 14.696 545.67 130.43 0.0000 1242.63 14.696 545.67 -----.- 0.0000 1.39999 +FS_2 Inlet.Fl_O 1211.50 14.578 545.67 130.43 0.0000 1252.65 13.136 529.66 5943.4 0.3886 1.39999 +FS_21 Fan.Fl_O 1211.50 19.954 602.46 144.06 0.0000 961.63 17.932 584.37 4515.2 0.3938 1.39901 +FS_13 Splitter.Fl_O2 1036.40 19.954 602.46 144.06 0.0000 822.64 17.850 583.60 3795.6 0.4023 1.39901 +FS_22 Splitter.Fl_O1 175.10 19.954 602.46 144.06 0.0000 138.99 18.330 588.04 719.5 0.3505 1.39901 +FS_23 Duct1.Fl_O 175.10 19.904 602.46 144.06 0.0000 139.33 18.284 588.04 721.3 0.3505 1.39901 +FS_24 LPC.Fl_O 175.10 36.682 736.38 176.37 0.0000 83.59 32.312 710.40 366.0 0.4302 1.39479 +FS_25 Duct2.Fl_O 175.10 36.590 736.38 176.37 0.0000 83.80 32.231 710.40 366.9 0.4302 1.39479 +FS_3 HPC.Fl_O 175.10 194.088 1236.05 300.52 0.0000 20.47 182.000 1214.91 119.9 0.3080 1.36588 +FS_36 Bld3.Fl_O 159.34 194.088 1236.05 300.52 0.0000 18.63 182.000 1214.91 109.1 0.3080 1.36588 +FS_4 Burner.Fl_O 162.06 183.414 2305.93 602.99 0.0171 27.38 182.233 2302.44 483.4 0.0994 1.30687 +FS_45 HPT.Fl_O 177.82 66.676 1787.84 453.94 0.0156 72.77 62.773 1761.52 439.1 0.3027 1.32551 +FS_48 Duct3.Fl_O 177.82 66.343 1787.84 453.94 0.0156 73.13 62.459 1761.52 441.4 0.3027 1.32551 +FS_5 LPT.Fl_O 177.82 18.137 1329.63 329.22 0.0156 230.69 17.203 1311.53 1477.4 0.2808 1.34929 +FS_7 Duct4.Fl_O 177.82 17.956 1329.63 329.22 0.0156 233.02 17.465 1320.11 2018.9 0.2031 1.34929 +FS_9 Core_Nozz.Fl_O 177.82 17.956 1329.63 329.22 0.0156 233.02 14.696 1262.10 862.9 0.5514 1.34929 +FS_15 BypBld.Fl_O 1036.40 19.954 602.46 144.06 0.0000 822.64 17.850 583.60 3795.6 0.4023 1.39901 +FS_17 Duct5.Fl_O 1036.40 19.804 602.46 144.06 0.0000 828.86 17.716 583.60 3824.3 0.4023 1.39901 +FS_19 Byp_Nozz.Fl_O 1036.40 19.804 602.46 144.06 0.0000 828.86 14.696 553.27 2706.4 0.6671 1.39901 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1252.65 1.369 0.9011 2973.122 1.1041 0.9053 -23375.9 35.97 14.74 +LPC 139.33 1.843 0.8539 2829.535 1.2223 0.8658 -8003.1 29.83 16.79 +HPC 83.80 5.304 0.8645 6283.366 1.6785 0.8909 -30757.1 25.40 25.52 +HPT 27.38 2.751 0.9150 155.910 1.2445 0.9049 30757.1 +LPT 73.13 3.658 0.9190 72.122 1.3446 0.9055 31378.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2401.79 1.257 0.9309 0.754 1.7750 0.5215 1.4369 0.9679 3943.9586 +LPC 149.46 1.258 0.8894 0.773 1.6989 0.9323 3.2631 0.9600 3662.6571 +HPC 199.22 20.898 0.8528 0.988 2.1564 0.4206 0.2163 1.0137 6357.1603 +HPT 30.12 5.121 0.9333 101.828 5.1207 1.4085 0.4249 0.9803 1.5311 +LPT 151.96 4.708 0.9178 88.917 4.7076 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 914.45 219.82 59.664 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 914.45 219.82 59.664 +Duct1 0.0025 0.3505 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 914.45 219.82 59.664 +Duct2 0.0025 0.4302 365.99 +Duct3 0.0050 0.3027 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2808 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.1285 1236.05 300.52 194.088 +Duct5 0.0075 0.4023 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.6305 1236.05 300.52 194.088 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 602.46 144.06 19.954 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9189 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7486.8 21576.5 30757.1 +LP_Shaft 3049.5 54042.6 31378.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2305.93 0.9940 0.0550 2.72414 0.01710 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.348 0.9975 1.0000 0.9975 2706.36 0.667 767.2 24714.2 +Core_Nozz 1.222 0.9999 1.0000 0.9999 862.88 0.551 944.0 5217.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:42 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 5 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 8/ 18/ 1/ 6 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 0.0 27.00 996.39 19954.4 0.3199 6383.00 6.1985 0.00 9.795 2039.2 1991.3 1570.4 + core size:20.87 Q: 0.00 Maximum Thrust: 49885.7 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 996.39 14.696 545.67 130.43 0.0000 1021.99 14.696 545.67 -----.- 0.0000 1.39999 +FS_2 Inlet.Fl_O 996.39 14.578 545.67 130.43 0.0000 1030.24 13.642 535.41 5943.4 0.3095 1.39999 +FS_21 Fan.Fl_O 996.39 18.207 585.60 140.01 0.0000 854.57 16.790 572.21 4515.2 0.3422 1.39927 +FS_13 Splitter.Fl_O2 857.97 18.207 585.60 140.01 0.0000 735.86 16.713 571.46 3795.6 0.3519 1.39927 +FS_22 Splitter.Fl_O1 138.42 18.207 585.60 140.01 0.0000 118.72 17.155 575.73 719.5 0.2929 1.39927 +FS_23 Duct1.Fl_O 138.42 18.161 585.60 140.01 0.0000 119.01 17.112 575.73 721.3 0.2929 1.39927 +FS_24 LPC.Fl_O 138.42 28.861 683.35 163.55 0.0000 80.90 25.675 661.01 366.0 0.4125 1.39659 +FS_25 Duct2.Fl_O 138.42 28.789 683.35 163.55 0.0000 81.10 25.611 661.01 366.9 0.4125 1.39659 +FS_3 HPC.Fl_O 138.42 143.944 1131.39 273.91 0.0000 20.87 134.595 1110.94 119.9 0.3141 1.37247 +FS_36 Bld3.Fl_O 125.96 143.944 1131.39 273.91 0.0000 18.99 134.595 1110.94 109.1 0.3141 1.37247 +FS_4 Burner.Fl_O 127.73 136.027 2039.21 524.06 0.0141 27.36 135.153 2036.05 483.4 0.0990 1.31676 +FS_45 HPT.Fl_O 140.19 48.911 1570.36 392.87 0.0128 73.29 46.005 1546.24 439.1 0.3036 1.33764 +FS_48 Duct3.Fl_O 140.19 48.666 1570.36 392.87 0.0128 73.66 45.775 1546.24 441.4 0.3036 1.33764 +FS_5 LPT.Fl_O 140.19 16.717 1226.90 301.50 0.0128 189.55 16.148 1215.75 1477.4 0.2264 1.35755 +FS_7 Duct4.Fl_O 140.19 16.550 1226.90 301.50 0.0128 191.46 16.247 1220.95 2018.9 0.1650 1.35755 +FS_9 Core_Nozz.Fl_O 140.19 16.550 1226.90 301.50 0.0128 191.46 14.696 1189.07 862.8 0.4209 1.35755 +FS_15 BypBld.Fl_O 857.97 18.207 585.60 140.01 0.0000 735.86 16.713 571.46 3795.6 0.3519 1.39927 +FS_17 Duct5.Fl_O 857.97 18.070 585.60 140.01 0.0000 741.42 16.587 571.46 3824.3 0.3519 1.39927 +FS_19 Byp_Nozz.Fl_O 857.97 18.070 585.60 140.01 0.0000 741.42 14.696 552.03 2706.4 0.5516 1.39927 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1030.24 1.249 0.8957 2502.849 1.0732 0.8990 -13514.1 34.31 11.90 +LPC 119.01 1.589 0.8447 2416.019 1.1669 0.8546 -4608.6 34.06 14.21 +HPC 81.10 5.000 0.8640 6231.937 1.6557 0.8902 -21613.8 29.89 30.08 +HPT 27.36 2.781 0.9155 158.405 1.2550 0.9052 21613.8 +LPT 73.66 2.911 0.9083 64.782 1.2799 0.8956 18122.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1975.34 1.173 0.9254 0.635 1.6951 0.5215 1.4369 0.9679 3943.9586 +LPC 127.66 1.181 0.8799 0.660 1.7278 0.9323 3.2631 0.9600 3662.6571 +HPC 192.81 19.491 0.8524 0.980 2.1907 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.192 0.9339 103.457 5.1921 1.4085 0.4249 0.9803 1.5311 +LPT 153.06 3.666 0.9071 79.868 3.6660 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 842.47 202.17 45.659 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 842.47 202.17 45.659 +Duct1 0.0025 0.2929 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 842.47 202.17 45.659 +Duct2 0.0025 0.4125 365.99 +Duct3 0.0050 0.3036 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2264 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.8446 1131.39 273.91 143.944 +Duct5 0.0075 0.3519 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.6129 1131.39 273.91 143.944 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 585.60 140.01 18.207 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.1985 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7153.2 15869.6 21613.8 +LP_Shaft 2567.2 37076.2 18122.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2039.21 0.9940 0.0550 1.77306 0.01408 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.230 0.9975 1.0000 0.9975 2706.36 0.552 633.7 16899.1 +Core_Nozz 1.126 0.9999 1.0000 0.9999 862.88 0.421 701.2 3055.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 6 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 0.0 27.00 710.96 9977.2 0.3341 3333.78 6.1327 0.00 6.388 1680.9 1644.1 1283.4 + core size:21.60 Q: 0.00 Maximum Thrust: 49885.7 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 710.96 14.696 545.67 130.43 0.0000 729.23 14.696 545.67 -----.- 0.0000 1.39999 +FS_2 Inlet.Fl_O 710.96 14.578 545.67 130.43 0.0000 735.11 14.119 540.70 5943.4 0.2144 1.39999 +FS_21 Fan.Fl_O 710.96 16.465 567.40 135.64 0.0000 663.71 15.720 559.95 4515.2 0.2580 1.39958 +FS_13 Splitter.Fl_O2 611.29 16.465 567.40 135.64 0.0000 570.66 15.684 559.58 3795.6 0.2644 1.39958 +FS_22 Splitter.Fl_O1 99.68 16.465 567.40 135.64 0.0000 93.05 15.896 561.72 719.5 0.2248 1.39958 +FS_23 Duct1.Fl_O 99.68 16.424 567.40 135.64 0.0000 93.28 15.856 561.72 721.3 0.2248 1.39958 +FS_24 LPC.Fl_O 99.68 21.249 619.79 148.23 0.0000 75.36 19.255 602.61 366.0 0.3780 1.39867 +FS_25 Duct2.Fl_O 99.68 21.196 619.79 148.23 0.0000 75.55 19.206 602.61 366.9 0.3780 1.39867 +FS_3 HPC.Fl_O 99.68 93.875 993.87 239.46 0.0000 21.60 87.309 974.16 119.9 0.3255 1.38109 +FS_36 Bld3.Fl_O 90.71 93.875 993.87 239.46 0.0000 19.66 87.309 974.16 109.1 0.3255 1.38109 +FS_4 Burner.Fl_O 91.63 88.712 1680.91 421.94 0.0102 27.33 88.143 1678.20 483.4 0.0982 1.33404 +FS_45 HPT.Fl_O 100.60 31.609 1283.38 315.28 0.0093 73.57 29.717 1262.71 439.1 0.3027 1.35638 +FS_48 Duct3.Fl_O 100.60 31.451 1283.38 315.28 0.0093 73.94 29.569 1262.71 441.4 0.3027 1.35638 +FS_5 LPT.Fl_O 100.60 15.694 1091.95 265.95 0.0093 136.69 15.421 1086.81 1477.4 0.1602 1.36854 +FS_7 Duct4.Fl_O 100.60 15.537 1091.95 265.95 0.0093 138.07 15.391 1089.17 2018.9 0.1176 1.36854 +FS_9 Core_Nozz.Fl_O 100.60 15.537 1091.95 265.95 0.0093 138.07 14.696 1075.67 862.8 0.2863 1.36854 +FS_15 BypBld.Fl_O 611.29 16.465 567.40 135.64 0.0000 570.66 15.684 559.58 3795.6 0.2644 1.39958 +FS_17 Duct5.Fl_O 611.29 16.342 567.40 135.64 0.0000 574.97 15.567 559.58 3824.3 0.2644 1.39958 +FS_19 Byp_Nozz.Fl_O 611.29 16.342 567.40 135.64 0.0000 574.97 14.696 550.45 2706.4 0.3925 1.39958 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 735.11 1.129 0.8886 1852.695 1.0398 0.8906 -5246.0 35.30 6.86 +LPC 93.28 1.294 0.8260 1816.875 1.0923 0.8322 -1775.5 47.52 12.46 +HPC 75.55 4.429 0.8617 6131.143 1.6036 0.8868 -12866.0 39.02 39.56 +HPT 27.33 2.807 0.9167 163.473 1.2700 0.9058 12865.9 +LPT 73.94 2.004 0.8835 53.045 1.1753 0.8737 7021.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1409.48 1.090 0.9180 0.470 1.6108 0.5215 1.4369 0.9679 3943.9586 +LPC 100.06 1.090 0.8603 0.496 1.8995 0.9323 3.2631 0.9600 3662.6571 +HPC 179.60 16.851 0.8501 0.964 2.2611 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.252 0.9351 106.767 5.2519 1.4085 0.4249 0.9803 1.5311 +LPT 153.65 2.401 0.8824 65.398 2.4006 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 752.04 180.16 31.844 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 752.04 180.16 31.844 +Duct1 0.0025 0.2248 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 752.04 180.16 31.844 +Duct2 0.0025 0.3780 365.99 +Duct3 0.0050 0.3027 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1602 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.4887 993.87 239.46 93.875 +Duct5 0.0075 0.2644 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.4822 993.87 239.46 93.875 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 567.40 135.64 16.465 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.1327 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6702.2 10082.2 12865.9 +LP_Shaft 1900.3 19405.7 7021.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1680.91 0.9940 0.0550 0.92605 0.01021 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.112 0.9975 1.0000 0.9975 2706.36 0.392 450.2 8553.8 +Core_Nozz 1.057 0.9999 1.0000 0.9999 862.88 0.286 455.2 1423.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 7 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 0.0 27.00 1549.97 45024.4 0.3985 17941.71 5.2900 114.51 20.169 2730.0 2661.4 2137.6 + core size:19.93 Q: 14.81 Maximum Thrust: 45024.4 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1549.97 14.799 546.76 130.69 0.0000 1580.30 14.696 545.67 26813.0 0.1000 1.39997 +FS_2 Inlet.Fl_O 1549.97 14.695 546.76 130.69 0.0000 1591.45 12.110 517.34 5943.4 0.5330 1.39997 +FS_21 Fan.Fl_O 1549.97 23.516 633.62 151.56 0.0000 1070.58 20.457 608.95 4515.2 0.4508 1.39832 +FS_13 Splitter.Fl_O2 1303.55 23.516 633.62 151.56 0.0000 900.37 20.454 608.92 3795.6 0.4511 1.39832 +FS_22 Splitter.Fl_O1 246.42 23.516 633.62 151.56 0.0000 170.20 20.474 609.09 719.5 0.4495 1.39832 +FS_23 Duct1.Fl_O 246.42 23.458 633.62 151.56 0.0000 170.63 20.423 609.09 721.3 0.4495 1.39832 +FS_24 LPC.Fl_O 246.42 52.788 822.62 197.33 0.0000 86.39 45.987 791.30 366.0 0.4495 1.39087 +FS_25 Duct2.Fl_O 246.42 52.656 822.62 197.33 0.0000 86.61 45.872 791.30 366.9 0.4495 1.39087 +FS_3 HPC.Fl_O 246.42 298.488 1399.72 342.84 0.0000 19.93 280.922 1377.58 119.9 0.3001 1.35591 +FS_36 Bld3.Fl_O 224.24 298.488 1399.72 342.84 0.0000 18.14 280.922 1377.58 109.1 0.3001 1.35591 +FS_4 Burner.Fl_O 229.22 282.071 2729.99 733.16 0.0222 27.40 280.253 2725.99 483.4 0.1000 1.29380 +FS_45 HPT.Fl_O 251.40 104.497 2137.56 556.10 0.0202 71.78 98.553 2108.15 439.1 0.3000 1.30940 +FS_48 Duct3.Fl_O 251.40 103.975 2137.56 556.10 0.0202 72.14 98.060 2108.15 441.4 0.3000 1.30940 +FS_5 LPT.Fl_O 251.40 22.648 1522.32 382.56 0.0202 279.48 20.879 1491.51 1477.4 0.3505 1.33519 +FS_7 Duct4.Fl_O 251.40 22.421 1522.32 382.56 0.0202 282.30 21.506 1506.47 2018.9 0.2503 1.33519 +FS_9 Core_Nozz.Fl_O 251.40 22.421 1522.32 382.56 0.0202 282.30 14.696 1367.83 862.9 0.8144 1.33519 +FS_15 BypBld.Fl_O 1303.55 23.516 633.62 151.56 0.0000 900.37 20.454 608.92 3795.6 0.4511 1.39832 +FS_17 Duct5.Fl_O 1303.55 23.340 633.62 151.56 0.0000 907.18 20.300 608.92 3824.3 0.4511 1.39832 +FS_19 Byp_Nozz.Fl_O 1303.55 23.340 633.62 151.56 0.0000 907.18 14.696 555.28 2706.4 0.8406 1.39832 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1591.45 1.600 0.9038 3653.518 1.1589 0.9099 -45769.8 28.18 16.34 +LPC 170.63 2.250 0.8656 3393.865 1.2983 0.8799 -15957.1 29.90 22.26 +HPC 86.61 5.669 0.8627 6354.305 1.7015 0.8901 -50730.2 20.12 20.10 +HPT 27.40 2.699 0.9145 153.159 1.2300 0.9050 50730.8 +LPT 72.14 4.591 0.9288 81.134 1.4041 0.9149 61726.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3051.38 1.418 0.9337 0.926 2.0080 0.5215 1.4369 0.9679 3943.9586 +LPC 183.02 1.383 0.9017 0.927 1.7661 0.9323 3.2631 0.9600 3662.6571 +HPC 205.90 22.582 0.8510 1.000 2.0815 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.000 0.9328 100.031 4.9995 1.4085 0.4249 0.9803 1.5311 +LPT 149.89 6.009 0.9276 100.029 6.0093 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 26812.95 5516.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1029.20 248.26 88.671 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1029.20 248.26 88.671 +Duct1 0.0025 0.4495 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1029.20 248.26 88.671 +Duct2 0.0025 0.4495 365.99 +Duct3 0.0050 0.3000 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3505 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.6246 1399.72 342.84 298.488 +Duct5 0.0075 0.4511 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 13.5530 1399.72 342.84 298.488 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 633.62 151.56 23.516 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.2900 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 8002.5 33295.3 50730.8 +LP_Shaft 3751.1 86425.4 61726.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2729.99 0.9940 0.0550 4.98381 0.02223 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.588 0.9975 1.0000 0.9975 2706.36 0.841 968.5 39239.9 +Core_Nozz 1.526 0.9999 1.0000 0.9999 862.88 0.814 1446.3 11301.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 8 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 0.0 27.00 1482.35 40522.2 0.3899 15800.83 5.4430 114.51 18.467 2631.0 2565.4 2055.9 + core size:20.06 Q: 14.81 Maximum Thrust: 45024.4 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1482.35 14.799 546.76 130.69 0.0000 1511.36 14.696 545.67 25643.2 0.1000 1.39997 +FS_2 Inlet.Fl_O 1482.35 14.695 546.76 130.69 0.0000 1522.02 12.388 520.71 5943.4 0.4999 1.39997 +FS_21 Fan.Fl_O 1482.35 22.725 626.47 149.84 0.0000 1053.54 19.879 603.02 4515.2 0.4415 1.39851 +FS_13 Splitter.Fl_O2 1252.28 22.725 626.47 149.84 0.0000 890.03 19.845 602.73 3795.6 0.4444 1.39851 +FS_22 Splitter.Fl_O1 230.07 22.725 626.47 149.84 0.0000 163.52 20.050 604.50 719.5 0.4269 1.39851 +FS_23 Duct1.Fl_O 230.07 22.668 626.47 149.84 0.0000 163.93 20.000 604.50 721.3 0.4269 1.39851 +FS_24 LPC.Fl_O 230.07 49.155 804.53 192.92 0.0000 85.67 42.949 774.49 366.0 0.4444 1.39173 +FS_25 Duct2.Fl_O 230.07 49.032 804.53 192.92 0.0000 85.88 42.841 774.49 366.9 0.4444 1.39173 +FS_3 HPC.Fl_O 230.07 273.299 1363.58 333.42 0.0000 20.06 256.992 1341.61 119.9 0.3021 1.35805 +FS_36 Bld3.Fl_O 209.36 273.299 1363.58 333.42 0.0000 18.25 256.992 1341.61 109.1 0.3021 1.35805 +FS_4 Burner.Fl_O 213.75 258.267 2630.97 702.24 0.0210 27.39 256.603 2627.08 483.4 0.0999 1.29657 +FS_45 HPT.Fl_O 234.46 95.338 2055.86 531.80 0.0191 71.95 89.887 2027.19 439.1 0.3004 1.31279 +FS_48 Duct3.Fl_O 234.46 94.862 2055.86 531.80 0.0191 72.31 89.438 2027.19 441.4 0.3004 1.31279 +FS_5 LPT.Fl_O 234.46 21.344 1471.93 368.45 0.0191 271.95 19.775 1443.73 1477.4 0.3392 1.33865 +FS_7 Duct4.Fl_O 234.46 21.130 1471.93 368.45 0.0191 274.70 20.316 1457.37 2018.9 0.2428 1.33865 +FS_9 Core_Nozz.Fl_O 234.46 21.130 1471.93 368.45 0.0191 274.70 14.696 1341.79 862.9 0.7516 1.33865 +FS_15 BypBld.Fl_O 1252.28 22.725 626.47 149.84 0.0000 890.03 19.845 602.73 3795.6 0.4444 1.39851 +FS_17 Duct5.Fl_O 1252.28 22.554 626.47 149.84 0.0000 896.75 19.696 602.73 3824.3 0.4444 1.39851 +FS_19 Byp_Nozz.Fl_O 1252.28 22.554 626.47 149.84 0.0000 896.75 14.696 554.39 2706.4 0.8069 1.39851 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1522.02 1.546 0.9088 3514.424 1.1458 0.9142 -40162.1 31.36 16.39 +LPC 163.93 2.169 0.8631 3283.248 1.2842 0.8770 -14023.0 29.40 20.72 +HPC 85.88 5.574 0.8636 6333.286 1.6949 0.8908 -45734.5 21.43 21.47 +HPT 27.39 2.709 0.9146 153.779 1.2331 0.9049 45734.2 +LPT 72.31 4.444 0.9267 79.581 1.3967 0.9126 54184.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2918.16 1.380 0.9389 0.891 1.9254 0.5215 1.4369 0.9679 3943.9586 +LPC 175.83 1.358 0.8990 0.896 1.7385 0.9323 3.2631 0.9600 3662.6571 +HPC 204.17 22.144 0.8520 0.996 2.1015 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.022 0.9329 100.435 5.0222 1.4085 0.4249 0.9803 1.5311 +LPT 150.27 5.805 0.9255 98.114 5.8049 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 25643.18 5275.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1004.45 242.09 81.887 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1004.45 242.09 81.887 +Duct1 0.0025 0.4269 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1004.45 242.09 81.887 +Duct2 0.0025 0.4444 365.99 +Duct3 0.0050 0.3004 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3392 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.0524 1363.58 333.42 273.299 +Duct5 0.0075 0.4444 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.6538 1363.58 333.42 273.299 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 626.47 149.84 22.725 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.4430 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7887.8 30452.4 45734.2 +LP_Shaft 3608.3 78868.3 54184.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2630.97 0.9940 0.0550 4.38912 0.02096 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.535 0.9975 1.0000 0.9975 2706.36 0.807 928.9 36155.6 +Core_Nozz 1.438 0.9999 1.0000 0.9999 862.88 0.752 1323.2 9642.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 9 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 0.0 27.00 1408.63 36019.5 0.3837 13819.26 5.6021 114.51 16.790 2533.9 2471.3 1975.9 + core size:20.18 Q: 14.81 Maximum Thrust: 45024.4 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1408.63 14.799 546.76 130.69 0.0000 1436.20 14.696 545.67 24367.9 0.1000 1.39997 +FS_2 Inlet.Fl_O 1408.63 14.695 546.76 130.69 0.0000 1446.32 12.661 523.96 5943.4 0.4663 1.39997 +FS_21 Fan.Fl_O 1408.63 21.912 619.41 148.14 0.0000 1032.43 19.295 597.35 4515.2 0.4302 1.39868 +FS_13 Splitter.Fl_O2 1195.27 21.912 619.41 148.14 0.0000 876.05 19.237 596.84 3795.6 0.4354 1.39868 +FS_22 Splitter.Fl_O1 213.36 21.912 619.41 148.14 0.0000 156.38 19.586 599.90 719.5 0.4037 1.39868 +FS_23 Duct1.Fl_O 213.36 21.857 619.41 148.14 0.0000 156.77 19.537 599.90 721.3 0.4037 1.39868 +FS_24 LPC.Fl_O 213.36 45.404 785.36 188.25 0.0000 84.98 39.780 756.58 366.0 0.4396 1.39265 +FS_25 Duct2.Fl_O 213.36 45.291 785.36 188.25 0.0000 85.19 39.681 756.58 366.9 0.4396 1.39265 +FS_3 HPC.Fl_O 213.36 248.471 1326.57 323.82 0.0000 20.18 233.453 1304.82 119.9 0.3039 1.36027 +FS_36 Bld3.Fl_O 194.16 248.471 1326.57 323.82 0.0000 18.37 233.453 1304.82 109.1 0.3039 1.36027 +FS_4 Burner.Fl_O 198.00 234.805 2533.90 672.24 0.0198 27.39 233.293 2530.13 483.4 0.0997 1.29952 +FS_45 HPT.Fl_O 217.20 86.323 1975.91 508.27 0.0180 72.17 81.356 1947.93 439.1 0.3010 1.31632 +FS_48 Duct3.Fl_O 217.20 85.892 1975.91 508.27 0.0180 72.53 80.949 1947.93 441.4 0.3010 1.31632 +FS_5 LPT.Fl_O 217.20 20.198 1425.99 355.69 0.0180 262.03 18.830 1400.68 1477.4 0.3246 1.34194 +FS_7 Duct4.Fl_O 217.20 19.996 1425.99 355.69 0.0180 264.68 19.284 1412.85 2018.9 0.2330 1.34194 +FS_9 Core_Nozz.Fl_O 217.20 19.996 1425.99 355.69 0.0180 264.68 14.696 1317.63 862.9 0.6894 1.34194 +FS_15 BypBld.Fl_O 1195.27 21.912 619.41 148.14 0.0000 876.05 19.237 596.84 3795.6 0.4354 1.39868 +FS_17 Duct5.Fl_O 1195.27 21.747 619.41 148.14 0.0000 882.67 19.093 596.84 3824.3 0.4354 1.39868 +FS_19 Byp_Nozz.Fl_O 1195.27 21.747 619.41 148.14 0.0000 882.67 14.696 553.86 2706.4 0.7698 1.39868 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1446.32 1.491 0.9091 3363.250 1.1329 0.9141 -34780.0 34.21 16.19 +LPC 156.77 2.077 0.8602 3159.875 1.2679 0.8737 -12109.0 29.04 19.32 +HPC 85.19 5.486 0.8642 6315.355 1.6891 0.8911 -40923.2 22.66 22.69 +HPT 27.39 2.720 0.9147 154.380 1.2361 0.9047 40923.2 +LPT 72.53 4.252 0.9247 77.684 1.3856 0.9106 46888.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2773.12 1.342 0.9392 0.853 1.8749 0.5215 1.4369 0.9679 3943.9586 +LPC 168.16 1.330 0.8960 0.863 1.7146 0.9323 3.2631 0.9600 3662.6571 +HPC 202.53 21.739 0.8526 0.993 2.1184 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.048 0.9330 100.828 5.0484 1.4085 0.4249 0.9803 1.5311 +LPT 150.72 5.537 0.9235 95.774 5.5370 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 24367.89 5013.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 978.72 235.70 75.057 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 978.72 235.70 75.057 +Duct1 0.0025 0.4037 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 978.72 235.70 75.057 +Duct2 0.0025 0.4396 365.99 +Duct3 0.0050 0.3010 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3246 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.4676 1326.57 323.82 248.471 +Duct5 0.0075 0.4354 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.7348 1326.57 323.82 248.471 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 619.41 148.14 21.912 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.6021 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7771.2 27657.8 40923.2 +LP_Shaft 3453.1 71316.7 46888.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2533.90 0.9940 0.0550 3.83868 0.01977 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.480 0.9975 1.0000 0.9975 2706.36 0.770 885.8 32907.1 +Core_Nozz 1.361 0.9999 1.0000 0.9999 862.88 0.689 1203.8 8125.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 10 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 0.0 27.00 1241.50 27014.7 0.3758 10150.84 5.9294 114.51 13.477 2325.1 2268.7 1803.7 + core size:20.45 Q: 14.81 Maximum Thrust: 45024.4 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1241.50 14.799 546.76 130.69 0.0000 1265.80 14.696 545.67 21476.8 0.1000 1.39997 +FS_2 Inlet.Fl_O 1241.50 14.695 546.76 130.69 0.0000 1274.73 13.182 530.04 5943.4 0.3970 1.39997 +FS_21 Fan.Fl_O 1241.50 20.243 604.71 144.61 0.0000 973.21 18.134 586.03 4515.2 0.3996 1.39897 +FS_13 Splitter.Fl_O2 1062.34 20.243 604.71 144.61 0.0000 832.76 18.047 585.22 3795.6 0.4084 1.39897 +FS_22 Splitter.Fl_O1 179.16 20.243 604.71 144.61 0.0000 140.45 18.556 589.89 719.5 0.3548 1.39897 +FS_23 Duct1.Fl_O 179.16 20.192 604.71 144.61 0.0000 140.80 18.510 589.89 721.3 0.3548 1.39897 +FS_24 LPC.Fl_O 179.16 37.673 741.99 177.73 0.0000 83.59 33.184 715.81 366.0 0.4302 1.39458 +FS_25 Duct2.Fl_O 179.16 37.579 741.99 177.73 0.0000 83.80 33.101 715.81 366.9 0.4302 1.39458 +FS_3 HPC.Fl_O 179.16 199.453 1245.15 302.85 0.0000 20.45 187.048 1223.91 119.9 0.3079 1.36531 +FS_36 Bld3.Fl_O 163.04 199.453 1245.15 302.85 0.0000 18.61 187.048 1223.91 109.1 0.3079 1.36531 +FS_4 Burner.Fl_O 165.86 188.483 2325.08 608.73 0.0173 27.38 187.270 2321.56 483.4 0.0995 1.30622 +FS_45 HPT.Fl_O 181.98 68.577 1803.65 458.44 0.0157 72.73 64.567 1777.18 439.1 0.3026 1.32471 +FS_48 Duct3.Fl_O 181.98 68.234 1803.65 458.44 0.0157 73.09 64.244 1777.18 441.4 0.3026 1.32471 +FS_5 LPT.Fl_O 181.98 18.313 1335.75 330.89 0.0157 234.36 17.338 1316.96 1477.4 0.2857 1.34880 +FS_7 Duct4.Fl_O 181.98 18.130 1335.75 330.89 0.0157 236.73 17.618 1325.88 2018.9 0.2065 1.34880 +FS_9 Core_Nozz.Fl_O 181.98 18.130 1335.75 330.89 0.0157 236.73 14.696 1264.78 862.9 0.5649 1.34880 +FS_15 BypBld.Fl_O 1062.34 20.243 604.71 144.61 0.0000 832.76 18.047 585.22 3795.6 0.4084 1.39897 +FS_17 Duct5.Fl_O 1062.34 20.091 604.71 144.61 0.0000 839.06 17.912 585.22 3824.3 0.4084 1.39897 +FS_19 Byp_Nozz.Fl_O 1062.34 20.091 604.71 144.61 0.0000 839.06 14.696 553.06 2706.4 0.6837 1.39897 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1274.73 1.377 0.9035 3008.607 1.1060 0.9078 -24445.6 36.61 15.22 +LPC 140.80 1.866 0.8543 2860.827 1.2270 0.8664 -8395.8 29.47 16.88 +HPC 83.80 5.308 0.8645 6283.526 1.6781 0.8909 -31717.1 25.32 25.44 +HPT 27.38 2.749 0.9150 155.861 1.2438 0.9050 31717.1 +LPT 73.09 3.726 0.9203 72.735 1.3503 0.9069 32841.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2444.12 1.263 0.9334 0.763 1.7977 0.5215 1.4369 0.9679 3943.9586 +LPC 151.03 1.265 0.8898 0.781 1.6945 0.9323 3.2631 0.9600 3662.6571 +HPC 199.23 20.913 0.8529 0.988 2.1543 0.4206 0.2163 1.0137 6357.1603 +HPT 30.12 5.115 0.9333 101.796 5.1153 1.4085 0.4249 0.9803 1.5311 +LPT 151.88 4.803 0.9191 89.673 4.8026 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 21476.83 4418.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 921.34 221.52 61.293 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 921.34 221.52 61.293 +Duct1 0.0025 0.3548 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 921.34 221.52 61.293 +Duct2 0.0025 0.4302 365.99 +Duct3 0.0050 0.3026 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2857 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.2707 1245.15 302.85 199.453 +Duct5 0.0075 0.4084 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.8540 1245.15 302.85 199.453 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 604.71 144.61 20.243 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9294 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7515.5 22165.2 31717.1 +LP_Shaft 3089.0 55838.5 32841.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2325.08 0.9940 0.0550 2.81968 0.01729 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.367 0.9975 1.0000 0.9975 2706.36 0.684 786.2 25957.5 +Core_Nozz 1.234 0.9999 1.0000 0.9999 862.88 0.565 968.2 5475.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 11 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 8/ 28/ 2/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 0.0 27.00 1038.80 18009.7 0.3770 6789.85 6.2368 114.51 10.174 2073.4 2024.5 1598.4 + core size:20.83 Q: 14.81 Maximum Thrust: 45024.4 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1038.80 14.799 546.76 130.69 0.0000 1059.13 14.696 545.67 17970.3 0.1000 1.39997 +FS_2 Inlet.Fl_O 1038.80 14.695 546.76 130.69 0.0000 1066.60 13.677 535.66 5943.4 0.3219 1.39997 +FS_21 Fan.Fl_O 1038.80 18.532 588.42 140.69 0.0000 877.40 17.004 574.14 4515.2 0.3529 1.39922 +FS_13 Splitter.Fl_O2 895.26 18.532 588.42 140.69 0.0000 756.16 16.917 573.30 3795.6 0.3634 1.39922 +FS_22 Splitter.Fl_O1 143.54 18.532 588.42 140.69 0.0000 121.24 17.412 578.04 719.5 0.2999 1.39922 +FS_23 Duct1.Fl_O 143.54 18.486 588.42 140.69 0.0000 121.54 17.368 578.04 721.3 0.2999 1.39922 +FS_24 LPC.Fl_O 143.54 30.025 691.42 165.49 0.0000 81.12 26.690 668.68 366.0 0.4140 1.39630 +FS_25 Duct2.Fl_O 143.54 29.950 691.42 165.49 0.0000 81.32 26.623 668.68 366.9 0.4140 1.39630 +FS_3 HPC.Fl_O 143.54 150.563 1145.94 277.59 0.0000 20.83 140.830 1125.35 119.9 0.3134 1.37155 +FS_36 Bld3.Fl_O 130.62 150.563 1145.94 277.59 0.0000 18.95 140.830 1125.35 109.1 0.3134 1.37155 +FS_4 Burner.Fl_O 132.51 142.282 2073.40 534.04 0.0144 27.36 141.368 2070.19 483.4 0.0991 1.31537 +FS_45 HPT.Fl_O 145.43 51.249 1598.38 400.62 0.0131 73.21 48.211 1573.98 439.1 0.3034 1.33601 +FS_48 Duct3.Fl_O 145.43 50.992 1598.38 400.62 0.0131 73.58 47.970 1573.98 441.4 0.3034 1.33601 +FS_5 LPT.Fl_O 145.43 16.882 1238.79 304.68 0.0131 195.65 16.267 1226.77 1477.4 0.2342 1.35658 +FS_7 Duct4.Fl_O 145.43 16.713 1238.79 304.68 0.0131 197.63 16.387 1232.39 2018.9 0.1706 1.35658 +FS_9 Core_Nozz.Fl_O 145.43 16.713 1238.79 304.68 0.0131 197.63 14.696 1197.56 862.8 0.4384 1.35658 +FS_15 BypBld.Fl_O 895.26 18.532 588.42 140.69 0.0000 756.16 16.917 573.30 3795.6 0.3634 1.39922 +FS_17 Duct5.Fl_O 895.26 18.393 588.42 140.69 0.0000 761.87 16.790 573.30 3824.3 0.3634 1.39922 +FS_19 Byp_Nozz.Fl_O 895.26 18.393 588.42 140.69 0.0000 761.87 14.696 551.89 2706.4 0.5755 1.39922 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1066.60 1.261 0.8991 2566.573 1.0762 0.9024 -14701.4 35.54 12.86 +LPC 121.54 1.624 0.8459 2474.051 1.1751 0.8561 -5037.3 32.99 14.37 +HPC 81.32 5.027 0.8642 6235.778 1.6574 0.8903 -22765.3 29.42 29.61 +HPT 27.36 2.776 0.9155 158.116 1.2534 0.9051 22765.2 +LPT 73.58 3.021 0.9093 65.912 1.2903 0.8964 19740.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2045.06 1.182 0.9288 0.651 1.7286 0.5215 1.4369 0.9679 3943.9586 +LPC 130.37 1.191 0.8811 0.675 1.7140 0.9323 3.2631 0.9600 3662.6571 +HPC 193.33 19.617 0.8526 0.981 2.1861 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.181 0.9338 103.268 5.1807 1.4085 0.4249 0.9803 1.5311 +LPT 152.89 3.819 0.9081 81.262 3.8187 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 17970.26 3697.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 852.91 204.73 47.620 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 852.91 204.73 47.620 +Duct1 0.0025 0.2999 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 852.91 204.73 47.620 +Duct2 0.0025 0.4140 365.99 +Duct3 0.0050 0.3034 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2342 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.0240 1145.94 277.59 150.563 +Duct5 0.0075 0.3634 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.8949 1145.94 277.59 150.563 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 588.42 140.69 18.532 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.2368 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7199.7 16606.9 22765.2 +LP_Shaft 2635.2 39343.7 19740.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2073.40 0.9940 0.0550 1.88607 0.01444 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.252 0.9975 1.0000 0.9975 2706.36 0.576 661.1 18395.4 +Core_Nozz 1.137 0.9999 1.0000 0.9999 862.88 0.438 732.7 3311.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 12 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 0.0 27.00 770.74 9004.4 0.4096 3687.88 6.3532 114.51 6.772 1731.3 1692.9 1323.5 + core size:21.48 Q: 14.81 Maximum Thrust: 45024.4 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 770.74 14.799 546.76 130.69 0.0000 785.83 14.696 545.67 13333.1 0.1000 1.39997 +FS_2 Inlet.Fl_O 770.74 14.695 546.76 130.69 0.0000 791.37 14.155 540.94 5943.4 0.2319 1.39997 +FS_21 Fan.Fl_O 770.74 16.788 570.40 136.36 0.0000 707.53 15.919 561.81 4515.2 0.2766 1.39952 +FS_13 Splitter.Fl_O2 665.92 16.788 570.40 136.36 0.0000 611.31 15.867 561.28 3795.6 0.2851 1.39952 +FS_22 Splitter.Fl_O1 104.82 16.788 570.40 136.36 0.0000 96.22 16.166 564.28 719.5 0.2330 1.39952 +FS_23 Duct1.Fl_O 104.82 16.746 570.40 136.36 0.0000 96.46 16.125 564.28 721.3 0.2330 1.39952 +FS_24 LPC.Fl_O 104.82 22.244 628.38 150.30 0.0000 76.22 20.102 610.50 366.0 0.3833 1.39847 +FS_25 Duct2.Fl_O 104.82 22.189 628.38 150.30 0.0000 76.41 20.052 610.50 366.9 0.3833 1.39847 +FS_3 HPC.Fl_O 104.82 100.213 1012.98 244.21 0.0000 21.48 93.287 993.18 119.9 0.3236 1.37990 +FS_36 Bld3.Fl_O 95.38 100.213 1012.98 244.21 0.0000 19.55 93.287 993.18 109.1 0.3236 1.37990 +FS_4 Burner.Fl_O 96.41 94.701 1731.33 436.02 0.0107 27.33 94.094 1728.56 483.4 0.0983 1.33134 +FS_45 HPT.Fl_O 105.84 33.783 1323.51 325.91 0.0098 73.55 31.763 1302.33 439.1 0.3029 1.35357 +FS_48 Duct3.Fl_O 105.84 33.614 1323.51 325.91 0.0098 73.92 31.604 1302.33 441.4 0.3029 1.35357 +FS_5 LPT.Fl_O 105.84 15.801 1110.55 270.79 0.0098 144.04 15.495 1104.74 1477.4 0.1692 1.36702 +FS_7 Duct4.Fl_O 105.84 15.643 1110.55 270.79 0.0098 145.50 15.479 1107.42 2018.9 0.1241 1.36702 +FS_9 Core_Nozz.Fl_O 105.84 15.643 1110.55 270.79 0.0098 145.50 14.696 1092.04 863.0 0.3036 1.36702 +FS_15 BypBld.Fl_O 665.92 16.788 570.40 136.36 0.0000 611.31 15.867 561.28 3795.6 0.2851 1.39952 +FS_17 Duct5.Fl_O 665.92 16.662 570.40 136.36 0.0000 615.93 15.748 561.28 3824.3 0.2851 1.39952 +FS_19 Byp_Nozz.Fl_O 665.92 16.662 570.40 136.36 0.0000 615.93 14.696 550.30 2706.4 0.4275 1.39952 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 791.37 1.142 0.8966 1937.446 1.0432 0.8987 -6188.3 38.28 8.12 +LPC 96.46 1.328 0.8299 1896.871 1.1016 0.8366 -2066.6 45.03 12.62 +HPC 76.41 4.516 0.8622 6147.515 1.6120 0.8875 -13927.7 37.51 37.98 +HPT 27.33 2.803 0.9165 162.621 1.2677 0.9057 13928.3 +LPT 73.92 2.127 0.8880 54.679 1.1918 0.8777 8254.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1517.34 1.099 0.9263 0.491 1.6835 0.5215 1.4369 0.9679 3943.9586 +LPC 103.47 1.101 0.8644 0.518 1.8646 0.9323 3.2631 0.9600 3662.6571 +HPC 181.66 17.255 0.8506 0.967 2.2450 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.244 0.9349 106.211 5.2440 1.4085 0.4249 0.9803 1.5311 +LPT 153.59 2.573 0.8869 67.412 2.5726 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 13333.09 2743.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 764.43 183.17 33.619 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 764.43 183.17 33.619 +Duct1 0.0025 0.2330 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 764.43 183.17 33.619 +Duct2 0.0025 0.3833 365.99 +Duct3 0.0050 0.3029 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1692 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.6686 1012.98 244.21 100.213 +Duct5 0.0075 0.2851 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.7649 1012.98 244.21 100.213 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 570.40 136.36 16.788 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.3532 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6766.5 10811.0 13928.3 +LP_Shaft 1989.2 21794.4 8254.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1731.33 0.9940 0.0550 1.02441 0.01074 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.134 0.9975 1.0000 0.9975 2706.36 0.427 490.3 10148.5 +Core_Nozz 1.064 0.9999 1.0000 0.9999 862.88 0.304 486.1 1599.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 13 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 0.0 27.00 1578.09 41056.7 0.4410 18104.69 5.3318 229.02 19.979 2730.0 2661.6 2137.8 + core size:19.95 Q: 59.25 Maximum Thrust: 41056.7 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1578.09 15.111 550.04 131.47 0.0000 1580.43 14.696 545.67 13649.8 0.2000 1.39991 +FS_2 Inlet.Fl_O 1578.09 15.021 550.03 131.47 0.0000 1589.98 12.385 520.52 5943.4 0.5322 1.39991 +FS_21 Fan.Fl_O 1578.09 23.914 636.38 152.22 0.0000 1074.22 20.777 611.39 4515.2 0.4529 1.39825 +FS_13 Splitter.Fl_O2 1328.86 23.914 636.38 152.22 0.0000 904.56 20.765 611.28 3795.6 0.4539 1.39825 +FS_22 Splitter.Fl_O1 249.23 23.914 636.38 152.22 0.0000 169.66 20.844 611.95 719.5 0.4476 1.39825 +FS_23 Duct1.Fl_O 249.23 23.854 636.38 152.22 0.0000 170.08 20.792 611.95 721.3 0.4476 1.39825 +FS_24 LPC.Fl_O 249.23 53.666 826.17 198.19 0.0000 86.14 46.800 794.96 366.0 0.4478 1.39070 +FS_25 Duct2.Fl_O 249.23 53.532 826.17 198.19 0.0000 86.35 46.683 794.96 366.9 0.4478 1.39070 +FS_3 HPC.Fl_O 249.23 301.904 1403.01 343.69 0.0000 19.95 284.092 1380.77 119.9 0.3006 1.35572 +FS_36 Bld3.Fl_O 226.80 301.904 1403.01 343.69 0.0000 18.16 284.092 1380.77 109.1 0.3006 1.35572 +FS_4 Burner.Fl_O 231.83 285.299 2730.00 733.11 0.0222 27.40 283.461 2725.99 483.4 0.1000 1.29383 +FS_45 HPT.Fl_O 254.26 105.705 2137.78 556.13 0.0202 71.77 99.693 2108.37 439.1 0.3000 1.30943 +FS_48 Duct3.Fl_O 254.26 105.176 2137.78 556.13 0.0202 72.13 99.195 2108.37 441.4 0.3000 1.30943 +FS_5 LPT.Fl_O 254.26 22.831 1521.38 382.29 0.0202 280.30 21.037 1490.38 1477.4 0.3517 1.33527 +FS_7 Duct4.Fl_O 254.26 22.603 1521.38 382.29 0.0202 283.13 21.675 1505.44 2018.9 0.2511 1.33527 +FS_9 Core_Nozz.Fl_O 254.26 22.603 1521.38 382.29 0.0202 283.13 14.696 1364.15 862.9 0.8225 1.33527 +FS_15 BypBld.Fl_O 1328.86 23.914 636.38 152.22 0.0000 904.56 20.765 611.28 3795.6 0.4539 1.39825 +FS_17 Duct5.Fl_O 1328.86 23.735 636.38 152.22 0.0000 911.40 20.609 611.28 3824.3 0.4539 1.39825 +FS_19 Byp_Nozz.Fl_O 1328.86 23.735 636.38 152.22 0.0000 911.40 14.696 555.04 2706.4 0.8567 1.39825 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1589.98 1.592 0.9038 3644.232 1.1570 0.9099 -46329.2 28.91 16.74 +LPC 170.08 2.250 0.8653 3387.990 1.2982 0.8796 -16210.4 29.61 21.97 +HPC 86.35 5.640 0.8631 6346.698 1.6982 0.8904 -51307.4 20.47 20.47 +HPT 27.40 2.699 0.9145 153.305 1.2300 0.9050 51307.5 +LPT 72.13 4.607 0.9286 81.166 1.4052 0.9147 62539.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3048.57 1.412 0.9338 0.924 2.0260 0.5215 1.4369 0.9679 3943.9586 +LPC 182.43 1.383 0.9013 0.925 1.7581 0.9323 3.2631 0.9600 3662.6571 +HPC 205.30 22.448 0.8515 0.998 2.0845 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 4.999 0.9328 100.126 4.9988 1.4085 0.4249 0.9803 1.5311 +LPT 149.87 6.031 0.9274 100.068 6.0312 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 13649.76 11233.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1032.65 249.12 89.918 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1032.65 249.12 89.918 +Duct1 0.0025 0.4476 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1032.65 249.12 89.918 +Duct2 0.0025 0.4478 365.99 +Duct3 0.0050 0.3000 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3517 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.7232 1403.01 343.69 301.904 +Duct5 0.0075 0.4539 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 13.7079 1403.01 343.69 301.904 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 636.38 152.22 23.914 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3318 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 8010.1 33641.7 51307.5 +LP_Shaft 3752.8 87525.3 62539.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.00 0.9940 0.0550 5.02908 0.02217 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.615 0.9975 1.0000 0.9975 2706.36 0.857 986.9 40761.0 +Core_Nozz 1.538 0.9999 1.0000 0.9999 862.88 0.822 1458.9 11529.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 14 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 4/ 14/ 1/ 2 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 0.0 27.00 1514.56 36951.1 0.4339 16032.26 5.4859 229.02 18.369 2634.8 2569.3 2059.2 + core size:20.08 Q: 59.25 Maximum Thrust: 41056.7 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1514.56 15.111 550.04 131.47 0.0000 1516.81 14.696 545.67 13100.3 0.2000 1.39991 +FS_2 Inlet.Fl_O 1514.56 15.021 550.03 131.47 0.0000 1525.97 12.647 523.65 5943.4 0.5017 1.39991 +FS_21 Fan.Fl_O 1514.56 23.150 629.52 150.57 0.0000 1059.25 20.213 605.64 4515.2 0.4446 1.39844 +FS_13 Splitter.Fl_O2 1281.05 23.150 629.52 150.57 0.0000 895.93 20.170 605.27 3795.6 0.4482 1.39844 +FS_22 Splitter.Fl_O1 233.52 23.150 629.52 150.57 0.0000 163.32 20.433 607.51 719.5 0.4262 1.39844 +FS_23 Duct1.Fl_O 233.52 23.092 629.52 150.57 0.0000 163.72 20.382 607.51 721.3 0.4262 1.39844 +FS_24 LPC.Fl_O 233.52 50.186 809.04 194.02 0.0000 85.40 43.896 779.08 366.0 0.4427 1.39151 +FS_25 Duct2.Fl_O 233.52 50.061 809.04 194.02 0.0000 85.62 43.786 779.08 366.9 0.4427 1.39151 +FS_3 HPC.Fl_O 233.52 277.585 1368.46 334.69 0.0000 20.08 260.984 1346.38 119.9 0.3025 1.35775 +FS_36 Bld3.Fl_O 212.50 277.585 1368.46 334.69 0.0000 18.27 260.984 1346.38 109.1 0.3025 1.35775 +FS_4 Burner.Fl_O 216.95 262.318 2634.75 703.36 0.0210 27.39 260.628 2630.86 483.4 0.0999 1.29650 +FS_45 HPT.Fl_O 237.97 96.862 2059.22 532.76 0.0191 71.94 91.326 2030.52 439.1 0.3004 1.31268 +FS_48 Duct3.Fl_O 237.97 96.378 2059.22 532.76 0.0191 72.30 90.870 2030.52 441.4 0.3004 1.31268 +FS_5 LPT.Fl_O 237.97 21.551 1472.41 368.58 0.0191 273.42 19.948 1443.85 1477.4 0.3413 1.33862 +FS_7 Duct4.Fl_O 237.97 21.335 1472.41 368.58 0.0191 276.18 20.504 1457.67 2018.9 0.2442 1.33862 +FS_9 Core_Nozz.Fl_O 237.97 21.335 1472.41 368.58 0.0191 276.18 14.696 1338.91 862.9 0.7619 1.33862 +FS_15 BypBld.Fl_O 1281.05 23.150 629.52 150.57 0.0000 895.93 20.170 605.27 3795.6 0.4482 1.39844 +FS_17 Duct5.Fl_O 1281.05 22.976 629.52 150.57 0.0000 902.70 20.019 605.27 3824.3 0.4482 1.39844 +FS_19 Byp_Nozz.Fl_O 1281.05 22.976 629.52 150.57 0.0000 902.70 14.696 554.15 2706.3 0.8252 1.39844 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1525.97 1.541 0.9092 3513.342 1.1445 0.9145 -40924.3 32.09 16.88 +LPC 163.72 2.173 0.8627 3284.063 1.2852 0.8768 -14353.5 29.08 20.48 +HPC 85.62 5.545 0.8640 6326.165 1.6915 0.8910 -46476.5 21.77 21.83 +HPT 27.39 2.708 0.9146 153.925 1.2329 0.9049 46478.2 +LPT 72.30 4.472 0.9267 79.729 1.3985 0.9125 55277.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2925.71 1.377 0.9393 0.891 1.9506 0.5215 1.4369 0.9679 3943.9586 +LPC 175.61 1.360 0.8986 0.897 1.7307 0.9323 3.2631 0.9600 3662.6571 +HPC 203.53 22.010 0.8523 0.995 2.1034 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.020 0.9329 100.531 5.0203 1.4085 0.4249 0.9803 1.5311 +LPT 150.23 5.844 0.9255 98.296 5.8436 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 13100.26 10781.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1009.11 243.25 83.393 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1009.11 243.25 83.393 +Duct1 0.0025 0.4262 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1009.11 243.25 83.393 +Duct2 0.0025 0.4427 365.99 +Duct3 0.0050 0.3004 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3413 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.1731 1368.46 334.69 277.585 +Duct5 0.0075 0.4482 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.8434 1368.46 334.69 277.585 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 629.52 150.57 23.150 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.4859 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7900.9 30896.1 46478.2 +LP_Shaft 3618.0 80243.9 55277.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2634.75 0.9940 0.0550 4.45340 0.02096 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.563 0.9975 1.0000 0.9975 2706.36 0.825 949.9 37820.5 +Core_Nozz 1.452 0.9999 1.0000 0.9999 862.88 0.762 1340.1 9911.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 15 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 0.0 27.00 1445.33 32845.4 0.4292 14097.34 5.6500 229.02 16.774 2540.9 2478.2 1981.9 + core size:20.20 Q: 59.25 Maximum Thrust: 41056.7 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1445.33 15.111 550.04 131.47 0.0000 1447.47 14.696 545.67 12501.4 0.2000 1.39991 +FS_2 Inlet.Fl_O 1445.33 15.021 550.03 131.47 0.0000 1456.22 12.906 526.70 5943.4 0.4706 1.39991 +FS_21 Fan.Fl_O 1445.33 22.362 622.69 148.93 0.0000 1040.76 19.641 600.07 4515.2 0.4347 1.39861 +FS_13 Splitter.Fl_O2 1227.99 22.362 622.69 148.93 0.0000 884.26 19.572 599.47 3795.6 0.4406 1.39861 +FS_22 Splitter.Fl_O1 217.34 22.362 622.69 148.93 0.0000 156.51 19.984 603.04 719.5 0.4041 1.39861 +FS_23 Duct1.Fl_O 217.34 22.306 622.69 148.93 0.0000 156.90 19.934 603.04 721.3 0.4041 1.39861 +FS_24 LPC.Fl_O 217.34 46.562 790.75 189.56 0.0000 84.70 40.839 762.02 366.0 0.4378 1.39239 +FS_25 Duct2.Fl_O 217.34 46.446 790.75 189.56 0.0000 84.91 40.737 762.02 366.9 0.4378 1.39239 +FS_3 HPC.Fl_O 217.34 253.478 1332.94 325.47 0.0000 20.20 238.125 1311.05 119.9 0.3042 1.35989 +FS_36 Bld3.Fl_O 197.78 253.478 1332.94 325.47 0.0000 18.38 238.125 1311.05 109.1 0.3042 1.35989 +FS_4 Burner.Fl_O 201.70 239.536 2540.89 674.34 0.0198 27.39 237.994 2537.11 483.4 0.0997 1.29935 +FS_45 HPT.Fl_O 221.26 88.110 1981.94 510.00 0.0180 72.14 83.045 1953.92 439.1 0.3009 1.31608 +FS_48 Duct3.Fl_O 221.26 87.669 1981.94 510.00 0.0180 72.50 82.629 1953.92 441.4 0.3009 1.31608 +FS_5 LPT.Fl_O 221.26 20.414 1427.38 356.07 0.0180 264.24 19.005 1401.58 1477.4 0.3277 1.34184 +FS_7 Duct4.Fl_O 221.26 20.210 1427.38 356.07 0.0180 266.91 19.477 1414.00 2018.9 0.2351 1.34184 +FS_9 Core_Nozz.Fl_O 221.26 20.210 1427.38 356.07 0.0180 266.91 14.696 1315.33 862.9 0.7017 1.34184 +FS_15 BypBld.Fl_O 1227.99 22.362 622.69 148.93 0.0000 884.26 19.572 599.47 3795.6 0.4406 1.39861 +FS_17 Duct5.Fl_O 1227.99 22.194 622.69 148.93 0.0000 890.94 19.425 599.47 3824.3 0.4406 1.39861 +FS_19 Byp_Nozz.Fl_O 1227.99 22.194 622.69 148.93 0.0000 890.94 14.696 553.57 2706.4 0.7906 1.39861 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1456.22 1.489 0.9105 3370.260 1.1321 0.9154 -35693.1 35.01 16.80 +LPC 156.90 2.087 0.8599 3167.551 1.2699 0.8735 -12495.7 28.67 19.11 +HPC 84.91 5.458 0.8645 6308.682 1.6857 0.8913 -41790.8 22.99 23.08 +HPT 27.39 2.719 0.9147 154.532 1.2359 0.9048 41790.8 +LPT 72.50 4.295 0.9247 77.959 1.3885 0.9106 48188.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2792.10 1.340 0.9407 0.855 1.9050 0.5215 1.4369 0.9679 3943.9586 +LPC 168.29 1.333 0.8957 0.865 1.7064 0.9323 3.2631 0.9600 3662.6571 +HPC 201.87 21.606 0.8529 0.992 2.1197 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.045 0.9330 100.928 5.0449 1.4085 0.4249 0.9803 1.5311 +LPT 150.65 5.596 0.9235 96.114 5.5958 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 12501.44 10288.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 984.48 237.13 76.776 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 984.48 237.13 76.776 +Duct1 0.0025 0.4041 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 984.48 237.13 76.776 +Duct2 0.0025 0.4378 365.99 +Duct3 0.0050 0.3009 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3277 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.6070 1332.94 325.47 253.478 +Duct5 0.0075 0.4406 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.9539 1332.94 325.47 253.478 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 622.69 148.93 22.362 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.6500 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7789.6 28177.5 41790.8 +LP_Shaft 3470.7 72923.3 48188.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2540.89 0.9940 0.0550 3.91593 0.01980 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.510 0.9975 1.0000 0.9975 2706.36 0.791 909.6 34715.8 +Core_Nozz 1.375 0.9999 1.0000 0.9999 862.88 0.702 1224.1 8417.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 16 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 0.0 27.00 1288.42 24633.6 0.4255 10481.75 6.0026 229.02 13.596 2338.6 2281.9 1815.1 + core size:20.47 Q: 59.25 Maximum Thrust: 41056.7 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1288.42 15.111 550.04 131.47 0.0000 1290.33 14.696 545.67 11144.2 0.2000 1.39991 +FS_2 Inlet.Fl_O 1288.42 15.021 550.03 131.47 0.0000 1298.12 13.408 532.47 5943.4 0.4060 1.39991 +FS_21 Fan.Fl_O 1288.42 20.732 608.41 145.50 0.0000 989.18 18.490 588.88 4515.2 0.4077 1.39891 +FS_13 Splitter.Fl_O2 1104.43 20.732 608.41 145.50 0.0000 847.92 18.387 587.94 3795.6 0.4177 1.39891 +FS_22 Splitter.Fl_O1 183.99 20.732 608.41 145.50 0.0000 141.26 18.982 593.30 719.5 0.3572 1.39891 +FS_23 Duct1.Fl_O 183.99 20.680 608.41 145.50 0.0000 141.61 18.935 593.30 721.3 0.3572 1.39891 +FS_24 LPC.Fl_O 183.99 39.021 749.26 179.49 0.0000 83.28 34.412 723.07 366.0 0.4283 1.39429 +FS_25 Duct2.Fl_O 183.99 38.924 749.26 179.49 0.0000 83.49 34.326 723.07 366.9 0.4283 1.39429 +FS_3 HPC.Fl_O 183.99 205.450 1254.53 305.25 0.0000 20.47 192.652 1233.12 119.9 0.3082 1.36472 +FS_36 Bld3.Fl_O 167.43 205.450 1254.53 305.25 0.0000 18.63 192.652 1233.12 109.1 0.3082 1.36472 +FS_4 Burner.Fl_O 170.34 194.151 2338.57 612.74 0.0174 27.38 192.901 2335.04 483.4 0.0995 1.30579 +FS_45 HPT.Fl_O 186.90 70.710 1815.13 461.69 0.0158 72.67 66.582 1788.57 439.1 0.3024 1.32416 +FS_48 Duct3.Fl_O 186.90 70.356 1815.13 461.69 0.0158 73.03 66.249 1788.57 441.4 0.3024 1.32416 +FS_5 LPT.Fl_O 186.90 18.515 1338.23 331.58 0.0158 238.30 17.493 1318.72 1477.4 0.2911 1.34859 +FS_7 Duct4.Fl_O 186.90 18.329 1338.23 331.58 0.0158 240.71 17.793 1328.00 2018.9 0.2102 1.34859 +FS_9 Core_Nozz.Fl_O 186.90 18.329 1338.23 331.58 0.0158 240.71 14.696 1263.55 863.0 0.5799 1.34859 +FS_15 BypBld.Fl_O 1104.43 20.732 608.41 145.50 0.0000 847.92 18.387 587.94 3795.6 0.4177 1.39891 +FS_17 Duct5.Fl_O 1104.43 20.576 608.41 145.50 0.0000 854.33 18.249 587.94 3824.3 0.4177 1.39891 +FS_19 Byp_Nozz.Fl_O 1104.43 20.576 608.41 145.50 0.0000 854.33 14.696 552.67 2706.4 0.7105 1.39891 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1298.12 1.380 0.9079 3034.072 1.1061 0.9120 -25560.2 38.11 16.13 +LPC 141.61 1.887 0.8541 2884.845 1.2315 0.8663 -8848.8 28.81 16.69 +HPC 83.49 5.278 0.8647 6277.090 1.6744 0.8910 -32739.8 25.65 25.78 +HPT 27.38 2.746 0.9150 156.010 1.2432 0.9050 32739.8 +LPT 73.03 3.800 0.9211 73.337 1.3564 0.9076 34408.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2488.97 1.265 0.9380 0.769 1.8409 0.5215 1.4369 0.9679 3943.9586 +LPC 151.90 1.272 0.8896 0.788 1.6822 0.9323 3.2631 0.9600 3662.6571 +HPC 198.49 20.778 0.8531 0.987 2.1537 0.4206 0.2163 1.0137 6357.1603 +HPT 30.12 5.109 0.9334 101.893 5.1088 1.4085 0.4249 0.9803 1.5311 +LPT 151.76 4.906 0.9199 90.415 4.9059 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 11144.21 9171.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 929.40 223.51 63.320 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 929.40 223.51 63.320 +Duct1 0.0025 0.3572 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 929.40 223.51 63.320 +Duct2 0.0025 0.4283 365.99 +Duct3 0.0050 0.3024 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2911 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.4397 1254.53 305.25 205.450 +Duct5 0.0075 0.4177 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.1196 1254.53 305.25 205.450 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 608.41 145.50 20.732 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.0026 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7544.5 22792.0 32739.8 +LP_Shaft 3124.5 57839.7 34408.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2338.57 0.9940 0.0550 2.91160 0.01739 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.400 0.9975 1.0000 0.9975 2706.36 0.711 816.7 28035.2 +Core_Nozz 1.247 0.9999 1.0000 0.9999 862.88 0.580 993.3 5769.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 17 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 8/ 18/ 1/ 6 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 0.0 27.00 1098.12 16422.7 0.4355 7151.67 6.3723 229.02 10.402 2098.0 2048.6 1618.8 + core size:20.82 Q: 59.25 Maximum Thrust: 41056.7 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1098.12 15.111 550.04 131.47 0.0000 1099.75 14.696 545.67 9498.2 0.2000 1.39991 +FS_2 Inlet.Fl_O 1098.12 15.021 550.03 131.47 0.0000 1106.39 13.893 537.91 5943.4 0.3357 1.39991 +FS_21 Fan.Fl_O 1098.12 19.034 592.54 141.68 0.0000 906.21 17.347 577.05 4515.2 0.3666 1.39916 +FS_13 Splitter.Fl_O2 949.17 19.034 592.54 141.68 0.0000 783.29 17.238 576.01 3795.6 0.3790 1.39916 +FS_22 Splitter.Fl_O1 148.95 19.034 592.54 141.68 0.0000 122.92 17.849 581.76 719.5 0.3045 1.39916 +FS_23 Duct1.Fl_O 148.95 18.986 592.54 141.68 0.0000 123.23 17.804 581.76 721.3 0.3045 1.39916 +FS_24 LPC.Fl_O 148.95 31.417 700.44 167.67 0.0000 80.97 27.942 677.52 366.0 0.4131 1.39599 +FS_25 Duct2.Fl_O 148.95 31.338 700.44 167.67 0.0000 81.17 27.872 677.52 366.9 0.4131 1.39599 +FS_3 HPC.Fl_O 148.95 157.195 1159.42 281.00 0.0000 20.82 147.039 1138.64 119.9 0.3134 1.37070 +FS_36 Bld3.Fl_O 135.55 157.195 1159.42 281.00 0.0000 18.95 147.039 1138.64 109.1 0.3134 1.37070 +FS_4 Burner.Fl_O 137.53 148.549 2097.97 541.21 0.0147 27.36 147.594 2094.74 483.4 0.0991 1.31442 +FS_45 HPT.Fl_O 150.94 53.585 1618.76 406.26 0.0133 73.13 50.416 1594.16 439.1 0.3032 1.33487 +FS_48 Duct3.Fl_O 150.94 53.317 1618.76 406.26 0.0133 73.50 50.163 1594.16 441.4 0.3032 1.33487 +FS_5 LPT.Fl_O 150.94 17.052 1245.01 306.36 0.0133 201.54 16.392 1232.16 1477.4 0.2418 1.35605 +FS_7 Duct4.Fl_O 150.94 16.881 1245.01 306.36 0.0133 203.58 16.532 1238.18 2018.9 0.1759 1.35605 +FS_9 Core_Nozz.Fl_O 150.94 16.881 1245.01 306.36 0.0133 203.58 14.696 1200.44 862.9 0.4555 1.35605 +FS_15 BypBld.Fl_O 949.17 19.034 592.54 141.68 0.0000 783.29 17.238 576.01 3795.6 0.3790 1.39916 +FS_17 Duct5.Fl_O 949.17 18.891 592.54 141.68 0.0000 789.21 17.109 576.01 3824.3 0.3790 1.39916 +FS_19 Byp_Nozz.Fl_O 949.17 18.891 592.54 141.68 0.0000 789.21 14.696 551.53 2706.4 0.6100 1.39916 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1106.39 1.267 0.9054 2614.692 1.0773 0.9086 -15857.1 38.23 14.40 +LPC 123.23 1.655 0.8463 2519.174 1.1821 0.8569 -5477.9 31.80 14.29 +HPC 81.17 5.016 0.8643 6233.202 1.6553 0.8903 -23883.3 29.51 29.70 +HPT 27.36 2.772 0.9155 158.144 1.2523 0.9050 23883.3 +LPT 73.50 3.127 0.9101 66.923 1.3002 0.8969 21334.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2121.35 1.186 0.9354 0.663 1.7951 0.5215 1.4369 0.9679 3943.9586 +LPC 132.18 1.201 0.8815 0.688 1.6952 0.9323 3.2631 0.9600 3662.6571 +HPC 192.98 19.566 0.8526 0.981 2.1837 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.171 0.9338 103.286 5.1712 1.4085 0.4249 0.9803 1.5311 +LPT 152.72 3.967 0.9090 82.508 3.9667 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 9498.22 7816.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 863.58 207.34 49.776 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 863.58 207.34 49.776 +Duct1 0.0025 0.3045 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 863.58 207.34 49.776 +Duct2 0.0025 0.4131 365.99 +Duct3 0.0050 0.3032 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2418 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.2133 1159.42 281.00 157.195 +Duct5 0.0075 0.3790 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.1923 1159.42 281.00 157.195 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 592.54 141.68 19.034 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.3723 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7243.6 17317.1 23883.3 +LP_Shaft 2692.6 41615.3 21334.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2097.97 0.9940 0.0550 1.98658 0.01466 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.285 0.9975 1.0000 0.9975 2706.36 0.610 700.5 20664.1 +Core_Nozz 1.149 0.9999 1.0000 0.9999 862.88 0.456 762.1 3575.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 18 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 0.0 27.00 848.55 8211.0 0.4866 3995.59 6.7065 229.02 7.042 1768.0 1728.7 1353.0 + core size:21.44 Q: 59.25 Maximum Thrust: 41056.7 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 848.55 15.111 550.04 131.47 0.0000 849.80 14.696 545.67 7339.5 0.2000 1.39991 +FS_2 Inlet.Fl_O 848.55 15.021 550.03 131.47 0.0000 854.94 14.372 543.14 5943.4 0.2520 1.39991 +FS_21 Fan.Fl_O 848.55 17.267 574.69 137.39 0.0000 760.19 16.225 564.57 4515.2 0.2996 1.39945 +FS_13 Splitter.Fl_O2 738.44 17.267 574.69 137.39 0.0000 661.55 16.144 563.77 3795.6 0.3114 1.39945 +FS_22 Splitter.Fl_O1 110.11 17.267 574.69 137.39 0.0000 98.64 16.593 568.19 719.5 0.2393 1.39945 +FS_23 Duct1.Fl_O 110.11 17.224 574.69 137.39 0.0000 98.89 16.551 568.19 721.3 0.2393 1.39945 +FS_24 LPC.Fl_O 110.11 23.468 638.42 152.72 0.0000 76.50 21.189 620.11 366.0 0.3850 1.39819 +FS_25 Duct2.Fl_O 110.11 23.409 638.42 152.72 0.0000 76.69 21.136 620.11 366.9 0.3850 1.39819 +FS_3 HPC.Fl_O 110.11 106.408 1030.55 248.59 0.0000 21.44 99.088 1010.55 119.9 0.3229 1.37880 +FS_36 Bld3.Fl_O 100.20 106.408 1030.55 248.59 0.0000 19.51 99.088 1010.55 109.1 0.3229 1.37880 +FS_4 Burner.Fl_O 101.31 100.556 1768.02 446.30 0.0111 27.34 99.911 1765.20 483.4 0.0984 1.32946 +FS_45 HPT.Fl_O 111.22 35.906 1352.99 333.76 0.0101 73.52 33.760 1331.45 439.1 0.3030 1.35156 +FS_48 Duct3.Fl_O 111.22 35.727 1352.99 333.76 0.0101 73.89 33.592 1331.45 441.4 0.3030 1.35156 +FS_5 LPT.Fl_O 111.22 15.912 1120.62 273.43 0.0101 150.99 15.573 1114.17 1477.4 0.1777 1.36617 +FS_7 Duct4.Fl_O 111.22 15.753 1120.62 273.43 0.0101 152.51 15.571 1117.14 2018.9 0.1303 1.36617 +FS_9 Core_Nozz.Fl_O 111.22 15.753 1120.62 273.43 0.0101 152.51 14.696 1099.91 862.9 0.3203 1.36617 +FS_15 BypBld.Fl_O 738.44 17.267 574.69 137.39 0.0000 661.55 16.144 563.77 3795.6 0.3114 1.39945 +FS_17 Duct5.Fl_O 738.44 17.138 574.69 137.39 0.0000 666.55 16.023 563.77 3824.3 0.3114 1.39945 +FS_19 Byp_Nozz.Fl_O 738.44 17.138 574.69 137.39 0.0000 666.55 14.696 550.00 2706.4 0.4739 1.39945 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 854.94 1.150 0.9061 2011.172 1.0448 0.9080 -7106.8 43.30 10.31 +LPC 98.89 1.363 0.8315 1967.554 1.1109 0.8387 -2386.9 42.31 12.52 +HPC 76.69 4.546 0.8624 6152.800 1.6142 0.8877 -14936.8 36.99 37.43 +HPT 27.34 2.801 0.9164 162.345 1.2661 0.9056 14937.7 +LPT 73.89 2.245 0.8930 56.306 1.2074 0.8823 9493.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1639.23 1.104 0.9361 0.510 1.7985 0.5215 1.4369 0.9679 3943.9586 +LPC 106.07 1.111 0.8662 0.537 1.8230 0.9323 3.2631 0.9600 3662.6571 +HPC 182.32 17.390 0.8508 0.968 2.2394 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.238 0.9348 106.030 5.2377 1.4085 0.4249 0.9803 1.5311 +LPT 153.53 2.737 0.8919 69.418 2.7372 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 7339.54 6040.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 777.21 186.27 35.569 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 777.21 186.27 35.569 +Duct1 0.0025 0.2393 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 777.21 186.27 35.569 +Duct2 0.0025 0.3850 365.99 +Duct3 0.0050 0.3030 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1777 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.8538 1030.55 248.59 106.408 +Duct5 0.0075 0.3114 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.0560 1030.55 248.59 106.408 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 574.69 137.39 17.267 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.7065 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6826.2 11493.1 14937.7 +LP_Shaft 2071.1 24073.5 9493.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1768.02 0.9940 0.0550 1.10989 0.01108 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.166 0.9975 1.0000 0.9975 2706.36 0.474 543.4 12472.5 +Core_Nozz 1.072 0.9999 1.0000 0.9999 862.88 0.320 514.6 1778.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 19 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 2/ 12/ 1/ 0 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 0.0 27.00 1597.56 39310.2 0.4633 18210.69 5.3616 286.28 19.820 2730.0 2661.7 2137.9 + core size:19.97 Q: 92.58 Maximum Thrust: 39310.2 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1597.56 15.349 552.49 132.06 0.0000 1578.70 14.696 545.67 11054.5 0.2500 1.39986 +FS_2 Inlet.Fl_O 1597.56 15.257 552.49 132.06 0.0000 1588.24 12.587 522.94 5943.4 0.5314 1.39986 +FS_21 Fan.Fl_O 1597.56 24.199 638.47 152.73 0.0000 1076.42 21.009 613.26 4515.2 0.4541 1.39818 +FS_13 Splitter.Fl_O2 1346.44 24.199 638.47 152.73 0.0000 907.21 20.990 613.10 3795.6 0.4556 1.39818 +FS_22 Splitter.Fl_O1 251.13 24.199 638.47 152.73 0.0000 169.21 21.112 614.11 719.5 0.4460 1.39818 +FS_23 Duct1.Fl_O 251.13 24.139 638.47 152.73 0.0000 169.63 21.059 614.11 721.3 0.4460 1.39818 +FS_24 LPC.Fl_O 251.13 54.276 828.76 198.83 0.0000 85.95 47.368 797.63 366.0 0.4465 1.39058 +FS_25 Duct2.Fl_O 251.13 54.141 828.76 198.83 0.0000 86.17 47.250 797.63 366.9 0.4465 1.39058 +FS_3 HPC.Fl_O 251.13 304.218 1405.45 344.33 0.0000 19.97 286.239 1383.14 119.9 0.3008 1.35558 +FS_36 Bld3.Fl_O 228.53 304.218 1405.45 344.33 0.0000 18.17 286.239 1383.14 109.1 0.3008 1.35558 +FS_4 Burner.Fl_O 233.58 287.486 2730.01 733.08 0.0221 27.39 285.634 2726.00 483.4 0.1000 1.29386 +FS_45 HPT.Fl_O 256.19 106.518 2137.92 556.15 0.0201 71.76 100.462 2108.52 439.1 0.2999 1.30945 +FS_48 Duct3.Fl_O 256.19 105.985 2137.92 556.15 0.0201 72.12 99.959 2108.52 441.4 0.2999 1.30945 +FS_5 LPT.Fl_O 256.19 22.957 1520.80 382.12 0.0201 280.82 21.145 1489.67 1477.4 0.3525 1.33532 +FS_7 Duct4.Fl_O 256.19 22.727 1520.80 382.12 0.0201 283.66 21.791 1504.80 2018.9 0.2516 1.33532 +FS_9 Core_Nozz.Fl_O 256.19 22.727 1520.80 382.12 0.0201 283.66 14.696 1361.69 862.8 0.8279 1.33532 +FS_15 BypBld.Fl_O 1346.44 24.199 638.47 152.73 0.0000 907.21 20.990 613.10 3795.6 0.4556 1.39818 +FS_17 Duct5.Fl_O 1346.44 24.018 638.47 152.73 0.0000 914.07 20.832 613.10 3824.3 0.4556 1.39818 +FS_19 Byp_Nozz.Fl_O 1346.44 24.018 638.47 152.73 0.0000 914.07 14.696 554.98 2706.4 0.8680 1.39818 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1588.24 1.586 0.9039 3636.582 1.1556 0.9099 -46702.2 29.43 17.01 +LPC 169.63 2.249 0.8650 3382.883 1.2981 0.8793 -16380.1 29.41 21.75 +HPC 86.17 5.619 0.8634 6341.431 1.6958 0.8906 -51698.9 20.72 20.73 +HPT 27.39 2.699 0.9145 153.417 1.2301 0.9050 51697.3 +LPT 72.12 4.617 0.9285 81.173 1.4058 0.9145 63081.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3045.20 1.408 0.9338 0.922 2.0364 0.5215 1.4369 0.9679 3943.9586 +LPC 181.95 1.383 0.9010 0.924 1.7523 0.9323 3.2631 0.9600 3662.6571 +HPC 204.86 22.353 0.8518 0.998 2.0866 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 4.999 0.9328 100.200 4.9987 1.4085 0.4249 0.9803 1.5311 +LPT 149.87 6.045 0.9273 100.077 6.0452 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 11054.54 14214.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1035.19 249.75 90.777 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1035.19 249.75 90.777 +Duct1 0.0025 0.4460 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1035.19 249.75 90.777 +Duct2 0.0025 0.4465 365.99 +Duct3 0.0050 0.2999 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3525 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.7894 1405.45 344.33 304.218 +Duct5 0.0075 0.4556 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 13.8120 1405.45 344.33 304.218 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 638.47 152.73 24.199 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3616 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 8016.0 33872.3 51697.3 +LP_Shaft 3753.3 88272.9 63081.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.01 0.9940 0.0550 5.05853 0.02214 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.634 0.9975 1.0000 0.9975 2706.36 0.868 999.8 41841.4 +Core_Nozz 1.546 0.9999 1.0000 0.9999 862.88 0.828 1467.4 11683.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 20 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 4/ 14/ 1/ 2 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 0.0 27.00 1536.05 35379.7 0.4570 16167.59 5.5173 286.28 18.260 2636.5 2571.1 2060.8 + core size:20.10 Q: 92.58 Maximum Thrust: 39310.2 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1536.05 15.349 552.49 132.06 0.0000 1517.91 14.696 545.67 10628.9 0.2500 1.39986 +FS_2 Inlet.Fl_O 1536.05 15.257 552.49 132.06 0.0000 1527.08 12.841 525.94 5943.4 0.5022 1.39986 +FS_21 Fan.Fl_O 1536.05 23.445 631.74 151.11 0.0000 1062.60 20.449 607.59 4515.2 0.4465 1.39838 +FS_13 Splitter.Fl_O2 1300.36 23.445 631.74 151.11 0.0000 899.56 20.398 607.16 3795.6 0.4506 1.39838 +FS_22 Splitter.Fl_O1 235.69 23.445 631.74 151.11 0.0000 163.04 20.705 609.75 719.5 0.4253 1.39838 +FS_23 Duct1.Fl_O 235.69 23.387 631.74 151.11 0.0000 163.45 20.653 609.75 721.3 0.4253 1.39838 +FS_24 LPC.Fl_O 235.69 50.867 812.12 194.77 0.0000 85.20 44.526 782.23 366.0 0.4414 1.39136 +FS_25 Duct2.Fl_O 235.69 50.740 812.12 194.77 0.0000 85.42 44.414 782.23 366.9 0.4414 1.39136 +FS_3 HPC.Fl_O 235.69 280.268 1371.68 335.52 0.0000 20.10 263.477 1349.51 119.9 0.3028 1.35756 +FS_36 Bld3.Fl_O 214.47 280.268 1371.68 335.52 0.0000 18.29 263.477 1349.51 109.1 0.3028 1.35756 +FS_4 Burner.Fl_O 218.97 264.853 2636.52 703.88 0.0209 27.39 263.147 2632.63 483.4 0.0999 1.29648 +FS_45 HPT.Fl_O 240.18 97.811 2060.84 533.22 0.0191 71.93 92.222 2032.13 439.1 0.3003 1.31264 +FS_48 Duct3.Fl_O 240.18 97.322 2060.84 533.22 0.0191 72.29 91.761 2032.13 441.4 0.3003 1.31264 +FS_5 LPT.Fl_O 240.18 21.682 1472.44 368.58 0.0191 274.29 20.058 1443.67 1477.4 0.3425 1.33863 +FS_7 Duct4.Fl_O 240.18 21.465 1472.44 368.58 0.0191 277.06 20.623 1457.60 2018.9 0.2450 1.33863 +FS_9 Core_Nozz.Fl_O 240.18 21.465 1472.44 368.58 0.0191 277.06 14.696 1336.84 862.9 0.7684 1.33863 +FS_15 BypBld.Fl_O 1300.36 23.445 631.74 151.11 0.0000 899.56 20.398 607.16 3795.6 0.4506 1.39838 +FS_17 Duct5.Fl_O 1300.36 23.270 631.74 151.11 0.0000 906.35 20.245 607.16 3824.3 0.4506 1.39838 +FS_19 Byp_Nozz.Fl_O 1300.36 23.270 631.74 151.11 0.0000 906.35 14.696 554.10 2706.3 0.8377 1.39838 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1527.08 1.537 0.9093 3509.960 1.1434 0.9146 -41386.2 32.62 17.19 +LPC 163.45 2.175 0.8624 3282.428 1.2855 0.8765 -14559.1 28.85 20.28 +HPC 85.42 5.524 0.8642 6321.128 1.6890 0.8912 -46937.3 22.03 22.09 +HPT 27.39 2.708 0.9146 154.043 1.2329 0.9050 46938.8 +LPT 72.29 4.489 0.9266 79.799 1.3996 0.9124 55945.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2927.93 1.374 0.9394 0.890 1.9659 0.5215 1.4369 0.9679 3943.9586 +LPC 175.32 1.360 0.8983 0.896 1.7248 0.9323 3.2631 0.9600 3662.6571 +HPC 203.06 21.912 0.8526 0.994 2.1051 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.019 0.9330 100.608 5.0195 1.4085 0.4249 0.9803 1.5311 +LPT 150.21 5.867 0.9254 98.382 5.8666 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 10628.87 13667.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1012.25 244.03 84.366 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1012.25 244.03 84.366 +Duct1 0.0025 0.4253 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1012.25 244.03 84.366 +Duct2 0.0025 0.4414 365.99 +Duct3 0.0050 0.3003 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3425 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.2490 1371.68 335.52 280.268 +Duct5 0.0075 0.4506 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.9628 1371.68 335.52 280.268 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 631.74 151.11 23.445 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5173 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7909.7 31167.9 46938.8 +LP_Shaft 3622.6 81110.5 55945.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2636.52 0.9940 0.0550 4.49100 0.02094 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.583 0.9975 1.0000 0.9975 2706.36 0.838 964.1 38966.1 +Core_Nozz 1.461 0.9999 1.0000 0.9999 862.88 0.768 1350.5 10081.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 21 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 0.0 27.00 1469.05 31448.2 0.4532 14250.92 5.6854 286.28 16.708 2544.1 2481.4 1984.7 + core size:20.22 Q: 92.58 Maximum Thrust: 39310.2 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1469.05 15.349 552.49 132.06 0.0000 1451.70 14.696 545.67 10165.3 0.2500 1.39986 +FS_2 Inlet.Fl_O 1469.05 15.257 552.49 132.06 0.0000 1460.47 13.094 528.87 5943.4 0.4724 1.39986 +FS_21 Fan.Fl_O 1469.05 22.667 625.01 149.49 0.0000 1045.55 19.879 602.06 4515.2 0.4372 1.39855 +FS_13 Splitter.Fl_O2 1249.31 22.667 625.01 149.49 0.0000 889.16 19.801 601.39 3795.6 0.4438 1.39855 +FS_22 Splitter.Fl_O1 219.74 22.667 625.01 149.49 0.0000 156.39 20.260 605.33 719.5 0.4038 1.39855 +FS_23 Duct1.Fl_O 219.74 22.610 625.01 149.49 0.0000 156.79 20.210 605.33 721.3 0.4038 1.39855 +FS_24 LPC.Fl_O 219.74 47.297 794.27 190.42 0.0000 84.49 41.517 765.59 366.0 0.4365 1.39222 +FS_25 Duct2.Fl_O 219.74 47.179 794.27 190.42 0.0000 84.70 41.413 765.59 366.9 0.4365 1.39222 +FS_3 HPC.Fl_O 219.74 256.441 1336.83 326.47 0.0000 20.22 240.883 1314.85 119.9 0.3045 1.35965 +FS_36 Bld3.Fl_O 199.96 256.441 1336.83 326.47 0.0000 18.40 240.883 1314.85 109.1 0.3045 1.35965 +FS_4 Burner.Fl_O 203.92 242.337 2544.07 675.29 0.0198 27.39 240.777 2540.29 483.4 0.0997 1.29928 +FS_45 HPT.Fl_O 223.70 89.163 1984.74 510.80 0.0180 72.12 84.040 1956.70 439.1 0.3008 1.31598 +FS_48 Duct3.Fl_O 223.70 88.717 1984.74 510.80 0.0180 72.49 83.619 1956.70 441.4 0.3008 1.31598 +FS_5 LPT.Fl_O 223.70 20.544 1427.74 356.16 0.0180 265.50 19.111 1401.65 1477.4 0.3295 1.34182 +FS_7 Duct4.Fl_O 223.70 20.338 1427.74 356.16 0.0180 268.18 19.593 1414.21 2018.9 0.2363 1.34182 +FS_9 Core_Nozz.Fl_O 223.70 20.338 1427.74 356.16 0.0180 268.18 14.696 1313.51 862.9 0.7089 1.34182 +FS_15 BypBld.Fl_O 1249.31 22.667 625.01 149.49 0.0000 889.16 19.801 601.39 3795.6 0.4438 1.39855 +FS_17 Duct5.Fl_O 1249.31 22.497 625.01 149.49 0.0000 895.88 19.653 601.39 3824.3 0.4438 1.39855 +FS_19 Byp_Nozz.Fl_O 1249.31 22.497 625.01 149.49 0.0000 895.88 14.696 553.50 2706.4 0.8043 1.39855 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1460.47 1.486 0.9112 3370.954 1.1313 0.9160 -36217.8 35.59 17.19 +LPC 156.79 2.092 0.8596 3169.349 1.2708 0.8733 -12725.3 28.40 18.93 +HPC 84.70 5.436 0.8647 6303.765 1.6831 0.8914 -42299.3 23.25 23.35 +HPT 27.39 2.718 0.9147 154.658 1.2358 0.9048 42299.3 +LPT 72.49 4.318 0.9247 78.094 1.3901 0.9105 48943.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2800.26 1.338 0.9413 0.855 1.9234 0.5215 1.4369 0.9679 3943.9586 +LPC 168.17 1.335 0.8954 0.865 1.7002 0.9323 3.2631 0.9600 3662.6571 +HPC 201.37 21.505 0.8530 0.992 2.1209 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.043 0.9331 101.010 5.0433 1.4085 0.4249 0.9803 1.5311 +LPT 150.62 5.629 0.9235 96.280 5.6291 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 10165.26 13071.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 988.14 238.04 77.836 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 988.14 238.04 77.836 +Duct1 0.0025 0.4038 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 988.14 238.04 77.836 +Duct2 0.0025 0.4365 365.99 +Duct3 0.0050 0.3008 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3295 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.6909 1336.83 326.47 256.441 +Duct5 0.0075 0.4438 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.0857 1336.83 326.47 256.441 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 625.01 149.49 22.667 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.6854 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7800.8 28479.4 42299.3 +LP_Shaft 3479.1 73884.8 48943.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2544.07 0.9940 0.0550 3.95859 0.01980 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.531 0.9975 1.0000 0.9975 2706.36 0.804 925.3 35926.9 +Core_Nozz 1.384 0.9999 1.0000 0.9999 862.88 0.709 1235.9 8592.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 22 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 0.0 27.00 1317.26 23585.8 0.4517 10654.22 6.0548 286.28 13.603 2344.7 2288.0 1820.4 + core size:20.48 Q: 92.58 Maximum Thrust: 39310.2 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1317.26 15.349 552.49 132.06 0.0000 1301.71 14.696 545.67 9115.0 0.2500 1.39986 +FS_2 Inlet.Fl_O 1317.26 15.257 552.49 132.06 0.0000 1309.57 13.585 534.48 5943.4 0.4104 1.39986 +FS_21 Fan.Fl_O 1317.26 21.050 610.92 146.10 0.0000 998.07 18.727 590.88 4515.2 0.4122 1.39886 +FS_13 Splitter.Fl_O2 1130.54 21.050 610.92 146.10 0.0000 856.59 18.613 589.85 3795.6 0.4231 1.39886 +FS_22 Splitter.Fl_O1 186.72 21.050 610.92 146.10 0.0000 141.47 19.268 595.70 719.5 0.3579 1.39886 +FS_23 Duct1.Fl_O 186.72 20.998 610.92 146.10 0.0000 141.83 19.220 595.70 721.3 0.3579 1.39886 +FS_24 LPC.Fl_O 186.72 39.832 753.66 180.56 0.0000 83.04 35.159 727.52 366.0 0.4267 1.39411 +FS_25 Duct2.Fl_O 186.72 39.733 753.66 180.56 0.0000 83.25 35.071 727.52 366.9 0.4267 1.39411 +FS_3 HPC.Fl_O 186.72 208.782 1259.79 306.60 0.0000 20.48 195.755 1238.27 119.9 0.3085 1.36439 +FS_36 Bld3.Fl_O 169.92 208.782 1259.79 306.60 0.0000 18.64 195.755 1238.27 109.1 0.3085 1.36439 +FS_4 Burner.Fl_O 172.87 197.299 2344.70 614.56 0.0174 27.38 196.029 2341.16 483.4 0.0995 1.30560 +FS_45 HPT.Fl_O 189.68 71.897 1820.44 463.19 0.0158 72.64 67.705 1793.84 439.1 0.3022 1.32391 +FS_48 Duct3.Fl_O 189.68 71.538 1820.44 463.19 0.0158 73.00 67.366 1793.84 441.4 0.3022 1.32391 +FS_5 LPT.Fl_O 189.68 18.630 1339.04 331.80 0.0158 240.41 17.582 1319.13 1477.4 0.2939 1.34852 +FS_7 Duct4.Fl_O 189.68 18.444 1339.04 331.80 0.0158 242.84 17.894 1328.61 2018.9 0.2122 1.34852 +FS_9 Core_Nozz.Fl_O 189.68 18.444 1339.04 331.80 0.0158 242.84 14.696 1262.28 862.9 0.5882 1.34852 +FS_15 BypBld.Fl_O 1130.54 21.050 610.92 146.10 0.0000 856.59 18.613 589.85 3795.6 0.4231 1.39886 +FS_17 Duct5.Fl_O 1130.54 20.892 610.92 146.10 0.0000 863.07 18.473 589.85 3824.3 0.4231 1.39886 +FS_19 Byp_Nozz.Fl_O 1130.54 20.892 610.92 146.10 0.0000 863.07 14.696 552.55 2706.4 0.7272 1.39886 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1309.57 1.380 0.9100 3043.881 1.1058 0.9140 -26159.7 39.06 16.70 +LPC 141.83 1.897 0.8537 2894.655 1.2336 0.8661 -9102.8 28.40 16.52 +HPC 83.25 5.255 0.8649 6272.143 1.6716 0.8910 -33299.4 25.92 26.06 +HPT 27.38 2.744 0.9150 156.141 1.2429 0.9050 33299.5 +LPT 73.00 3.840 0.9213 73.630 1.3595 0.9077 35262.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2510.92 1.264 0.9401 0.772 1.8673 0.5215 1.4369 0.9679 3943.9586 +LPC 152.13 1.275 0.8893 0.790 1.6737 0.9323 3.2631 0.9600 3662.6571 +HPC 197.92 20.668 0.8532 0.987 2.1537 0.4206 0.2163 1.0137 6357.1603 +HPT 30.12 5.105 0.9334 101.978 5.1051 1.4085 0.4249 0.9803 1.5311 +LPT 151.69 4.962 0.9201 90.777 4.9616 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 9114.96 11720.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 934.14 224.67 64.499 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 934.14 224.67 64.499 +Duct1 0.0025 0.3579 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 934.14 224.67 64.499 +Duct2 0.0025 0.4267 365.99 +Duct3 0.0050 0.3022 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2939 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.5352 1259.79 306.60 208.782 +Duct5 0.0075 0.4231 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.2696 1259.79 306.60 208.782 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 610.92 146.10 21.050 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.0548 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7560.7 23131.9 33299.5 +LP_Shaft 3141.6 58952.1 35262.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2344.70 0.9940 0.0550 2.95950 0.01742 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.422 0.9975 1.0000 0.9975 2706.36 0.727 835.8 29370.1 +Core_Nozz 1.255 0.9999 1.0000 0.9999 862.88 0.588 1007.0 5936.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 23 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 0.0 27.00 1133.39 15723.8 0.4661 7329.08 6.4615 286.28 10.471 2108.4 2058.8 1627.5 + core size:20.83 Q: 92.58 Maximum Thrust: 39310.2 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1133.39 15.349 552.49 132.06 0.0000 1120.00 14.696 545.67 7842.6 0.2500 1.39986 +FS_2 Inlet.Fl_O 1133.39 15.257 552.49 132.06 0.0000 1126.77 14.065 539.80 5943.4 0.3428 1.39986 +FS_21 Fan.Fl_O 1133.39 19.354 595.23 142.33 0.0000 921.92 17.571 579.04 4515.2 0.3742 1.39912 +FS_13 Splitter.Fl_O2 981.49 19.354 595.23 142.33 0.0000 798.36 17.448 577.88 3795.6 0.3878 1.39912 +FS_22 Splitter.Fl_O1 151.90 19.354 595.23 142.33 0.0000 123.56 18.136 584.29 719.5 0.3063 1.39912 +FS_23 Duct1.Fl_O 151.90 19.306 595.23 142.33 0.0000 123.87 18.090 584.29 721.3 0.3063 1.39912 +FS_24 LPC.Fl_O 151.90 32.235 705.70 168.95 0.0000 80.78 28.690 682.75 366.0 0.4119 1.39582 +FS_25 Duct2.Fl_O 151.90 32.155 705.70 168.95 0.0000 80.98 28.618 682.75 366.9 0.4119 1.39582 +FS_3 HPC.Fl_O 151.90 160.719 1166.50 282.80 0.0000 20.83 150.325 1145.58 119.9 0.3136 1.37025 +FS_36 Bld3.Fl_O 138.23 160.719 1166.50 282.80 0.0000 18.95 150.325 1145.58 109.1 0.3136 1.37025 +FS_4 Burner.Fl_O 140.26 151.880 2108.39 544.24 0.0147 27.36 150.904 2105.15 483.4 0.0991 1.31404 +FS_45 HPT.Fl_O 153.93 54.824 1627.50 408.67 0.0134 73.09 51.585 1602.82 439.1 0.3031 1.33440 +FS_48 Duct3.Fl_O 153.93 54.549 1627.50 408.67 0.0134 73.46 51.327 1602.82 441.4 0.3031 1.33440 +FS_5 LPT.Fl_O 153.93 17.145 1246.79 306.84 0.0134 204.58 16.460 1233.51 1477.4 0.2458 1.35590 +FS_7 Duct4.Fl_O 153.93 16.973 1246.79 306.84 0.0134 206.64 16.611 1239.74 2018.9 0.1787 1.35590 +FS_9 Core_Nozz.Fl_O 153.93 16.973 1246.79 306.84 0.0134 206.64 14.696 1200.45 863.0 0.4645 1.35590 +FS_15 BypBld.Fl_O 981.49 19.354 595.23 142.33 0.0000 798.36 17.448 577.88 3795.6 0.3878 1.39912 +FS_17 Duct5.Fl_O 981.49 19.209 595.23 142.33 0.0000 804.40 17.317 577.88 3824.3 0.3878 1.39912 +FS_19 Byp_Nozz.Fl_O 981.49 19.209 595.23 142.33 0.0000 804.40 14.696 551.40 2706.4 0.6307 1.39912 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1126.77 1.269 0.9087 2635.906 1.0774 0.9117 -16459.2 39.85 15.31 +LPC 123.87 1.670 0.8462 2539.511 1.1856 0.8570 -5720.5 31.12 14.16 +HPC 80.98 4.998 0.8643 6229.867 1.6530 0.8902 -24468.1 29.73 29.92 +HPT 27.36 2.770 0.9155 158.259 1.2518 0.9051 24468.1 +LPT 73.46 3.182 0.9107 67.435 1.3053 0.8973 22179.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2160.43 1.187 0.9388 0.668 1.8352 0.5215 1.4369 0.9679 3943.9586 +LPC 132.87 1.205 0.8814 0.693 1.6833 0.9323 3.2631 0.9600 3662.6571 +HPC 192.52 19.483 0.8527 0.980 2.1831 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.167 0.9338 103.362 5.1667 1.4085 0.4249 0.9803 1.5311 +LPT 152.65 4.043 0.9095 83.139 4.0434 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 7842.60 10084.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 869.52 208.79 50.989 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 869.52 208.79 50.989 +Duct1 0.0025 0.3063 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 869.52 208.79 50.989 +Duct2 0.0025 0.4119 365.99 +Duct3 0.0050 0.3031 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2458 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.3164 1166.50 282.80 160.719 +Duct5 0.0075 0.3878 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.3544 1166.50 282.80 160.719 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 595.23 142.33 19.354 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.4615 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7266.8 17684.4 24468.1 +LP_Shaft 2720.5 42818.5 22179.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2108.39 0.9940 0.0550 2.03586 0.01473 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.307 0.9975 1.0000 0.9975 2706.36 0.631 724.1 22090.2 +Core_Nozz 1.155 0.9999 1.0000 0.9999 862.88 0.465 777.2 3718.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 24 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 0.0 27.00 893.56 7861.8 0.5281 4151.99 6.9058 286.28 7.151 1784.9 1745.2 1366.7 + core size:21.43 Q: 92.58 Maximum Thrust: 39310.2 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 893.56 15.349 552.49 132.06 0.0000 883.01 14.696 545.67 6183.1 0.2500 1.39986 +FS_2 Inlet.Fl_O 893.56 15.257 552.49 132.06 0.0000 888.34 14.542 544.97 5943.4 0.2627 1.39986 +FS_21 Fan.Fl_O 893.56 17.573 577.52 138.07 0.0000 788.50 16.426 566.49 4515.2 0.3121 1.39940 +FS_13 Splitter.Fl_O2 780.53 17.573 577.52 138.07 0.0000 688.77 16.326 565.51 3795.6 0.3260 1.39940 +FS_22 Splitter.Fl_O1 113.03 17.573 577.52 138.07 0.0000 99.74 16.871 570.83 719.5 0.2421 1.39940 +FS_23 Duct1.Fl_O 113.03 17.529 577.52 138.07 0.0000 99.99 16.829 570.83 721.3 0.2421 1.39940 +FS_24 LPC.Fl_O 113.03 24.207 644.48 154.17 0.0000 76.49 21.857 626.00 366.0 0.3849 1.39800 +FS_25 Duct2.Fl_O 113.03 24.147 644.48 154.17 0.0000 76.68 21.803 626.00 366.9 0.3849 1.39800 +FS_3 HPC.Fl_O 113.03 109.764 1039.98 250.95 0.0000 21.43 102.219 1019.82 119.9 0.3229 1.37821 +FS_36 Bld3.Fl_O 102.85 109.764 1039.98 250.95 0.0000 19.50 102.219 1019.82 109.1 0.3229 1.37821 +FS_4 Burner.Fl_O 104.01 103.727 1784.89 451.04 0.0112 27.34 103.062 1782.05 483.4 0.0984 1.32862 +FS_45 HPT.Fl_O 114.18 37.063 1366.70 337.41 0.0102 73.49 34.850 1345.00 439.1 0.3030 1.35065 +FS_48 Duct3.Fl_O 114.18 36.878 1366.70 337.41 0.0102 73.86 34.676 1345.00 441.4 0.3030 1.35065 +FS_5 LPT.Fl_O 114.18 15.974 1124.49 274.45 0.0102 154.67 15.616 1117.69 1477.4 0.1823 1.36584 +FS_7 Duct4.Fl_O 114.18 15.814 1124.49 274.45 0.0102 156.23 15.623 1120.83 2018.9 0.1335 1.36584 +FS_9 Core_Nozz.Fl_O 114.18 15.814 1124.49 274.45 0.0102 156.23 14.696 1102.57 862.9 0.3293 1.36584 +FS_15 BypBld.Fl_O 780.53 17.573 577.52 138.07 0.0000 688.77 16.326 565.51 3795.6 0.3260 1.39940 +FS_17 Duct5.Fl_O 780.53 17.442 577.52 138.07 0.0000 693.97 16.204 565.51 3824.3 0.3260 1.39940 +FS_19 Byp_Nozz.Fl_O 780.53 17.442 577.52 138.07 0.0000 693.97 14.696 549.94 2706.4 0.5009 1.39940 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 888.34 1.152 0.9096 2047.996 1.0453 0.9114 -7597.5 46.01 11.67 +LPC 99.99 1.381 0.8314 2003.125 1.1159 0.8389 -2574.5 40.80 12.38 +HPC 76.68 4.546 0.8625 6152.579 1.6137 0.8878 -15475.8 36.97 37.41 +HPT 27.34 2.799 0.9164 162.334 1.2653 0.9055 15476.3 +LPT 73.86 2.309 0.8950 57.175 1.2154 0.8841 10171.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1703.27 1.106 0.9397 0.519 1.8629 0.5215 1.4369 0.9679 3943.9586 +LPC 107.25 1.117 0.8660 0.547 1.7987 0.9323 3.2631 0.9600 3662.6571 +HPC 182.29 17.391 0.8508 0.968 2.2387 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.233 0.9348 106.023 5.2333 1.4085 0.4249 0.9803 1.5311 +LPT 153.47 2.826 0.8939 70.490 2.8255 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 6183.08 7950.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 784.50 188.04 36.690 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 784.50 188.04 36.690 +Duct1 0.0025 0.2421 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 784.50 188.04 36.690 +Duct2 0.0025 0.3849 365.99 +Duct3 0.0050 0.3030 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1823 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.9559 1039.98 250.95 109.764 +Duct5 0.0075 0.3260 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.2164 1039.98 250.95 109.764 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 577.52 138.07 17.573 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.9058 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6858.3 11851.9 15476.3 +LP_Shaft 2113.7 25274.3 10171.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1784.89 0.9940 0.0550 1.15333 0.01121 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.187 0.9975 1.0000 0.9975 2706.36 0.501 574.4 13933.4 +Core_Nozz 1.076 0.9999 1.0000 0.9999 862.88 0.329 529.6 1879.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 25 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 0.0 27.00 1621.17 37733.1 0.4861 18341.11 5.3962 343.54 19.627 2730.0 2661.8 2138.1 + core size:19.99 Q: 133.32 Maximum Thrust: 37733.1 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1621.17 15.642 555.49 132.78 0.0000 1576.21 14.696 545.67 9348.2 0.3000 1.39980 +FS_2 Inlet.Fl_O 1621.17 15.549 555.49 132.78 0.0000 1585.73 12.839 525.91 5943.4 0.5302 1.39980 +FS_21 Fan.Fl_O 1621.17 24.553 641.03 153.34 0.0000 1078.73 21.300 615.59 4515.2 0.4554 1.39811 +FS_13 Splitter.Fl_O2 1367.71 24.553 641.03 153.34 0.0000 910.08 21.272 615.36 3795.6 0.4575 1.39811 +FS_22 Splitter.Fl_O1 253.46 24.553 641.03 153.34 0.0000 168.65 21.445 616.78 719.5 0.4442 1.39811 +FS_23 Duct1.Fl_O 253.46 24.492 641.03 153.34 0.0000 169.07 21.391 616.78 721.3 0.4442 1.39811 +FS_24 LPC.Fl_O 253.46 55.027 831.92 199.60 0.0000 85.73 48.066 800.88 366.0 0.4450 1.39043 +FS_25 Duct2.Fl_O 253.46 54.889 831.92 199.60 0.0000 85.94 47.946 800.88 366.9 0.4450 1.39043 +FS_3 HPC.Fl_O 253.46 307.014 1408.39 345.10 0.0000 19.99 288.826 1385.99 119.9 0.3012 1.35541 +FS_36 Bld3.Fl_O 230.65 307.014 1408.39 345.10 0.0000 18.19 288.826 1385.99 109.1 0.3012 1.35541 +FS_4 Burner.Fl_O 235.74 290.129 2730.00 733.03 0.0221 27.40 288.259 2725.99 483.4 0.1000 1.29389 +FS_45 HPT.Fl_O 258.55 107.499 2138.07 556.17 0.0201 71.76 101.386 2108.66 439.1 0.2999 1.30947 +FS_48 Duct3.Fl_O 258.55 106.961 2138.07 556.17 0.0201 72.12 100.879 2108.66 441.4 0.2999 1.30947 +FS_5 LPT.Fl_O 258.55 23.110 1520.12 381.92 0.0201 281.47 21.277 1488.84 1477.4 0.3534 1.33538 +FS_7 Duct4.Fl_O 258.55 22.879 1520.12 381.92 0.0201 284.31 21.932 1504.05 2018.9 0.2522 1.33538 +FS_9 Core_Nozz.Fl_O 258.55 22.879 1520.12 381.92 0.0201 284.31 14.696 1358.74 862.9 0.8346 1.33538 +FS_15 BypBld.Fl_O 1367.71 24.553 641.03 153.34 0.0000 910.08 21.272 615.36 3795.6 0.4575 1.39811 +FS_17 Duct5.Fl_O 1367.71 24.369 641.03 153.34 0.0000 916.95 21.112 615.36 3824.3 0.4575 1.39811 +FS_19 Byp_Nozz.Fl_O 1367.71 24.369 641.03 153.34 0.0000 916.95 14.696 554.91 2706.4 0.8817 1.39811 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1585.73 1.579 0.9040 3627.045 1.1540 0.9100 -47156.1 30.03 17.31 +LPC 169.07 2.247 0.8646 3376.389 1.2978 0.8790 -16587.4 29.17 21.48 +HPC 85.94 5.593 0.8638 6335.124 1.6929 0.8908 -52177.9 21.03 21.06 +HPT 27.40 2.699 0.9145 153.557 1.2301 0.9051 52177.9 +LPT 72.12 4.628 0.9283 81.177 1.4065 0.9143 63743.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3040.42 1.403 0.9339 0.920 2.0469 0.5215 1.4369 0.9679 3943.9586 +LPC 181.35 1.382 0.9006 0.922 1.7452 0.9323 3.2631 0.9600 3662.6571 +HPC 204.32 22.234 0.8521 0.997 2.0894 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 4.999 0.9329 100.291 4.9986 1.4085 0.4249 0.9803 1.5311 +LPT 149.87 6.061 0.9271 100.081 6.0613 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 9348.21 17309.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1038.28 250.52 91.826 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1038.28 250.52 91.826 +Duct1 0.0025 0.4442 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1038.28 250.52 91.826 +Duct2 0.0025 0.4450 365.99 +Duct3 0.0050 0.2999 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3534 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.8710 1408.39 345.10 307.014 +Duct5 0.0075 0.4575 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 13.9401 1408.39 345.10 307.014 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 641.03 153.34 24.553 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3962 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 8023.3 34156.2 52177.9 +LP_Shaft 3753.6 89191.5 63743.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.00 0.9940 0.0550 5.09475 0.02209 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.658 0.9975 1.0000 0.9975 2706.36 0.882 1015.5 43169.0 +Core_Nozz 1.557 0.9999 1.0000 0.9999 862.88 0.835 1477.6 11873.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 26 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 4/ 14/ 1/ 2 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 0.0 27.00 1561.63 33961.0 0.4806 16321.62 5.5549 343.54 18.118 2638.2 2572.9 2062.4 + core size:20.12 Q: 133.32 Maximum Thrust: 37733.1 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1561.63 15.642 555.49 132.78 0.0000 1518.32 14.696 545.67 9004.9 0.3000 1.39980 +FS_2 Inlet.Fl_O 1561.63 15.549 555.49 132.78 0.0000 1527.49 13.086 528.78 5943.4 0.5024 1.39980 +FS_21 Fan.Fl_O 1561.63 23.807 634.44 151.76 0.0000 1066.14 20.740 609.99 4515.2 0.4484 1.39830 +FS_13 Splitter.Fl_O2 1323.39 23.807 634.44 151.76 0.0000 903.49 20.681 609.49 3795.6 0.4532 1.39830 +FS_22 Splitter.Fl_O1 238.24 23.807 634.44 151.76 0.0000 162.65 21.040 612.49 719.5 0.4240 1.39830 +FS_23 Duct1.Fl_O 238.24 23.748 634.44 151.76 0.0000 163.06 20.987 612.49 721.3 0.4240 1.39830 +FS_24 LPC.Fl_O 238.24 51.679 815.76 195.66 0.0000 84.96 45.279 785.96 366.0 0.4398 1.39119 +FS_25 Duct2.Fl_O 238.24 51.550 815.76 195.66 0.0000 85.18 45.166 785.96 366.9 0.4398 1.39119 +FS_3 HPC.Fl_O 238.24 283.405 1375.43 336.50 0.0000 20.12 266.389 1353.16 119.9 0.3031 1.35734 +FS_36 Bld3.Fl_O 216.80 283.405 1375.43 336.50 0.0000 18.31 266.389 1353.16 109.1 0.3031 1.35734 +FS_4 Burner.Fl_O 221.33 267.818 2638.24 704.37 0.0209 27.39 266.093 2634.34 483.4 0.0999 1.29646 +FS_45 HPT.Fl_O 242.77 98.918 2062.44 533.66 0.0190 71.92 93.267 2033.71 439.1 0.3003 1.31260 +FS_48 Duct3.Fl_O 242.77 98.423 2062.44 533.66 0.0190 72.28 92.801 2033.71 441.4 0.3003 1.31260 +FS_5 LPT.Fl_O 242.77 21.837 1472.32 368.54 0.0190 275.27 20.189 1443.32 1477.4 0.3439 1.33865 +FS_7 Duct4.Fl_O 242.77 21.619 1472.32 368.54 0.0190 278.05 20.765 1457.37 2018.9 0.2460 1.33865 +FS_9 Core_Nozz.Fl_O 242.77 21.619 1472.32 368.54 0.0190 278.05 14.696 1334.27 862.9 0.7759 1.33865 +FS_15 BypBld.Fl_O 1323.39 23.807 634.44 151.76 0.0000 903.49 20.681 609.49 3795.6 0.4532 1.39830 +FS_17 Duct5.Fl_O 1323.39 23.629 634.44 151.76 0.0000 910.32 20.526 609.49 3824.3 0.4532 1.39830 +FS_19 Byp_Nozz.Fl_O 1323.39 23.629 634.44 151.76 0.0000 910.32 14.696 554.05 2706.3 0.8524 1.39830 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1527.49 1.531 0.9094 3504.650 1.1421 0.9146 -41919.3 33.24 17.55 +LPC 163.06 2.176 0.8620 3279.353 1.2858 0.8762 -14797.2 28.58 20.03 +HPC 85.18 5.498 0.8645 6315.167 1.6861 0.8913 -47474.6 22.34 22.38 +HPT 27.39 2.707 0.9146 154.193 1.2329 0.9050 47475.9 +LPT 72.28 4.507 0.9265 79.863 1.4008 0.9123 56715.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2928.81 1.370 0.9395 0.889 1.9821 0.5215 1.4369 0.9679 3943.9586 +LPC 174.90 1.360 0.8979 0.895 1.7175 0.9323 3.2631 0.9600 3662.6571 +HPC 202.49 21.792 0.8528 0.993 2.1072 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.019 0.9330 100.706 5.0187 1.4085 0.4249 0.9803 1.5311 +LPT 150.20 5.892 0.9253 98.461 5.8924 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 9004.88 16674.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1015.94 244.95 85.517 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1015.94 244.95 85.517 +Duct1 0.0025 0.4240 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1015.94 244.95 85.517 +Duct2 0.0025 0.4398 365.99 +Duct3 0.0050 0.3003 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3439 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.3383 1375.43 336.50 283.405 +Duct5 0.0075 0.4532 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 13.1031 1375.43 336.50 283.405 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 634.44 151.76 23.807 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5549 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7919.9 31483.7 47475.9 +LP_Shaft 3626.9 82129.9 56715.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2638.24 0.9940 0.0550 4.53378 0.02091 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.608 0.9975 1.0000 0.9975 2706.36 0.852 981.1 40354.4 +Core_Nozz 1.471 0.9999 1.0000 0.9999 862.88 0.776 1362.5 10280.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 27 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 0.0 27.00 1496.81 30186.5 0.4777 14419.31 5.7277 343.54 16.609 2547.1 2484.5 1987.4 + core size:20.24 Q: 133.32 Maximum Thrust: 37733.1 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1496.81 15.642 555.49 132.78 0.0000 1455.30 14.696 545.67 8631.2 0.3000 1.39980 +FS_2 Inlet.Fl_O 1496.81 15.549 555.49 132.78 0.0000 1464.10 13.331 531.59 5943.4 0.4740 1.39980 +FS_21 Fan.Fl_O 1496.81 23.035 627.82 150.16 0.0000 1050.60 20.170 604.48 4515.2 0.4399 1.39848 +FS_13 Splitter.Fl_O2 1274.33 23.035 627.82 150.16 0.0000 894.44 20.082 603.73 3795.6 0.4472 1.39848 +FS_22 Splitter.Fl_O1 222.49 23.035 627.82 150.16 0.0000 156.16 20.598 608.12 719.5 0.4030 1.39848 +FS_23 Duct1.Fl_O 222.49 22.978 627.82 150.16 0.0000 156.55 20.547 608.12 721.3 0.4030 1.39848 +FS_24 LPC.Fl_O 222.49 48.157 798.35 191.41 0.0000 84.23 42.314 769.75 366.0 0.4348 1.39202 +FS_25 Duct2.Fl_O 222.49 48.037 798.35 191.41 0.0000 84.45 42.208 769.75 366.9 0.4348 1.39202 +FS_3 HPC.Fl_O 222.49 259.808 1341.23 327.61 0.0000 20.24 244.010 1319.14 119.9 0.3049 1.35939 +FS_36 Bld3.Fl_O 202.46 259.808 1341.23 327.61 0.0000 18.42 244.010 1319.14 109.1 0.3049 1.35939 +FS_4 Burner.Fl_O 206.47 245.518 2547.09 676.17 0.0198 27.39 243.938 2543.30 483.4 0.0997 1.29922 +FS_45 HPT.Fl_O 226.49 90.356 1987.44 511.57 0.0180 72.11 85.167 1959.39 439.1 0.3008 1.31590 +FS_48 Duct3.Fl_O 226.49 89.904 1987.44 511.57 0.0180 72.47 84.741 1959.39 441.4 0.3008 1.31590 +FS_5 LPT.Fl_O 226.49 20.693 1427.86 356.19 0.0180 266.88 19.234 1401.47 1477.4 0.3315 1.34182 +FS_7 Duct4.Fl_O 226.49 20.486 1427.86 356.19 0.0180 269.58 19.728 1414.19 2018.9 0.2376 1.34182 +FS_9 Core_Nozz.Fl_O 226.49 20.486 1427.86 356.19 0.0180 269.58 14.696 1311.16 862.9 0.7170 1.34182 +FS_15 BypBld.Fl_O 1274.33 23.035 627.82 150.16 0.0000 894.44 20.082 603.73 3795.6 0.4472 1.39848 +FS_17 Duct5.Fl_O 1274.33 22.863 627.82 150.16 0.0000 901.20 19.931 603.73 3824.3 0.4472 1.39848 +FS_19 Byp_Nozz.Fl_O 1274.33 22.863 627.82 150.16 0.0000 901.20 14.696 553.43 2706.4 0.8204 1.39848 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1464.10 1.482 0.9116 3369.806 1.1302 0.9164 -36804.3 36.27 17.61 +LPC 156.55 2.096 0.8592 3169.766 1.2716 0.8729 -12984.8 28.09 18.70 +HPC 84.45 5.409 0.8649 6297.884 1.6800 0.8915 -42873.9 23.58 23.68 +HPT 27.39 2.717 0.9147 154.818 1.2357 0.9048 42873.9 +LPT 72.47 4.345 0.9246 78.226 1.3919 0.9103 49789.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2807.20 1.335 0.9418 0.854 1.9434 0.5215 1.4369 0.9679 3943.9586 +LPC 167.92 1.336 0.8950 0.865 1.6926 0.9323 3.2631 0.9600 3662.6571 +HPC 200.76 21.380 0.8532 0.991 2.1226 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.042 0.9331 101.115 5.0417 1.4085 0.4249 0.9803 1.5311 +LPT 150.59 5.666 0.9234 96.443 5.6656 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 8631.16 15982.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 992.34 239.08 79.061 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 992.34 239.08 79.061 +Duct1 0.0025 0.4030 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 992.34 239.08 79.061 +Duct2 0.0025 0.4348 365.99 +Duct3 0.0050 0.3008 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3315 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.7870 1341.23 327.61 259.808 +Duct5 0.0075 0.4472 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.2367 1341.23 327.61 259.808 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 627.82 150.16 23.035 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.7277 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7813.5 28819.3 42873.9 +LP_Shaft 3487.4 74984.4 49789.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2547.09 0.9940 0.0550 4.00536 0.01978 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.556 0.9975 1.0000 0.9975 2706.36 0.820 943.7 37375.7 +Core_Nozz 1.394 0.9999 1.0000 0.9999 862.88 0.717 1249.1 8792.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 28 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 0.0 27.00 1350.11 22639.7 0.4786 10834.83 6.1158 343.54 13.580 2350.4 2293.7 1825.4 + core size:20.50 Q: 133.32 Maximum Thrust: 37733.1 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1350.11 15.642 555.49 132.78 0.0000 1312.67 14.696 545.67 7785.2 0.3000 1.39980 +FS_2 Inlet.Fl_O 1350.11 15.549 555.49 132.78 0.0000 1320.60 13.812 537.01 5943.4 0.4148 1.39980 +FS_21 Fan.Fl_O 1350.11 21.428 613.90 146.82 0.0000 1007.37 19.012 593.31 4515.2 0.4171 1.39880 +FS_13 Splitter.Fl_O2 1160.38 21.428 613.90 146.82 0.0000 865.80 18.884 592.17 3795.6 0.4289 1.39880 +FS_22 Splitter.Fl_O1 189.73 21.428 613.90 146.82 0.0000 141.57 19.611 598.58 719.5 0.3581 1.39880 +FS_23 Duct1.Fl_O 189.73 21.374 613.90 146.82 0.0000 141.92 19.562 598.58 721.3 0.3581 1.39880 +FS_24 LPC.Fl_O 189.73 40.754 758.62 181.76 0.0000 82.74 36.013 732.54 366.0 0.4248 1.39390 +FS_25 Duct2.Fl_O 189.73 40.653 758.62 181.76 0.0000 82.95 35.923 732.54 366.9 0.4248 1.39390 +FS_3 HPC.Fl_O 189.73 212.423 1265.49 308.07 0.0000 20.50 199.141 1243.84 119.9 0.3088 1.36403 +FS_36 Bld3.Fl_O 172.66 212.423 1265.49 308.07 0.0000 18.66 199.141 1243.84 109.1 0.3088 1.36403 +FS_4 Burner.Fl_O 175.67 200.740 2350.39 616.24 0.0174 27.38 199.448 2346.85 483.4 0.0995 1.30544 +FS_45 HPT.Fl_O 192.74 73.192 1825.43 464.60 0.0159 72.60 68.928 1798.80 439.1 0.3021 1.32369 +FS_48 Duct3.Fl_O 192.74 72.827 1825.43 464.60 0.0159 72.97 68.584 1798.80 441.4 0.3021 1.32369 +FS_5 LPT.Fl_O 192.74 18.758 1339.46 331.91 0.0159 242.67 17.682 1319.14 1477.4 0.2970 1.34849 +FS_7 Duct4.Fl_O 192.74 18.571 1339.46 331.91 0.0159 245.12 18.006 1328.82 2018.9 0.2143 1.34849 +FS_9 Core_Nozz.Fl_O 192.74 18.571 1339.46 331.91 0.0159 245.12 14.696 1260.42 862.9 0.5972 1.34849 +FS_15 BypBld.Fl_O 1160.38 21.428 613.90 146.82 0.0000 865.80 18.884 592.17 3795.6 0.4289 1.39880 +FS_17 Duct5.Fl_O 1160.38 21.267 613.90 146.82 0.0000 872.34 18.742 592.17 3824.3 0.4289 1.39880 +FS_19 Byp_Nozz.Fl_O 1160.38 21.267 613.90 146.82 0.0000 872.34 14.696 552.43 2706.4 0.7463 1.39880 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1320.60 1.378 0.9117 3051.896 1.1051 0.9157 -26803.6 40.10 17.32 +LPC 141.92 1.907 0.8533 2903.083 1.2357 0.8658 -9380.6 27.93 16.30 +HPC 82.95 5.225 0.8650 6266.222 1.6681 0.8910 -33906.9 26.28 26.42 +HPT 27.38 2.743 0.9150 156.316 1.2426 0.9051 33906.9 +LPT 72.97 3.882 0.9214 73.923 1.3628 0.9078 36183.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2532.07 1.263 0.9419 0.774 1.8960 0.5215 1.4369 0.9679 3943.9586 +LPC 152.23 1.278 0.8888 0.793 1.6637 0.9323 3.2631 0.9600 3662.6571 +HPC 197.21 20.533 0.8533 0.986 2.1542 0.4206 0.2163 1.0137 6357.1603 +HPT 30.12 5.101 0.9334 102.093 5.1015 1.4085 0.4249 0.9803 1.5311 +LPT 151.62 5.021 0.9202 91.138 5.0208 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 7785.24 14415.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 939.38 225.97 65.817 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 939.38 225.97 65.817 +Duct1 0.0025 0.3581 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 939.38 225.97 65.817 +Duct2 0.0025 0.4248 365.99 +Duct3 0.0050 0.3021 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2970 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.6407 1265.49 308.07 212.423 +Duct5 0.0075 0.4289 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.4354 1265.49 308.07 212.423 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 613.90 146.82 21.428 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.1158 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7578.3 23499.0 33906.9 +LP_Shaft 3158.4 60171.0 36183.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2350.39 0.9940 0.0550 3.00967 0.01743 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.447 0.9975 1.0000 0.9975 2706.36 0.746 857.7 30934.3 +Core_Nozz 1.264 0.9999 1.0000 0.9999 862.88 0.597 1021.8 6121.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 29 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 0.0 27.00 1172.67 15093.1 0.4975 7508.97 6.5620 343.54 10.514 2118.0 2068.3 1635.6 + core size:20.85 Q: 133.32 Maximum Thrust: 37733.1 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1172.67 15.642 555.49 132.78 0.0000 1140.15 14.696 545.67 6762.0 0.3000 1.39980 +FS_2 Inlet.Fl_O 1172.67 15.549 555.49 132.78 0.0000 1147.04 14.285 542.21 5943.4 0.3500 1.39980 +FS_21 Fan.Fl_O 1172.67 19.730 598.38 143.09 0.0000 938.20 17.839 581.43 4515.2 0.3821 1.39907 +FS_13 Splitter.Fl_O2 1017.60 19.730 598.38 143.09 0.0000 814.13 17.698 580.11 3795.6 0.3972 1.39907 +FS_22 Splitter.Fl_O1 155.08 19.730 598.38 143.09 0.0000 124.07 18.476 587.28 719.5 0.3077 1.39907 +FS_23 Duct1.Fl_O 155.08 19.681 598.38 143.09 0.0000 124.38 18.430 587.28 721.3 0.3077 1.39907 +FS_24 LPC.Fl_O 155.08 33.154 711.53 170.35 0.0000 80.51 29.535 688.58 366.0 0.4102 1.39562 +FS_25 Duct2.Fl_O 155.08 33.071 711.53 170.35 0.0000 80.71 29.461 688.58 366.9 0.4102 1.39562 +FS_3 HPC.Fl_O 155.08 164.470 1173.93 284.68 0.0000 20.85 153.814 1152.87 119.9 0.3140 1.36978 +FS_36 Bld3.Fl_O 141.12 164.470 1173.93 284.68 0.0000 18.97 153.814 1152.87 109.1 0.3140 1.36978 +FS_4 Burner.Fl_O 143.20 155.424 2117.95 547.01 0.0148 27.36 154.425 2114.69 483.4 0.0991 1.31371 +FS_45 HPT.Fl_O 157.16 56.140 1635.58 410.90 0.0135 73.06 52.827 1610.82 439.1 0.3030 1.33397 +FS_48 Duct3.Fl_O 157.16 55.860 1635.58 410.90 0.0135 73.42 52.563 1610.82 441.4 0.3030 1.33397 +FS_5 LPT.Fl_O 157.16 17.246 1247.87 307.13 0.0135 207.73 16.535 1234.14 1477.4 0.2499 1.35580 +FS_7 Duct4.Fl_O 157.16 17.073 1247.87 307.13 0.0135 209.83 16.697 1240.59 2018.9 0.1816 1.35580 +FS_9 Core_Nozz.Fl_O 157.16 17.073 1247.87 307.13 0.0135 209.83 14.696 1199.63 862.9 0.4741 1.35580 +FS_15 BypBld.Fl_O 1017.60 19.730 598.38 143.09 0.0000 814.13 17.698 580.11 3795.6 0.3972 1.39907 +FS_17 Duct5.Fl_O 1017.60 19.582 598.38 143.09 0.0000 820.28 17.565 580.11 3824.3 0.3972 1.39907 +FS_19 Byp_Nozz.Fl_O 1017.60 19.582 598.38 143.09 0.0000 820.28 14.696 551.29 2706.4 0.6538 1.39907 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1147.04 1.269 0.9113 2655.442 1.0772 0.9143 -17092.4 41.59 16.28 +LPC 124.38 1.685 0.8459 2558.501 1.1891 0.8568 -5982.9 30.38 13.97 +HPC 80.71 4.973 0.8643 6225.349 1.6499 0.8901 -25085.1 30.05 30.25 +HPT 27.36 2.768 0.9155 158.437 1.2514 0.9051 25085.2 +LPT 73.42 3.239 0.9113 67.951 1.3107 0.8978 23074.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2199.29 1.187 0.9415 0.673 1.8787 0.5215 1.4369 0.9679 3943.9586 +LPC 133.42 1.210 0.8811 0.699 1.6698 0.9323 3.2631 0.9600 3662.6571 +HPC 191.89 19.367 0.8527 0.979 2.1829 0.4206 0.2163 1.0137 6357.1603 +HPT 30.10 5.162 0.9339 103.478 5.1623 1.4085 0.4249 0.9803 1.5311 +LPT 152.57 4.123 0.9101 83.775 4.1233 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 6762.04 12521.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 875.95 210.37 52.321 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 875.95 210.37 52.321 +Duct1 0.0025 0.3077 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 875.95 210.37 52.321 +Duct2 0.0025 0.4102 365.99 +Duct3 0.0050 0.3030 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2499 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.4276 1173.93 284.68 164.470 +Duct5 0.0075 0.3972 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.5291 1173.93 284.68 164.470 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 598.38 143.09 19.730 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.5620 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7291.5 18069.1 25085.2 +LP_Shaft 2748.1 44100.3 23074.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2117.95 0.9940 0.0550 2.08582 0.01478 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.332 0.9975 1.0000 0.9975 2706.36 0.654 750.6 23740.8 +Core_Nozz 1.162 0.9999 1.0000 0.9999 862.88 0.474 793.0 3873.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 30 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 0.0 27.00 942.69 7546.5 0.5715 4312.94 7.1139 343.54 7.246 1800.8 1760.8 1379.8 + core size:21.43 Q: 133.32 Maximum Thrust: 37733.1 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 942.69 15.642 555.49 132.78 0.0000 916.54 14.696 545.67 5435.9 0.3000 1.39980 +FS_2 Inlet.Fl_O 942.69 15.549 555.49 132.78 0.0000 922.08 14.760 547.30 5943.4 0.2736 1.39980 +FS_21 Fan.Fl_O 942.69 17.932 580.83 138.87 0.0000 817.55 16.665 568.82 4515.2 0.3252 1.39935 +FS_13 Splitter.Fl_O2 826.51 17.932 580.83 138.87 0.0000 716.79 16.543 567.62 3795.6 0.3413 1.39935 +FS_22 Splitter.Fl_O1 116.18 17.932 580.83 138.87 0.0000 100.76 17.200 573.96 719.5 0.2448 1.39935 +FS_23 Duct1.Fl_O 116.18 17.887 580.83 138.87 0.0000 101.01 17.157 573.96 721.3 0.2448 1.39935 +FS_24 LPC.Fl_O 116.18 25.044 651.08 155.76 0.0000 76.39 22.619 632.48 366.0 0.3843 1.39778 +FS_25 Duct2.Fl_O 116.18 24.981 651.08 155.76 0.0000 76.58 22.563 632.48 366.9 0.3843 1.39778 +FS_3 HPC.Fl_O 116.18 113.349 1049.67 253.37 0.0000 21.43 105.556 1029.35 119.9 0.3230 1.37761 +FS_36 Bld3.Fl_O 105.73 113.349 1049.67 253.37 0.0000 19.50 105.556 1029.35 109.1 0.3230 1.37761 +FS_4 Burner.Fl_O 106.92 107.115 1800.85 455.52 0.0113 27.33 106.428 1797.99 483.4 0.0985 1.32785 +FS_45 HPT.Fl_O 117.38 38.305 1379.77 340.90 0.0103 73.45 36.020 1357.92 439.1 0.3029 1.34980 +FS_48 Duct3.Fl_O 117.38 38.113 1379.77 340.90 0.0103 73.82 35.840 1357.92 441.4 0.3029 1.34980 +FS_5 LPT.Fl_O 117.38 16.042 1127.75 275.31 0.0103 158.56 15.664 1120.57 1477.4 0.1871 1.36556 +FS_7 Duct4.Fl_O 117.38 15.882 1127.75 275.31 0.0103 160.16 15.680 1123.89 2018.9 0.1370 1.36556 +FS_9 Core_Nozz.Fl_O 117.38 15.882 1127.75 275.31 0.0103 160.16 14.696 1104.51 862.9 0.3388 1.36556 +FS_15 BypBld.Fl_O 826.51 17.932 580.83 138.87 0.0000 716.79 16.543 567.62 3795.6 0.3413 1.39935 +FS_17 Duct5.Fl_O 826.51 17.798 580.83 138.87 0.0000 722.21 16.419 567.62 3824.3 0.3413 1.39935 +FS_19 Byp_Nozz.Fl_O 826.51 17.798 580.83 138.87 0.0000 722.21 14.696 549.92 2706.4 0.5304 1.39935 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 922.08 1.153 0.9112 2083.770 1.0456 0.9131 -8116.6 48.88 13.18 +LPC 101.01 1.400 0.8324 2037.802 1.1209 0.8402 -2777.0 39.28 12.19 +HPC 76.58 4.537 0.8625 6150.673 1.6122 0.8877 -16045.0 37.07 37.52 +HPT 27.33 2.796 0.9164 162.389 1.2646 0.9055 16045.4 +LPT 73.82 2.376 0.8961 58.055 1.2235 0.8848 10893.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1767.97 1.107 0.9414 0.528 1.9318 0.5215 1.4369 0.9679 3943.9586 +LPC 108.35 1.123 0.8671 0.556 1.7741 0.9323 3.2631 0.9600 3662.6571 +HPC 182.05 17.353 0.8509 0.968 2.2392 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.228 0.9348 106.059 5.2280 1.4085 0.4249 0.9803 1.5311 +LPT 153.39 2.919 0.8949 71.574 2.9192 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 5435.87 10065.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 792.24 189.93 37.927 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 792.24 189.93 37.927 +Duct1 0.0025 0.2448 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 792.24 189.93 37.927 +Duct2 0.0025 0.3843 365.99 +Duct3 0.0050 0.3029 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1871 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.0664 1049.67 253.37 113.349 +Duct5 0.0075 0.3413 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.3900 1049.67 253.37 113.349 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 580.83 138.87 17.932 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.1139 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6891.2 12229.0 16045.4 +LP_Shaft 2156.5 26531.0 10893.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1800.85 0.9940 0.0550 1.19804 0.01133 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.211 0.9975 1.0000 0.9975 2706.36 0.530 608.2 15622.4 +Core_Nozz 1.081 0.9999 1.0000 0.9999 862.88 0.339 545.4 1989.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 31 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 0.0 27.00 1682.38 35120.3 0.5321 18688.33 5.4792 458.05 19.168 2730.0 2662.2 2138.4 + core size:20.05 Q: 237.01 Maximum Thrust: 35120.3 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1682.38 16.408 563.13 134.62 0.0000 1570.07 14.696 545.67 7275.9 0.4000 1.39966 +FS_2 Inlet.Fl_O 1682.38 16.326 563.13 134.62 0.0000 1577.98 13.517 533.55 5943.4 0.5264 1.39966 +FS_21 Fan.Fl_O 1682.38 25.508 647.63 154.93 0.0000 1083.11 22.095 621.67 4515.2 0.4578 1.39789 +FS_13 Splitter.Fl_O2 1422.73 25.508 647.63 154.93 0.0000 915.94 22.046 621.28 3795.6 0.4614 1.39789 +FS_22 Splitter.Fl_O1 259.66 25.508 647.63 154.93 0.0000 167.17 22.345 623.67 719.5 0.4391 1.39789 +FS_23 Duct1.Fl_O 259.66 25.444 647.63 154.93 0.0000 167.59 22.290 623.67 721.3 0.4391 1.39789 +FS_24 LPC.Fl_O 259.66 57.027 839.97 201.56 0.0000 85.15 49.927 809.17 366.0 0.4413 1.39006 +FS_25 Duct2.Fl_O 259.66 56.885 839.97 201.56 0.0000 85.37 49.802 809.17 366.9 0.4413 1.39006 +FS_3 HPC.Fl_O 259.66 314.520 1415.97 347.08 0.0000 20.05 295.777 1393.33 119.9 0.3022 1.35498 +FS_36 Bld3.Fl_O 236.29 314.520 1415.97 347.08 0.0000 18.24 295.777 1393.33 109.1 0.3022 1.35498 +FS_4 Burner.Fl_O 241.48 297.221 2730.00 732.92 0.0220 27.39 295.306 2726.00 483.4 0.1000 1.29397 +FS_45 HPT.Fl_O 264.85 110.122 2138.44 556.21 0.0200 71.77 103.860 2109.02 439.1 0.3000 1.30953 +FS_48 Duct3.Fl_O 264.85 109.572 2138.44 556.21 0.0200 72.13 103.340 2109.02 441.4 0.3000 1.30953 +FS_5 LPT.Fl_O 264.85 23.531 1518.51 381.44 0.0200 283.02 21.642 1486.85 1477.4 0.3557 1.33554 +FS_7 Duct4.Fl_O 264.85 23.296 1518.51 381.44 0.0200 285.88 22.320 1502.26 2018.9 0.2537 1.33554 +FS_9 Core_Nozz.Fl_O 264.85 23.296 1518.51 381.44 0.0200 285.88 14.696 1350.97 862.9 0.8523 1.33554 +FS_15 BypBld.Fl_O 1422.73 25.508 647.63 154.93 0.0000 915.94 22.046 621.28 3795.6 0.4614 1.39789 +FS_17 Duct5.Fl_O 1422.73 25.316 647.63 154.93 0.0000 922.86 21.880 621.28 3824.3 0.4614 1.39789 +FS_19 Byp_Nozz.Fl_O 1422.73 25.316 647.63 154.93 0.0000 922.86 14.696 554.57 2706.4 0.9169 1.39789 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1577.98 1.562 0.9043 3602.174 1.1501 0.9101 -48358.9 31.46 17.94 +LPC 167.59 2.241 0.8635 3358.947 1.2970 0.8780 -17130.9 28.54 20.79 +HPC 85.37 5.529 0.8645 6320.041 1.6857 0.8912 -53460.7 21.81 21.88 +HPT 27.39 2.699 0.9146 153.930 1.2302 0.9051 53460.7 +LPT 72.13 4.656 0.9279 81.166 1.4082 0.9138 65490.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3025.56 1.391 0.9342 0.913 2.0650 0.5215 1.4369 0.9679 3943.9586 +LPC 179.76 1.380 0.8995 0.917 1.7270 0.9323 3.2631 0.9600 3662.6571 +HPC 202.95 21.937 0.8528 0.994 2.0962 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 4.999 0.9329 100.535 4.9988 1.4085 0.4249 0.9803 1.5311 +LPT 149.87 6.101 0.9267 100.067 6.1006 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 7275.92 23951.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1046.17 252.50 94.628 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1046.17 252.50 94.628 +Duct1 0.0025 0.4391 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1046.17 252.50 94.628 +Duct2 0.0025 0.4413 365.99 +Duct3 0.0050 0.3000 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3557 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 9.0880 1415.97 347.08 314.520 +Duct5 0.0075 0.4614 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 14.2812 1415.97 347.08 314.520 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 647.63 154.93 25.508 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.4792 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 8042.8 34911.1 53460.7 +LP_Shaft 3753.4 91640.5 65490.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.00 0.9940 0.0550 5.19120 0.02197 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.723 0.9975 1.0000 0.9975 2706.36 0.917 1055.7 46683.5 +Core_Nozz 1.585 0.9999 1.0000 0.9999 862.88 0.852 1504.9 12388.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:43 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 32 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 0.0 27.00 1626.56 31608.3 0.5284 16701.28 5.6458 458.05 17.756 2641.4 2576.3 2065.5 + core size:20.17 Q: 237.01 Maximum Thrust: 35120.3 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1626.56 16.408 563.13 134.62 0.0000 1517.98 14.696 545.67 7034.5 0.4000 1.39966 +FS_2 Inlet.Fl_O 1626.56 16.326 563.13 134.62 0.0000 1525.62 13.748 536.14 5943.4 0.5016 1.39966 +FS_21 Fan.Fl_O 1626.56 24.769 641.31 153.41 0.0000 1073.12 21.528 616.19 4515.2 0.4523 1.39810 +FS_13 Splitter.Fl_O2 1381.81 24.769 641.31 153.41 0.0000 911.64 21.445 615.51 3795.6 0.4586 1.39810 +FS_22 Splitter.Fl_O1 244.75 24.769 641.31 153.41 0.0000 161.47 21.938 619.51 719.5 0.4202 1.39810 +FS_23 Duct1.Fl_O 244.75 24.707 641.31 153.41 0.0000 161.88 21.883 619.51 721.3 0.4202 1.39810 +FS_24 LPC.Fl_O 244.75 53.768 824.73 197.84 0.0000 84.35 47.221 795.15 366.0 0.4358 1.39077 +FS_25 Duct2.Fl_O 244.75 53.633 824.73 197.84 0.0000 84.57 47.103 795.15 366.9 0.4358 1.39077 +FS_3 HPC.Fl_O 244.75 291.337 1384.46 338.85 0.0000 20.17 273.745 1361.94 119.9 0.3041 1.35681 +FS_36 Bld3.Fl_O 222.72 291.337 1384.46 338.85 0.0000 18.36 273.745 1361.94 109.1 0.3041 1.35681 +FS_4 Burner.Fl_O 227.36 275.313 2641.41 705.25 0.0208 27.39 273.541 2637.51 483.4 0.0999 1.29645 +FS_45 HPT.Fl_O 249.39 101.708 2065.49 534.50 0.0190 71.91 95.900 2036.74 439.1 0.3003 1.31255 +FS_48 Duct3.Fl_O 249.39 101.199 2065.49 534.50 0.0190 72.27 95.420 2036.74 441.4 0.3003 1.31255 +FS_5 LPT.Fl_O 249.39 22.238 1471.61 368.32 0.0190 277.60 20.528 1442.05 1477.4 0.3473 1.33874 +FS_7 Duct4.Fl_O 249.39 22.016 1471.61 368.32 0.0190 280.41 21.130 1456.39 2018.9 0.2482 1.33874 +FS_9 Core_Nozz.Fl_O 249.39 22.016 1471.61 368.32 0.0190 280.41 14.696 1327.35 862.9 0.7949 1.33874 +FS_15 BypBld.Fl_O 1381.81 24.769 641.31 153.41 0.0000 911.64 21.445 615.51 3795.6 0.4586 1.39810 +FS_17 Duct5.Fl_O 1381.81 24.583 641.31 153.41 0.0000 918.53 21.284 615.51 3824.3 0.4586 1.39810 +FS_19 Byp_Nozz.Fl_O 1381.81 24.583 641.31 153.41 0.0000 918.53 14.696 553.76 2706.4 0.8898 1.39810 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1525.62 1.517 0.9093 3487.886 1.1388 0.9145 -43247.4 34.68 18.30 +LPC 161.88 2.176 0.8609 3268.384 1.2860 0.8751 -15386.7 27.87 19.39 +HPC 84.57 5.432 0.8650 6300.755 1.6787 0.8915 -48830.4 23.14 23.23 +HPT 27.39 2.707 0.9147 154.591 1.2328 0.9051 48830.3 +LPT 72.27 4.551 0.9262 79.966 1.4036 0.9118 58634.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2925.17 1.360 0.9394 0.884 2.0138 0.5215 1.4369 0.9679 3943.9586 +LPC 173.64 1.360 0.8967 0.892 1.6988 0.9323 3.2631 0.9600 3662.6571 +HPC 201.05 21.488 0.8534 0.991 2.1127 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.017 0.9330 100.966 5.0174 1.4085 0.4249 0.9803 1.5311 +LPT 150.17 5.953 0.9250 98.589 5.9531 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 7034.48 23156.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1024.95 247.20 88.457 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1024.95 247.20 88.457 +Duct1 0.0025 0.4202 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1024.95 247.20 88.457 +Duct2 0.0025 0.4358 365.99 +Duct3 0.0050 0.3003 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3473 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.5663 1384.46 338.85 291.337 +Duct5 0.0075 0.4586 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 13.4613 1384.46 338.85 291.337 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 641.31 153.41 24.769 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.6458 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7945.2 32279.1 48830.3 +LP_Shaft 3634.3 84735.3 58634.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2641.41 0.9940 0.0550 4.63924 0.02083 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.673 0.9975 1.0000 0.9975 2706.36 0.890 1023.9 43972.6 +Core_Nozz 1.498 0.9999 1.0000 0.9999 862.88 0.795 1392.3 10792.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 33 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 0.0 27.00 1565.88 28096.3 0.5274 14817.05 5.8295 458.05 16.337 2552.8 2490.4 1992.7 + core size:20.29 Q: 237.01 Maximum Thrust: 35120.3 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1565.88 16.408 563.13 134.62 0.0000 1461.35 14.696 545.67 6772.1 0.4000 1.39966 +FS_2 Inlet.Fl_O 1565.88 16.326 563.13 134.62 0.0000 1468.71 13.979 538.71 5943.4 0.4760 1.39966 +FS_21 Fan.Fl_O 1565.88 24.002 634.90 151.87 0.0000 1060.74 20.947 610.73 4515.2 0.4455 1.39829 +FS_13 Splitter.Fl_O2 1336.60 24.002 634.90 151.87 0.0000 905.42 20.834 609.79 3795.6 0.4544 1.39829 +FS_22 Splitter.Fl_O1 229.28 24.002 634.90 151.87 0.0000 155.32 21.494 615.24 719.5 0.4004 1.39829 +FS_23 Duct1.Fl_O 229.28 23.942 634.90 151.87 0.0000 155.71 21.440 615.24 721.3 0.4004 1.39829 +FS_24 LPC.Fl_O 229.28 50.324 808.24 193.82 0.0000 83.58 44.328 779.86 366.0 0.4306 1.39155 +FS_25 Duct2.Fl_O 229.28 50.198 808.24 193.82 0.0000 83.79 44.217 779.86 366.9 0.4306 1.39155 +FS_3 HPC.Fl_O 229.28 268.061 1351.60 330.31 0.0000 20.29 251.667 1329.24 119.9 0.3059 1.35876 +FS_36 Bld3.Fl_O 208.65 268.061 1351.60 330.31 0.0000 18.47 251.667 1329.24 109.1 0.3059 1.35876 +FS_4 Burner.Fl_O 212.76 253.318 2552.82 677.83 0.0197 27.38 251.687 2549.02 483.4 0.0997 1.29913 +FS_45 HPT.Fl_O 233.40 93.269 1992.66 513.03 0.0180 72.08 87.917 1964.56 439.1 0.3007 1.31574 +FS_48 Duct3.Fl_O 233.40 92.803 1992.66 513.03 0.0180 72.44 87.477 1964.56 441.4 0.3007 1.31574 +FS_5 LPT.Fl_O 233.40 21.069 1427.52 356.09 0.0180 270.08 19.544 1400.41 1477.4 0.3360 1.34188 +FS_7 Duct4.Fl_O 233.40 20.858 1427.52 356.09 0.0180 272.81 20.066 1413.50 2018.9 0.2407 1.34188 +FS_9 Core_Nozz.Fl_O 233.40 20.858 1427.52 356.09 0.0180 272.81 14.696 1304.74 862.9 0.7370 1.34188 +FS_15 BypBld.Fl_O 1336.60 24.002 634.90 151.87 0.0000 905.42 20.834 609.79 3795.6 0.4544 1.39829 +FS_17 Duct5.Fl_O 1336.60 23.822 634.90 151.87 0.0000 912.27 20.678 609.79 3824.3 0.4544 1.39829 +FS_19 Byp_Nozz.Fl_O 1336.60 23.822 634.90 151.87 0.0000 912.27 14.696 553.16 2706.4 0.8602 1.39829 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1468.71 1.470 0.9118 3361.794 1.1274 0.9165 -38215.9 37.84 18.53 +LPC 155.71 2.102 0.8579 3166.089 1.2730 0.8719 -13610.2 27.30 18.09 +HPC 83.79 5.340 0.8653 6283.630 1.6723 0.8916 -44275.6 24.41 24.53 +HPT 27.38 2.716 0.9148 155.247 1.2355 0.9049 44275.6 +LPT 72.44 4.405 0.9243 78.472 1.3959 0.9098 51826.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2816.05 1.327 0.9420 0.852 1.9846 0.5215 1.4369 0.9679 3943.9586 +LPC 167.02 1.338 0.8937 0.864 1.6730 0.9323 3.2631 0.9600 3662.6571 +HPC 199.21 21.063 0.8536 0.988 2.1270 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.039 0.9332 101.395 5.0387 1.4085 0.4249 0.9803 1.5311 +LPT 150.53 5.749 0.9231 96.746 5.7495 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6772.08 22292.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1002.43 241.59 82.115 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1002.43 241.59 82.115 +Duct1 0.0025 0.4004 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1002.43 241.59 82.115 +Duct2 0.0025 0.4306 365.99 +Duct3 0.0050 0.3007 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3360 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.0249 1351.60 330.31 268.061 +Duct5 0.0075 0.4544 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.6105 1351.60 330.31 268.061 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 634.90 151.87 24.002 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.8295 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7843.9 29645.9 44275.6 +LP_Shaft 3502.9 77705.9 51826.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2552.82 0.9940 0.0550 4.11585 0.01973 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.621 0.9975 1.0000 0.9975 2706.36 0.860 989.3 41097.4 +Core_Nozz 1.419 0.9999 1.0000 0.9999 862.88 0.737 1280.9 9291.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 34 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 0.0 27.00 1428.93 21072.1 0.5331 11234.52 6.2590 458.05 13.463 2360.9 2304.3 1834.8 + core size:20.56 Q: 237.01 Maximum Thrust: 35120.3 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1428.93 16.408 563.13 134.62 0.0000 1333.54 14.696 545.67 6179.8 0.4000 1.39966 +FS_2 Inlet.Fl_O 1428.93 16.326 563.13 134.62 0.0000 1340.25 14.439 543.71 5943.4 0.4225 1.39966 +FS_21 Fan.Fl_O 1428.93 22.396 621.32 148.60 0.0000 1026.22 19.760 599.52 4515.2 0.4269 1.39864 +FS_13 Splitter.Fl_O2 1232.08 22.396 621.32 148.60 0.0000 884.85 19.598 598.11 3795.6 0.4410 1.39864 +FS_22 Splitter.Fl_O1 196.85 22.396 621.32 148.60 0.0000 141.37 20.503 605.87 719.5 0.3576 1.39864 +FS_23 Duct1.Fl_O 196.85 22.340 621.32 148.60 0.0000 141.73 20.452 605.87 721.3 0.3576 1.39864 +FS_24 LPC.Fl_O 196.85 42.996 770.27 184.59 0.0000 81.99 38.099 744.39 366.0 0.4200 1.39338 +FS_25 Duct2.Fl_O 196.85 42.889 770.27 184.59 0.0000 82.20 38.004 744.39 366.9 0.4200 1.39338 +FS_3 HPC.Fl_O 196.85 220.907 1278.35 311.37 0.0000 20.56 207.013 1256.38 119.9 0.3099 1.36323 +FS_36 Bld3.Fl_O 179.13 220.907 1278.35 311.37 0.0000 18.71 207.013 1256.38 109.1 0.3099 1.36323 +FS_4 Burner.Fl_O 182.25 208.757 2360.90 619.31 0.0174 27.37 207.415 2357.34 483.4 0.0995 1.30517 +FS_45 HPT.Fl_O 199.97 76.199 1834.79 467.22 0.0159 72.54 71.768 1808.09 439.1 0.3019 1.32331 +FS_48 Duct3.Fl_O 199.97 75.818 1834.79 467.22 0.0159 72.90 71.410 1808.09 441.4 0.3019 1.32331 +FS_5 LPT.Fl_O 199.97 19.066 1339.33 331.87 0.0159 247.69 17.923 1318.07 1477.4 0.3039 1.34851 +FS_7 Duct4.Fl_O 199.97 18.875 1339.33 331.87 0.0159 250.19 18.277 1328.22 2018.9 0.2189 1.34851 +FS_9 Core_Nozz.Fl_O 199.97 18.875 1339.33 331.87 0.0159 250.19 14.696 1254.95 862.9 0.6182 1.34851 +FS_15 BypBld.Fl_O 1232.08 22.396 621.32 148.60 0.0000 884.85 19.598 598.11 3795.6 0.4410 1.39864 +FS_17 Duct5.Fl_O 1232.08 22.228 621.32 148.60 0.0000 891.54 19.451 598.11 3824.3 0.4410 1.39864 +FS_19 Byp_Nozz.Fl_O 1232.08 22.228 621.32 148.60 0.0000 891.54 14.696 552.11 2706.4 0.7922 1.39864 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1340.25 1.372 0.9135 3062.480 1.1033 0.9173 -28269.7 42.34 18.67 +LPC 141.73 1.925 0.8518 2915.541 1.2397 0.8647 -10022.5 26.84 15.70 +HPC 82.20 5.151 0.8652 6251.844 1.6596 0.8910 -35311.6 27.20 27.36 +HPT 27.37 2.740 0.9151 156.800 1.2422 0.9052 35311.6 +LPT 72.90 3.977 0.9213 74.497 1.3699 0.9074 38292.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2569.75 1.259 0.9438 0.776 1.9568 0.5215 1.4369 0.9679 3943.9586 +LPC 152.02 1.283 0.8873 0.796 1.6394 0.9323 3.2631 0.9600 3662.6571 +HPC 195.42 20.188 0.8535 0.983 2.1560 0.4206 0.2163 1.0137 6357.1603 +HPT 30.12 5.094 0.9335 102.409 5.0944 1.4085 0.4249 0.9803 1.5311 +LPT 151.48 5.152 0.9202 91.845 5.1523 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6179.77 20343.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 951.50 228.96 68.968 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 951.50 228.96 68.968 +Duct1 0.0025 0.3576 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 951.50 228.96 68.968 +Duct2 0.0025 0.4200 365.99 +Duct3 0.0050 0.3019 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3039 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.8897 1278.35 311.37 220.907 +Duct5 0.0075 0.4410 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.8267 1278.35 311.37 220.907 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 621.32 148.60 22.396 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.2590 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7618.7 24342.7 35311.6 +LP_Shaft 3191.0 63024.8 38292.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2360.90 0.9940 0.0550 3.12070 0.01742 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.513 0.9975 1.0000 0.9975 2706.36 0.792 910.2 34854.9 +Core_Nozz 1.284 0.9999 1.0000 0.9999 862.88 0.618 1055.5 6560.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 35 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 0.0 27.00 1264.02 14048.1 0.5612 7884.38 6.7881 458.05 10.534 2134.8 2085.1 1650.0 + core size:20.90 Q: 237.01 Maximum Thrust: 35120.3 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1264.02 16.408 563.13 134.62 0.0000 1179.64 14.696 545.67 5466.6 0.4000 1.39966 +FS_2 Inlet.Fl_O 1264.02 16.326 563.13 134.62 0.0000 1185.58 14.899 548.60 5943.4 0.3639 1.39966 +FS_21 Fan.Fl_O 1264.02 20.679 606.16 144.96 0.0000 971.11 18.536 587.54 4515.2 0.3985 1.39895 +FS_13 Splitter.Fl_O2 1101.72 20.679 606.16 144.96 0.0000 846.42 18.350 585.85 3795.6 0.4168 1.39895 +FS_22 Splitter.Fl_O1 162.30 20.679 606.16 144.96 0.0000 124.69 19.351 594.79 719.5 0.3095 1.39895 +FS_23 Duct1.Fl_O 162.30 20.627 606.16 144.96 0.0000 125.00 19.303 594.79 721.3 0.3095 1.39895 +FS_24 LPC.Fl_O 162.30 35.347 724.94 173.60 0.0000 79.78 31.569 702.08 366.0 0.4057 1.39519 +FS_25 Duct2.Fl_O 162.30 35.259 724.94 173.60 0.0000 79.98 31.490 702.08 366.9 0.4057 1.39519 +FS_3 HPC.Fl_O 162.30 172.851 1190.02 288.77 0.0000 20.90 161.587 1168.58 119.9 0.3150 1.36877 +FS_36 Bld3.Fl_O 147.69 172.851 1190.02 288.77 0.0000 19.02 161.587 1168.58 109.1 0.3150 1.36877 +FS_4 Burner.Fl_O 149.88 163.344 2134.80 551.88 0.0148 27.36 162.295 2131.52 483.4 0.0991 1.31316 +FS_45 HPT.Fl_O 164.49 59.077 1650.00 414.87 0.0135 72.98 55.598 1625.13 439.1 0.3027 1.33325 +FS_48 Duct3.Fl_O 164.49 58.781 1650.00 414.87 0.0135 73.35 55.320 1625.13 441.4 0.3027 1.33325 +FS_5 LPT.Fl_O 164.49 17.480 1247.98 307.17 0.0135 214.52 16.708 1233.27 1477.4 0.2587 1.35576 +FS_7 Duct4.Fl_O 164.49 17.305 1247.98 307.17 0.0135 216.68 16.898 1240.19 2018.9 0.1877 1.35576 +FS_9 Core_Nozz.Fl_O 164.49 17.305 1247.98 307.17 0.0135 216.68 14.696 1195.48 862.9 0.4954 1.35576 +FS_15 BypBld.Fl_O 1101.72 20.679 606.16 144.96 0.0000 846.42 18.350 585.85 3795.6 0.4168 1.39895 +FS_17 Duct5.Fl_O 1101.72 20.524 606.16 144.96 0.0000 852.81 18.213 585.85 3824.3 0.4168 1.39895 +FS_19 Byp_Nozz.Fl_O 1101.72 20.524 606.16 144.96 0.0000 852.81 14.696 551.03 2706.4 0.7077 1.39895 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1185.58 1.267 0.9133 2689.753 1.0764 0.9162 -18489.1 45.23 18.33 +LPC 125.00 1.714 0.8446 2592.516 1.1960 0.8559 -6577.4 28.65 13.44 +HPC 79.98 4.902 0.8642 6213.184 1.6415 0.8897 -26448.2 31.00 31.22 +HPT 27.36 2.765 0.9156 158.980 1.2507 0.9052 26448.3 +LPT 73.35 3.363 0.9125 68.997 1.3221 0.8987 25066.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2273.18 1.186 0.9435 0.682 1.9709 0.5215 1.4369 0.9679 3943.9586 +LPC 134.09 1.219 0.8798 0.708 1.6373 0.9323 3.2631 0.9600 3662.6571 +HPC 190.13 19.040 0.8525 0.977 2.1835 0.4206 0.2163 1.0137 6357.1603 +HPT 30.10 5.154 0.9340 103.832 5.1540 1.4085 0.4249 0.9803 1.5311 +LPT 152.42 4.296 0.9113 85.064 4.2960 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5466.58 17995.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 890.38 213.91 55.416 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 890.38 213.91 55.416 +Duct1 0.0025 0.3095 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 890.38 213.91 55.416 +Duct2 0.0025 0.4057 365.99 +Duct3 0.0050 0.3027 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2587 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.6806 1190.02 288.77 172.851 +Duct5 0.0075 0.4168 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.9266 1190.02 288.77 172.851 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 606.16 144.96 20.679 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.7881 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7345.5 18910.9 26448.3 +LP_Shaft 2802.7 46973.0 25066.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2134.80 0.9940 0.0550 2.19011 0.01483 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.397 0.9975 1.0000 0.9975 2706.36 0.708 812.3 27814.6 +Core_Nozz 1.178 0.9999 1.0000 0.9999 862.88 0.495 827.1 4228.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 36 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 0.0 27.00 1053.33 7024.1 0.6604 4638.57 7.5422 458.05 7.390 1828.5 1788.1 1402.6 + core size:21.47 Q: 237.01 Maximum Thrust: 35120.3 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1053.33 16.408 563.13 134.62 0.0000 983.02 14.696 545.67 4555.4 0.4000 1.39966 +FS_2 Inlet.Fl_O 1053.33 16.326 563.13 134.62 0.0000 987.96 15.367 553.48 5943.4 0.2953 1.39966 +FS_21 Fan.Fl_O 1053.33 18.837 588.98 140.83 0.0000 875.70 17.290 574.75 4515.2 0.3521 1.39921 +FS_13 Splitter.Fl_O2 930.02 18.837 588.98 140.83 0.0000 773.19 17.111 573.04 3795.6 0.3731 1.39921 +FS_22 Splitter.Fl_O1 123.31 18.837 588.98 140.83 0.0000 102.51 18.039 581.75 719.5 0.2494 1.39921 +FS_23 Duct1.Fl_O 123.31 18.790 588.98 140.83 0.0000 102.77 17.994 581.75 721.3 0.2494 1.39921 +FS_24 LPC.Fl_O 123.31 27.055 666.31 159.43 0.0000 75.92 24.472 647.56 366.0 0.3816 1.39721 +FS_25 Duct2.Fl_O 123.31 26.987 666.31 159.43 0.0000 76.11 24.411 647.56 366.9 0.3816 1.39721 +FS_3 HPC.Fl_O 123.31 121.255 1070.23 258.52 0.0000 21.47 112.885 1049.48 119.9 0.3238 1.37632 +FS_36 Bld3.Fl_O 112.21 121.255 1070.23 258.52 0.0000 19.54 112.885 1049.48 109.1 0.3238 1.37632 +FS_4 Burner.Fl_O 113.50 114.586 1828.48 463.28 0.0115 27.33 113.852 1825.58 483.4 0.0985 1.32657 +FS_45 HPT.Fl_O 124.60 41.027 1402.56 346.98 0.0104 73.39 38.583 1380.45 439.1 0.3028 1.34836 +FS_48 Duct3.Fl_O 124.60 40.821 1402.56 346.98 0.0104 73.76 38.390 1380.45 441.4 0.3028 1.34836 +FS_5 LPT.Fl_O 124.60 16.199 1130.64 276.08 0.0104 166.89 15.775 1122.65 1477.4 0.1974 1.36528 +FS_7 Duct4.Fl_O 124.60 16.037 1130.64 276.08 0.0104 168.58 15.811 1126.35 2018.9 0.1444 1.36528 +FS_9 Core_Nozz.Fl_O 124.60 16.037 1130.64 276.08 0.0104 168.58 14.696 1104.47 862.9 0.3596 1.36528 +FS_15 BypBld.Fl_O 930.02 18.837 588.98 140.83 0.0000 773.19 17.111 573.04 3795.6 0.3731 1.39921 +FS_17 Duct5.Fl_O 930.02 18.696 588.98 140.83 0.0000 779.03 16.983 573.04 3824.3 0.3731 1.39921 +FS_19 Byp_Nozz.Fl_O 930.02 18.696 588.98 140.83 0.0000 779.03 14.696 549.84 2706.4 0.5968 1.39921 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 987.96 1.154 0.9083 2152.842 1.0459 0.9102 -9252.4 54.62 16.42 +LPC 102.77 1.440 0.8334 2105.069 1.1313 0.8419 -3246.6 36.08 11.67 +HPC 76.11 4.493 0.8624 6141.768 1.6062 0.8875 -17286.8 37.76 38.25 +HPT 27.33 2.793 0.9165 162.795 1.2634 0.9056 17286.8 +LPT 73.76 2.520 0.8985 59.898 1.2405 0.8868 12498.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1894.29 1.107 0.9383 0.546 2.0743 0.5215 1.4369 0.9679 3943.9586 +LPC 110.24 1.135 0.8681 0.575 1.7207 0.9323 3.2631 0.9600 3662.6571 +HPC 180.93 17.148 0.8507 0.966 2.2455 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.220 0.9348 106.324 5.2200 1.4085 0.4249 0.9803 1.5311 +LPT 153.27 3.120 0.8974 73.846 3.1204 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4555.42 14995.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 809.44 194.11 40.798 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 809.44 194.11 40.798 +Duct1 0.0025 0.2494 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 809.44 194.11 40.798 +Duct2 0.0025 0.3816 365.99 +Duct3 0.0050 0.3028 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1974 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.3158 1070.23 258.52 121.255 +Duct5 0.0075 0.3731 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.7820 1070.23 258.52 121.255 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 588.98 140.83 18.837 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.5422 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6961.2 13042.5 17286.8 +LP_Shaft 2243.2 29264.2 12498.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1828.48 0.9940 0.0550 1.28849 0.01148 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.272 0.9975 1.0000 0.9975 2706.36 0.597 684.2 19778.3 +Core_Nozz 1.091 0.9999 1.0000 0.9999 862.88 0.360 578.9 2241.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 37 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 0.0 27.00 1757.28 32941.4 0.5801 19108.74 5.5726 572.56 18.578 2730.0 2662.6 2138.8 + core size:20.12 Q: 370.33 Maximum Thrust: 32941.4 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1757.28 17.432 572.94 136.97 0.0000 1557.08 14.696 545.67 6079.8 0.5000 1.39948 +FS_2 Inlet.Fl_O 1757.28 17.344 572.94 136.97 0.0000 1564.92 14.423 543.54 5943.4 0.5201 1.39948 +FS_21 Fan.Fl_O 1757.28 26.765 656.27 157.01 0.0000 1085.33 23.166 629.84 4515.2 0.4591 1.39759 +FS_13 Splitter.Fl_O2 1489.91 26.765 656.27 157.01 0.0000 920.20 23.092 629.26 3795.6 0.4643 1.39759 +FS_22 Splitter.Fl_O1 267.37 26.765 656.27 157.01 0.0000 165.13 23.541 632.72 719.5 0.4324 1.39759 +FS_23 Duct1.Fl_O 267.37 26.698 656.27 157.01 0.0000 165.54 23.483 632.72 721.3 0.4324 1.39759 +FS_24 LPC.Fl_O 267.37 59.585 850.21 204.07 0.0000 84.43 52.314 819.71 366.0 0.4365 1.38957 +FS_25 Duct2.Fl_O 267.37 59.436 850.21 204.07 0.0000 84.64 52.183 819.71 366.9 0.4365 1.38957 +FS_3 HPC.Fl_O 267.37 323.848 1425.70 349.63 0.0000 20.12 304.405 1402.76 119.9 0.3034 1.35442 +FS_36 Bld3.Fl_O 243.30 323.848 1425.70 349.63 0.0000 18.31 304.405 1402.76 109.1 0.3034 1.35442 +FS_4 Burner.Fl_O 248.61 306.036 2730.00 732.78 0.0218 27.39 304.065 2725.99 483.4 0.1000 1.29407 +FS_45 HPT.Fl_O 272.67 113.364 2138.83 556.23 0.0199 71.78 106.914 2109.39 439.1 0.3000 1.30961 +FS_48 Duct3.Fl_O 272.67 112.797 2138.83 556.23 0.0199 72.14 106.379 2109.39 441.4 0.3000 1.30961 +FS_5 LPT.Fl_O 272.67 24.073 1516.91 380.95 0.0199 284.68 22.115 1484.85 1477.4 0.3581 1.33572 +FS_7 Duct4.Fl_O 272.67 23.832 1516.91 380.95 0.0199 287.55 22.821 1500.46 2018.9 0.2553 1.33572 +FS_9 Core_Nozz.Fl_O 272.67 23.832 1516.91 380.95 0.0199 287.55 14.696 1341.62 862.9 0.8742 1.33572 +FS_15 BypBld.Fl_O 1489.91 26.765 656.27 157.01 0.0000 920.20 23.092 629.26 3795.6 0.4643 1.39759 +FS_17 Duct5.Fl_O 1489.91 26.564 656.27 157.01 0.0000 927.16 22.918 629.26 3824.3 0.4643 1.39759 +FS_19 Byp_Nozz.Fl_O 1489.91 26.564 656.27 157.01 0.0000 927.16 14.696 554.32 2706.4 0.9599 1.39759 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1564.92 1.543 0.9051 3568.594 1.1454 0.9108 -49823.4 33.06 18.51 +LPC 165.54 2.232 0.8620 3334.357 1.2955 0.8765 -17799.3 27.75 19.91 +HPC 84.64 5.449 0.8651 6302.505 1.6769 0.8915 -55064.6 22.81 22.90 +HPT 27.39 2.700 0.9146 154.436 1.2303 0.9052 55064.8 +LPT 72.14 4.686 0.9274 81.100 1.4100 0.9131 67622.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3000.52 1.378 0.9351 0.905 2.0703 0.5215 1.4369 0.9679 3943.9586 +LPC 177.57 1.377 0.8979 0.910 1.7040 0.9323 3.2631 0.9600 3662.6571 +HPC 201.22 21.565 0.8535 0.991 2.1044 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.000 0.9330 100.865 5.0002 1.4085 0.4249 0.9803 1.5311 +LPT 149.90 6.141 0.9262 99.986 6.1414 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6079.85 31272.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1056.24 255.01 98.172 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1056.24 255.01 98.172 +Duct1 0.0025 0.4324 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1056.24 255.01 98.172 +Duct2 0.0025 0.4365 365.99 +Duct3 0.0050 0.3000 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3581 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 9.3578 1425.70 349.63 323.848 +Duct5 0.0075 0.4643 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 14.7051 1425.70 349.63 323.848 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 656.27 157.01 26.765 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5726 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 8069.2 35840.8 55064.8 +LP_Shaft 3750.7 94693.5 67622.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.00 0.9940 0.0550 5.30798 0.02182 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.808 0.9975 1.0000 0.9975 2706.36 0.960 1105.1 51173.4 +Core_Nozz 1.622 0.9999 1.0000 0.9999 862.88 0.874 1538.7 13040.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 38 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 0.0 27.00 1704.92 29647.3 0.5786 17153.08 5.7485 572.56 17.265 2645.3 2580.5 2069.1 + core size:20.24 Q: 370.33 Maximum Thrust: 32941.4 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1704.92 17.432 572.94 136.97 0.0000 1510.69 14.696 545.67 5898.7 0.5000 1.39948 +FS_2 Inlet.Fl_O 1704.92 17.344 572.94 136.97 0.0000 1518.30 14.638 545.85 5943.4 0.4983 1.39948 +FS_21 Fan.Fl_O 1704.92 26.028 650.24 155.56 0.0000 1077.85 22.586 624.50 4515.2 0.4549 1.39781 +FS_13 Splitter.Fl_O2 1452.29 26.028 650.24 155.56 0.0000 918.14 22.475 623.62 3795.6 0.4629 1.39781 +FS_22 Splitter.Fl_O1 252.64 26.028 650.24 155.56 0.0000 159.72 23.127 628.73 719.5 0.4145 1.39781 +FS_23 Duct1.Fl_O 252.64 25.963 650.24 155.56 0.0000 160.12 23.069 628.73 721.3 0.4145 1.39781 +FS_24 LPC.Fl_O 252.64 56.363 835.78 200.54 0.0000 83.62 49.639 806.47 366.0 0.4311 1.39025 +FS_25 Duct2.Fl_O 252.64 56.222 835.78 200.54 0.0000 83.83 49.515 806.47 366.9 0.4311 1.39025 +FS_3 HPC.Fl_O 252.64 300.957 1395.68 341.78 0.0000 20.24 282.655 1372.84 119.9 0.3053 1.35615 +FS_36 Bld3.Fl_O 229.90 300.957 1395.68 341.78 0.0000 18.42 282.655 1372.84 109.1 0.3053 1.35615 +FS_4 Burner.Fl_O 234.67 284.405 2645.27 706.31 0.0207 27.38 282.574 2641.37 483.4 0.0998 1.29644 +FS_45 HPT.Fl_O 257.40 105.070 2069.13 535.49 0.0189 71.91 99.070 2040.34 439.1 0.3003 1.31249 +FS_48 Duct3.Fl_O 257.40 104.545 2069.13 535.49 0.0189 72.27 98.575 2040.34 441.4 0.3003 1.31249 +FS_5 LPT.Fl_O 257.40 22.745 1471.37 368.23 0.0189 280.12 20.960 1441.20 1477.4 0.3509 1.33882 +FS_7 Duct4.Fl_O 257.40 22.517 1471.37 368.23 0.0189 282.95 21.594 1455.85 2018.9 0.2506 1.33882 +FS_9 Core_Nozz.Fl_O 257.40 22.517 1471.37 368.23 0.0189 282.95 14.696 1319.42 862.9 0.8178 1.33882 +FS_15 BypBld.Fl_O 1452.29 26.028 650.24 155.56 0.0000 918.14 22.475 623.62 3795.6 0.4629 1.39781 +FS_17 Duct5.Fl_O 1452.29 25.832 650.24 155.56 0.0000 925.07 22.306 623.62 3824.3 0.4629 1.39781 +FS_19 Byp_Nozz.Fl_O 1452.29 25.832 650.24 155.56 0.0000 925.07 14.696 553.61 2706.4 0.9351 1.39781 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1518.30 1.501 0.9093 3461.404 1.1349 0.9144 -44836.4 36.22 18.97 +LPC 160.12 2.171 0.8593 3249.157 1.2853 0.8736 -16077.7 27.04 18.58 +HPC 83.83 5.353 0.8655 6284.503 1.6699 0.8916 -50485.4 24.12 24.23 +HPT 27.38 2.707 0.9148 155.109 1.2328 0.9052 50485.3 +LPT 72.27 4.596 0.9256 79.978 1.4063 0.9109 60914.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2911.14 1.348 0.9394 0.878 2.0362 0.5215 1.4369 0.9679 3943.9586 +LPC 171.75 1.359 0.8950 0.887 1.6758 0.9323 3.2631 0.9600 3662.6571 +HPC 199.29 21.123 0.8538 0.989 2.1192 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.017 0.9331 101.304 5.0172 1.4085 0.4249 0.9803 1.5311 +LPT 150.17 6.017 0.9244 98.602 6.0169 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5898.71 30340.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1036.08 249.97 92.076 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1036.08 249.97 92.076 +Duct1 0.0025 0.4145 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1036.08 249.97 92.076 +Duct2 0.0025 0.4311 365.99 +Duct3 0.0050 0.3003 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3509 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.8424 1395.68 341.78 300.957 +Duct5 0.0075 0.4629 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 13.8951 1395.68 341.78 300.957 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 650.24 155.56 26.028 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.7485 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7977.6 33237.5 50485.3 +LP_Shaft 3638.0 87940.8 60914.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2645.27 0.9940 0.0550 4.76475 0.02073 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.758 0.9975 1.0000 0.9975 2706.36 0.935 1075.8 48559.1 +Core_Nozz 1.532 0.9999 1.0000 0.9999 862.88 0.818 1428.5 11428.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 39 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 0.0 27.00 1648.25 26353.2 0.5798 15279.79 5.9424 572.56 15.945 2559.2 2497.1 1998.4 + core size:20.36 Q: 370.33 Maximum Thrust: 32941.4 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1648.25 17.432 572.94 136.97 0.0000 1460.48 14.696 545.67 5702.6 0.5000 1.39948 +FS_2 Inlet.Fl_O 1648.25 17.344 572.94 136.97 0.0000 1467.83 14.855 548.15 5943.4 0.4757 1.39948 +FS_21 Fan.Fl_O 1648.25 25.260 644.07 154.08 0.0000 1068.60 21.988 619.12 4515.2 0.4498 1.39801 +FS_13 Splitter.Fl_O2 1410.83 25.260 644.07 154.08 0.0000 914.68 21.843 617.95 3795.6 0.4606 1.39801 +FS_22 Splitter.Fl_O1 237.42 25.260 644.07 154.08 0.0000 153.92 22.674 624.56 719.5 0.3960 1.39801 +FS_23 Duct1.Fl_O 237.42 25.197 644.07 154.08 0.0000 154.31 22.617 624.56 721.3 0.3960 1.39801 +FS_24 LPC.Fl_O 237.42 52.999 820.33 196.77 0.0000 82.79 46.822 792.22 366.0 0.4256 1.39097 +FS_25 Duct2.Fl_O 237.42 52.866 820.33 196.77 0.0000 83.00 46.705 792.22 366.9 0.4256 1.39097 +FS_3 HPC.Fl_O 237.42 277.939 1364.26 333.59 0.0000 20.36 260.817 1341.55 119.9 0.3071 1.35801 +FS_36 Bld3.Fl_O 216.05 277.939 1364.26 333.59 0.0000 18.53 260.817 1341.55 109.1 0.3071 1.35801 +FS_4 Burner.Fl_O 220.30 262.653 2559.17 679.65 0.0196 27.38 260.963 2555.37 483.4 0.0997 1.29904 +FS_45 HPT.Fl_O 241.66 96.738 1998.44 514.64 0.0179 72.06 91.190 1970.29 439.1 0.3006 1.31559 +FS_48 Duct3.Fl_O 241.66 96.254 1998.44 514.64 0.0179 72.42 90.734 1970.29 441.4 0.3006 1.31559 +FS_5 LPT.Fl_O 241.66 21.538 1427.47 356.05 0.0179 273.56 19.934 1399.56 1477.4 0.3410 1.34193 +FS_7 Duct4.Fl_O 241.66 21.322 1427.47 356.05 0.0179 276.32 20.491 1413.06 2018.9 0.2440 1.34193 +FS_9 Core_Nozz.Fl_O 241.66 21.322 1427.47 356.05 0.0179 276.32 14.696 1297.27 862.9 0.7607 1.34193 +FS_15 BypBld.Fl_O 1410.83 25.260 644.07 154.08 0.0000 914.68 21.843 617.95 3795.6 0.4606 1.39801 +FS_17 Duct5.Fl_O 1410.83 25.070 644.07 154.08 0.0000 921.59 21.679 617.95 3824.3 0.4606 1.39801 +FS_19 Byp_Nozz.Fl_O 1410.83 25.070 644.07 154.08 0.0000 921.59 14.696 553.05 2706.4 0.9079 1.39801 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1467.83 1.456 0.9114 3344.935 1.1242 0.9160 -39882.7 39.42 19.35 +LPC 154.31 2.103 0.8561 3154.824 1.2737 0.8703 -14341.7 26.37 17.31 +HPC 83.00 5.257 0.8656 6267.452 1.6630 0.8916 -45960.6 25.45 25.59 +HPT 27.38 2.715 0.9149 155.809 1.2354 0.9050 45960.6 +LPT 72.42 4.469 0.9238 78.642 1.4000 0.9091 54224.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2814.37 1.318 0.9416 0.848 2.0184 0.5215 1.4369 0.9679 3943.9586 +LPC 165.52 1.338 0.8918 0.861 1.6490 0.9323 3.2631 0.9600 3662.6571 +HPC 197.32 20.681 0.8539 0.986 2.1325 0.4206 0.2163 1.0137 6357.1603 +HPT 30.12 5.037 0.9332 101.761 5.0366 1.4085 0.4249 0.9803 1.5311 +LPT 150.49 5.839 0.9226 96.955 5.8393 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5702.64 29331.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1014.76 244.66 85.840 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1014.76 244.66 85.840 +Duct1 0.0025 0.3960 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1014.76 244.66 85.840 +Duct2 0.0025 0.4256 365.99 +Duct3 0.0050 0.3006 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3410 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.3097 1364.26 333.59 277.939 +Duct5 0.0075 0.4606 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 13.0581 1364.26 333.59 277.939 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 644.07 154.08 25.260 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9424 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7882.1 30625.2 45960.6 +LP_Shaft 3515.6 81008.7 54224.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2559.17 0.9940 0.0550 4.24439 0.01965 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.706 0.9975 1.0000 0.9975 2706.36 0.908 1044.0 45780.5 +Core_Nozz 1.451 0.9999 1.0000 0.9999 862.88 0.761 1318.6 9904.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 40 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 0.0 27.00 1520.77 19764.9 0.5916 11693.87 6.4089 572.56 13.249 2372.5 2316.1 1845.1 + core size:20.63 Q: 370.33 Maximum Thrust: 32941.4 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1520.77 17.432 572.94 136.97 0.0000 1347.52 14.696 545.67 5261.6 0.5000 1.39948 +FS_2 Inlet.Fl_O 1520.77 17.344 572.94 136.97 0.0000 1354.30 15.290 552.69 5943.4 0.4282 1.39948 +FS_21 Fan.Fl_O 1520.77 23.644 630.92 150.91 0.0000 1042.52 20.755 607.92 4515.2 0.4356 1.39840 +FS_13 Splitter.Fl_O2 1315.51 23.644 630.92 150.91 0.0000 901.81 20.553 606.22 3795.6 0.4520 1.39840 +FS_22 Splitter.Fl_O1 205.26 23.644 630.92 150.91 0.0000 140.71 21.666 615.41 719.5 0.3556 1.39840 +FS_23 Duct1.Fl_O 205.26 23.585 630.92 150.91 0.0000 141.07 21.612 615.41 721.3 0.3556 1.39840 +FS_24 LPC.Fl_O 205.26 45.740 784.35 188.01 0.0000 81.10 40.660 758.72 366.0 0.4144 1.39270 +FS_25 Duct2.Fl_O 205.26 45.626 784.35 188.01 0.0000 81.30 40.559 758.72 366.9 0.4144 1.39270 +FS_3 HPC.Fl_O 205.26 230.946 1293.78 315.35 0.0000 20.63 216.312 1271.42 119.9 0.3112 1.36228 +FS_36 Bld3.Fl_O 186.79 230.946 1293.78 315.35 0.0000 18.77 216.312 1271.42 109.1 0.3112 1.36228 +FS_4 Burner.Fl_O 190.04 218.244 2372.46 622.67 0.0174 27.37 216.841 2368.89 483.4 0.0995 1.30489 +FS_45 HPT.Fl_O 208.51 79.742 1845.07 470.09 0.0158 72.48 75.113 1818.30 439.1 0.3016 1.32289 +FS_48 Duct3.Fl_O 208.51 79.343 1845.07 470.09 0.0158 72.84 74.737 1818.30 441.4 0.3016 1.32289 +FS_5 LPT.Fl_O 208.51 19.447 1339.56 331.93 0.0158 253.22 18.224 1317.23 1477.4 0.3115 1.34851 +FS_7 Duct4.Fl_O 208.51 19.253 1339.56 331.93 0.0158 255.78 18.614 1327.92 2018.9 0.2241 1.34851 +FS_9 Core_Nozz.Fl_O 208.51 19.253 1339.56 331.93 0.0158 255.78 14.696 1248.69 862.9 0.6429 1.34851 +FS_15 BypBld.Fl_O 1315.51 23.644 630.92 150.91 0.0000 901.81 20.553 606.22 3795.6 0.4520 1.39840 +FS_17 Duct5.Fl_O 1315.51 23.467 630.92 150.91 0.0000 908.62 20.398 606.22 3824.3 0.4520 1.39840 +FS_19 Byp_Nozz.Fl_O 1315.51 23.467 630.92 150.91 0.0000 908.62 14.696 552.05 2706.4 0.8458 1.39840 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1354.30 1.363 0.9130 3066.091 1.1012 0.9168 -29986.0 44.40 19.92 +LPC 141.07 1.939 0.8498 2921.816 1.2432 0.8629 -10774.0 25.63 14.96 +HPC 81.30 5.062 0.8652 6235.712 1.6495 0.8908 -36981.4 28.35 28.53 +HPT 27.37 2.737 0.9152 157.433 1.2417 0.9053 36981.5 +LPT 72.84 4.080 0.9209 75.022 1.3774 0.9066 40760.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2596.69 1.253 0.9432 0.777 2.0118 0.5215 1.4369 0.9679 3943.9586 +LPC 151.31 1.288 0.8851 0.798 1.6112 0.9323 3.2631 0.9600 3662.6571 +HPC 193.29 19.777 0.8535 0.981 2.1589 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.088 0.9336 102.822 5.0880 1.4085 0.4249 0.9803 1.5311 +LPT 151.36 5.296 0.9197 92.493 5.2963 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5261.57 27063.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 966.11 232.58 72.775 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 966.11 232.58 72.775 +Duct1 0.0025 0.3556 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 966.11 232.58 72.775 +Duct2 0.0025 0.4144 365.99 +Duct3 0.0050 0.3016 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3115 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.1842 1293.78 315.35 230.946 +Duct5 0.0075 0.4520 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.2895 1293.78 315.35 230.946 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 630.92 150.91 23.644 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.4089 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7668.3 25329.2 36981.5 +LP_Shaft 3222.5 66431.3 40760.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2372.46 0.9940 0.0550 3.24830 0.01739 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.597 0.9975 1.0000 0.9975 2706.36 0.846 971.7 39730.7 +Core_Nozz 1.310 0.9999 1.0000 0.9999 862.88 0.643 1095.2 7097.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 41 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 8/ 18/ 1/ 6 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 0.0 27.00 1368.33 13176.6 0.6304 8307.09 7.0092 572.56 10.483 2152.2 2102.5 1665.0 + core size:20.98 Q: 370.33 Maximum Thrust: 32941.4 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1368.33 17.432 572.94 136.97 0.0000 1212.45 14.696 545.67 4734.2 0.5000 1.39948 +FS_2 Inlet.Fl_O 1368.33 17.344 572.94 136.97 0.0000 1218.55 15.732 557.20 5943.4 0.3760 1.39948 +FS_21 Fan.Fl_O 1368.33 21.901 616.21 147.37 0.0000 1000.81 19.468 595.87 4515.2 0.4137 1.39875 +FS_13 Splitter.Fl_O2 1197.48 21.901 616.21 147.37 0.0000 875.85 19.229 593.77 3795.6 0.4352 1.39875 +FS_22 Splitter.Fl_O1 170.84 21.901 616.21 147.37 0.0000 124.96 20.487 604.60 719.5 0.3102 1.39875 +FS_23 Duct1.Fl_O 170.84 21.846 616.21 147.37 0.0000 125.27 20.436 604.60 721.3 0.3102 1.39875 +FS_24 LPC.Fl_O 170.84 38.069 741.26 177.55 0.0000 78.84 34.107 718.55 366.0 0.3999 1.39460 +FS_25 Duct2.Fl_O 170.84 37.973 741.26 177.55 0.0000 79.04 34.022 718.55 366.9 0.3999 1.39460 +FS_3 HPC.Fl_O 170.84 182.726 1209.00 293.61 0.0000 20.98 170.723 1187.09 119.9 0.3165 1.36758 +FS_36 Bld3.Fl_O 155.47 182.726 1209.00 293.61 0.0000 19.09 170.723 1187.09 109.1 0.3165 1.36758 +FS_4 Burner.Fl_O 157.78 172.676 2152.17 556.89 0.0148 27.35 171.567 2148.87 483.4 0.0991 1.31263 +FS_45 HPT.Fl_O 173.15 62.531 1665.00 419.00 0.0135 72.91 58.857 1639.99 439.1 0.3025 1.33252 +FS_48 Duct3.Fl_O 173.15 62.219 1665.00 419.00 0.0135 73.28 58.562 1639.99 441.4 0.3025 1.33252 +FS_5 LPT.Fl_O 173.15 17.769 1247.51 307.05 0.0135 222.09 16.925 1231.66 1477.4 0.2686 1.35578 +FS_7 Duct4.Fl_O 173.15 17.592 1247.51 307.05 0.0135 224.33 17.147 1239.15 2018.9 0.1947 1.35578 +FS_9 Core_Nozz.Fl_O 173.15 17.592 1247.51 307.05 0.0135 224.33 14.696 1189.86 862.9 0.5202 1.35578 +FS_15 BypBld.Fl_O 1197.48 21.901 616.21 147.37 0.0000 875.85 19.229 593.77 3795.6 0.4352 1.39875 +FS_17 Duct5.Fl_O 1197.48 21.736 616.21 147.37 0.0000 882.47 19.085 593.77 3824.3 0.4352 1.39875 +FS_19 Byp_Nozz.Fl_O 1197.48 21.736 616.21 147.37 0.0000 882.47 14.696 551.07 2706.4 0.7692 1.39875 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1218.55 1.263 0.9112 2720.556 1.0755 0.9141 -20129.8 48.43 20.22 +LPC 125.27 1.743 0.8424 2623.302 1.2029 0.8541 -7294.7 26.76 12.75 +HPC 79.04 4.812 0.8639 6198.414 1.6310 0.8891 -28053.8 32.27 32.52 +HPT 27.35 2.761 0.9157 159.728 1.2500 0.9053 28053.8 +LPT 73.28 3.501 0.9139 70.075 1.3347 0.8998 27424.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2336.40 1.183 0.9413 0.690 2.0549 0.5215 1.4369 0.9679 3943.9586 +LPC 134.37 1.228 0.8775 0.716 1.5997 0.9323 3.2631 0.9600 3662.6571 +HPC 187.91 18.622 0.8523 0.975 2.1850 0.4206 0.2163 1.0137 6357.1603 +HPT 30.09 5.146 0.9341 104.321 5.1457 1.4085 0.4249 0.9803 1.5311 +LPT 152.26 4.489 0.9127 86.393 4.4895 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4734.16 24350.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 907.72 218.17 59.180 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 907.72 218.17 59.180 +Duct1 0.0025 0.3102 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 907.72 218.17 59.180 +Duct2 0.0025 0.3999 365.99 +Duct3 0.0050 0.3025 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2686 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.9795 1209.00 293.61 182.726 +Duct5 0.0075 0.4352 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.3964 1209.00 293.61 182.726 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 616.21 147.37 21.901 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.0092 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7410.0 19884.1 28053.8 +LP_Shaft 2859.4 50373.5 27424.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2152.17 0.9940 0.0550 2.30753 0.01484 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.479 0.9975 1.0000 0.9975 2706.36 0.769 883.0 32863.2 +Core_Nozz 1.197 0.9999 1.0000 0.9999 862.88 0.520 866.6 4663.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 42 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 0.0 27.00 1176.46 6588.1 0.7611 5014.00 7.9180 572.56 7.503 1857.4 1816.8 1426.5 + core size:21.53 Q: 370.33 Maximum Thrust: 32941.4 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1176.46 17.432 572.94 136.97 0.0000 1042.43 14.696 545.67 4070.3 0.5000 1.39948 +FS_2 Inlet.Fl_O 1176.46 17.344 572.94 136.97 0.0000 1047.68 16.188 561.77 5943.4 0.3154 1.39948 +FS_21 Fan.Fl_O 1176.46 20.011 599.55 143.37 0.0000 928.90 18.136 582.95 4515.2 0.3776 1.39905 +FS_13 Splitter.Fl_O2 1044.54 20.011 599.55 143.37 0.0000 824.74 17.888 580.67 3795.6 0.4035 1.39905 +FS_22 Splitter.Fl_O1 131.92 20.011 599.55 143.37 0.0000 104.16 19.135 591.94 719.5 0.2538 1.39905 +FS_23 Duct1.Fl_O 131.92 19.961 599.55 143.37 0.0000 104.42 19.087 591.94 721.3 0.2538 1.39905 +FS_24 LPC.Fl_O 131.92 29.607 685.02 163.95 0.0000 75.25 26.836 666.16 366.0 0.3777 1.39653 +FS_25 Duct2.Fl_O 131.92 29.533 685.02 163.95 0.0000 75.44 26.769 666.16 366.9 0.3777 1.39653 +FS_3 HPC.Fl_O 131.92 130.783 1094.52 264.62 0.0000 21.53 121.694 1073.21 119.9 0.3251 1.37479 +FS_36 Bld3.Fl_O 120.05 130.783 1094.52 264.62 0.0000 19.60 121.694 1073.21 109.1 0.3251 1.37479 +FS_4 Burner.Fl_O 121.44 123.590 1857.42 471.41 0.0116 27.33 122.798 1854.49 483.4 0.0985 1.32529 +FS_45 HPT.Fl_O 133.31 44.291 1426.48 353.37 0.0106 73.36 41.656 1404.09 439.1 0.3028 1.34690 +FS_48 Duct3.Fl_O 133.31 44.069 1426.48 353.37 0.0106 73.73 41.447 1404.09 441.4 0.3028 1.34690 +FS_5 LPT.Fl_O 133.31 16.399 1132.58 276.60 0.0106 176.54 15.917 1123.57 1477.4 0.2094 1.36508 +FS_7 Duct4.Fl_O 133.31 16.235 1132.58 276.60 0.0106 178.32 15.978 1127.76 2018.9 0.1529 1.36508 +FS_9 Core_Nozz.Fl_O 133.31 16.235 1132.58 276.60 0.0106 178.32 14.696 1102.73 863.0 0.3844 1.36508 +FS_15 BypBld.Fl_O 1044.54 20.011 599.55 143.37 0.0000 824.74 17.888 580.67 3795.6 0.4035 1.39905 +FS_17 Duct5.Fl_O 1044.54 19.861 599.55 143.37 0.0000 830.97 17.754 580.67 3824.3 0.4035 1.39905 +FS_19 Byp_Nozz.Fl_O 1044.54 19.861 599.55 143.37 0.0000 830.97 14.696 550.14 2706.4 0.6704 1.39905 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1047.68 1.154 0.8973 2223.772 1.0464 0.8994 -10639.2 59.20 19.50 +LPC 104.42 1.483 0.8330 2173.873 1.1426 0.8422 -3841.7 32.75 11.03 +HPC 75.44 4.428 0.8620 6129.230 1.5978 0.8870 -18789.7 38.82 39.37 +HPT 27.33 2.790 0.9166 163.440 1.2623 0.9058 18789.8 +LPT 73.73 2.687 0.9015 61.882 1.2595 0.8892 14481.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2008.79 1.107 0.9270 0.564 2.1995 0.5215 1.4369 0.9679 3943.9586 +LPC 112.01 1.148 0.8677 0.594 1.6635 0.9323 3.2631 0.9600 3662.6571 +HPC 179.35 16.849 0.8504 0.964 2.2565 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.214 0.9350 106.745 5.2140 1.4085 0.4249 0.9803 1.5311 +LPT 153.20 3.354 0.9004 76.293 3.3538 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4070.33 20935.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 830.22 199.18 44.366 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 830.22 199.18 44.366 +Duct1 0.0025 0.2538 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 830.22 199.18 44.366 +Duct2 0.0025 0.3777 365.99 +Duct3 0.0050 0.3028 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2094 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.6172 1094.52 264.62 130.783 +Duct5 0.0075 0.4035 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.2556 1094.52 264.62 130.783 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 599.55 143.37 20.011 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.9180 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7043.9 14010.2 18789.8 +LP_Shaft 2337.2 32541.1 14481.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1857.42 0.9940 0.0550 1.39278 0.01160 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.351 0.9975 1.0000 0.9975 2706.36 0.670 768.9 24962.3 +Core_Nozz 1.105 0.9999 1.0000 0.9999 862.88 0.384 618.3 2561.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 43 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 2000.0 27.00 1459.69 47779.6 0.3590 17153.14 5.2220 0.00 20.797 2730.0 2661.2 2138.1 + core size:19.89 Q: 0.00 Maximum Thrust: 47779.6 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1459.69 13.664 538.54 128.72 0.0000 1599.68 13.664 538.54 -----.- 0.0000 1.40014 +FS_2 Inlet.Fl_O 1459.69 13.555 538.54 128.72 0.0000 1612.58 11.087 508.46 5943.4 0.5435 1.40014 +FS_21 Fan.Fl_O 1459.69 21.954 626.77 149.91 0.0000 1074.11 19.075 602.15 4515.2 0.4528 1.39851 +FS_13 Splitter.Fl_O2 1225.09 21.954 626.77 149.91 0.0000 901.48 19.086 602.25 3795.6 0.4518 1.39851 +FS_22 Splitter.Fl_O1 234.60 21.954 626.77 149.91 0.0000 172.63 19.016 601.61 719.5 0.4578 1.39851 +FS_23 Duct1.Fl_O 234.60 21.899 626.77 149.91 0.0000 173.06 18.969 601.61 721.3 0.4578 1.39851 +FS_24 LPC.Fl_O 234.60 49.998 817.37 196.05 0.0000 86.56 43.526 786.08 366.0 0.4506 1.39111 +FS_25 Duct2.Fl_O 234.60 49.873 817.37 196.05 0.0000 86.78 43.418 786.08 366.9 0.4506 1.39111 +FS_3 HPC.Fl_O 234.60 284.177 1393.78 341.29 0.0000 19.89 267.530 1371.83 119.9 0.2994 1.35626 +FS_36 Bld3.Fl_O 213.49 284.177 1393.78 341.29 0.0000 18.10 267.530 1371.83 109.1 0.2994 1.35626 +FS_4 Burner.Fl_O 218.25 268.547 2730.00 733.24 0.0223 27.40 266.816 2725.99 483.4 0.1000 1.29373 +FS_45 HPT.Fl_O 239.37 99.666 2138.14 556.32 0.0203 71.66 94.016 2108.83 439.1 0.2995 1.30933 +FS_48 Duct3.Fl_O 239.37 99.167 2138.14 556.32 0.0203 72.02 93.546 2108.83 441.4 0.2995 1.30933 +FS_5 LPT.Fl_O 239.37 21.416 1519.62 381.86 0.0203 281.15 19.722 1488.44 1477.4 0.3530 1.33528 +FS_7 Duct4.Fl_O 239.37 21.202 1519.62 381.86 0.0203 283.99 20.326 1503.59 2018.9 0.2520 1.33528 +FS_9 Core_Nozz.Fl_O 239.37 21.202 1519.62 381.86 0.0203 283.99 13.664 1359.50 862.9 0.8312 1.33528 +FS_15 BypBld.Fl_O 1225.09 21.954 626.77 149.91 0.0000 901.48 19.086 602.25 3795.6 0.4518 1.39851 +FS_17 Duct5.Fl_O 1225.09 21.790 626.77 149.91 0.0000 908.29 18.943 602.25 3824.3 0.4518 1.39851 +FS_19 Byp_Nozz.Fl_O 1225.09 21.790 626.77 149.91 0.0000 908.29 13.664 548.62 2706.4 0.8445 1.39851 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1612.58 1.620 0.9007 3705.970 1.1638 0.9072 -43772.1 26.93 16.15 +LPC 173.06 2.283 0.8665 3435.236 1.3041 0.8809 -15313.7 29.99 22.76 +HPC 86.78 5.698 0.8621 6362.154 1.7052 0.8898 -48208.7 19.64 19.62 +HPT 27.40 2.694 0.9142 152.857 1.2295 0.9048 48208.6 +LPT 72.02 4.631 0.9291 81.667 1.4070 0.9153 59085.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3091.90 1.431 0.9305 0.940 2.0359 0.5215 1.4369 0.9679 3943.9586 +LPC 185.63 1.393 0.9025 0.938 1.7746 0.9323 3.2631 0.9600 3662.6571 +HPC 206.31 22.718 0.8505 1.001 2.0714 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.988 0.9326 99.834 4.9881 1.4085 0.4249 0.9803 1.5311 +LPT 149.65 6.064 0.9279 100.685 6.0645 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1023.68 246.88 84.199 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1023.68 246.88 84.199 +Duct1 0.0025 0.4578 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1023.68 246.88 84.199 +Duct2 0.0025 0.4506 365.99 +Duct3 0.0050 0.2995 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3530 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.2110 1393.78 341.29 284.177 +Duct5 0.0075 0.4518 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.9031 1393.78 341.29 284.177 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 626.77 149.91 21.954 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.2220 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7986.7 31702.4 48208.6 +LP_Shaft 3776.3 82177.7 59085.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.00 0.9940 0.0550 4.76476 0.02232 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.595 0.9975 1.0000 0.9975 2706.36 0.844 967.2 36828.1 +Core_Nozz 1.552 0.9999 1.0000 0.9999 862.88 0.831 1472.0 10951.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 44 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 2000.0 27.00 1392.32 43002.6 0.3477 14952.57 5.3881 0.00 18.914 2622.1 2556.5 2048.6 + core size:20.03 Q: 0.00 Maximum Thrust: 47779.6 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1392.32 13.664 538.54 128.72 0.0000 1525.84 13.664 538.54 -----.- 0.0000 1.40014 +FS_2 Inlet.Fl_O 1392.32 13.555 538.54 128.72 0.0000 1538.15 11.370 512.14 5943.4 0.5073 1.40014 +FS_21 Fan.Fl_O 1392.32 21.168 619.04 148.05 0.0000 1055.99 18.503 595.73 4515.2 0.4428 1.39869 +FS_13 Splitter.Fl_O2 1174.37 21.168 619.04 148.05 0.0000 890.69 18.481 595.54 3795.6 0.4448 1.39869 +FS_22 Splitter.Fl_O1 217.95 21.168 619.04 148.05 0.0000 165.31 18.613 596.74 719.5 0.4328 1.39869 +FS_23 Duct1.Fl_O 217.95 21.115 619.04 148.05 0.0000 165.72 18.566 596.74 721.3 0.4328 1.39869 +FS_24 LPC.Fl_O 217.95 46.208 797.24 191.14 0.0000 85.94 40.329 767.22 366.0 0.4462 1.39208 +FS_25 Duct2.Fl_O 217.95 46.092 797.24 191.14 0.0000 86.15 40.229 767.22 366.9 0.4462 1.39208 +FS_3 HPC.Fl_O 217.95 258.450 1354.53 331.07 0.0000 20.03 243.082 1332.76 119.9 0.3015 1.35859 +FS_36 Bld3.Fl_O 198.34 258.450 1354.53 331.07 0.0000 18.23 243.082 1332.76 109.1 0.3015 1.35859 +FS_4 Burner.Fl_O 202.49 244.235 2622.05 699.54 0.0209 27.39 242.662 2618.18 483.4 0.0999 1.29678 +FS_45 HPT.Fl_O 222.11 90.210 2048.60 529.70 0.0191 71.91 85.059 2020.05 439.1 0.3002 1.31305 +FS_48 Duct3.Fl_O 222.11 89.759 2048.60 529.70 0.0191 72.27 84.633 2020.05 441.4 0.3002 1.31305 +FS_5 LPT.Fl_O 222.11 20.048 1463.65 366.20 0.0191 273.51 18.556 1435.22 1477.4 0.3413 1.33912 +FS_7 Duct4.Fl_O 222.11 19.847 1463.65 366.20 0.0191 276.27 19.074 1448.98 2018.9 0.2442 1.33912 +FS_9 Core_Nozz.Fl_O 222.11 19.847 1463.65 366.20 0.0191 276.27 13.664 1330.62 862.8 0.7624 1.33912 +FS_15 BypBld.Fl_O 1174.37 21.168 619.04 148.05 0.0000 890.69 18.481 595.54 3795.6 0.4448 1.39869 +FS_17 Duct5.Fl_O 1174.37 21.010 619.04 148.05 0.0000 897.42 18.343 595.54 3824.3 0.4448 1.39869 +FS_19 Byp_Nozz.Fl_O 1174.37 21.010 619.04 148.05 0.0000 897.42 13.664 547.51 2706.3 0.8087 1.39869 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1538.15 1.562 0.9079 3550.813 1.1495 0.9135 -38089.4 30.36 16.23 +LPC 165.72 2.188 0.8638 3311.897 1.2879 0.8778 -13288.0 29.62 21.18 +HPC 86.15 5.607 0.8633 6340.901 1.6990 0.8906 -43148.6 20.99 21.01 +HPT 27.39 2.707 0.9145 153.525 1.2331 0.9048 43147.9 +LPT 72.27 4.477 0.9272 79.939 1.3996 0.9131 51377.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2949.21 1.391 0.9379 0.900 1.9323 0.5215 1.4369 0.9679 3943.9586 +LPC 177.76 1.364 0.8998 0.904 1.7476 0.9323 3.2631 0.9600 3662.6571 +HPC 204.83 22.298 0.8516 0.997 2.0961 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.019 0.9329 100.270 5.0186 1.4085 0.4249 0.9803 1.5311 +LPT 150.18 5.851 0.9260 98.555 5.8506 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 996.50 240.12 77.203 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 996.50 240.12 77.203 +Duct1 0.0025 0.4328 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 996.50 240.12 77.203 +Duct2 0.0025 0.4462 365.99 +Duct3 0.0050 0.3002 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3413 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.6284 1354.53 331.07 258.450 +Duct5 0.0075 0.4448 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.9874 1354.53 331.07 258.450 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 619.04 148.05 21.168 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3881 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7861.4 28826.7 43147.9 +LP_Shaft 3618.2 74578.6 51377.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2622.05 0.9940 0.0550 4.15349 0.02094 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.538 0.9975 1.0000 0.9975 2706.36 0.809 925.3 33773.1 +Core_Nozz 1.452 0.9999 1.0000 0.9999 862.88 0.762 1337.0 9229.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 45 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 2000.0 27.00 1318.35 38223.7 0.3391 12961.80 5.5564 0.00 17.084 2518.9 2456.4 1963.7 + core size:20.16 Q: 0.00 Maximum Thrust: 47779.6 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1318.35 13.664 538.54 128.72 0.0000 1444.78 13.664 538.54 -----.- 0.0000 1.40014 +FS_2 Inlet.Fl_O 1318.35 13.555 538.54 128.72 0.0000 1456.43 11.646 515.67 5943.4 0.4706 1.40014 +FS_21 Fan.Fl_O 1318.35 20.358 611.51 146.24 0.0000 1033.38 17.922 589.68 4515.2 0.4307 1.39885 +FS_13 Splitter.Fl_O2 1117.27 20.358 611.51 146.24 0.0000 875.77 17.875 589.24 3795.6 0.4352 1.39885 +FS_22 Splitter.Fl_O1 201.08 20.358 611.51 146.24 0.0000 157.61 18.157 591.89 719.5 0.4076 1.39885 +FS_23 Duct1.Fl_O 201.08 20.307 611.51 146.24 0.0000 158.01 18.112 591.89 721.3 0.4076 1.39885 +FS_24 LPC.Fl_O 201.08 42.437 776.81 186.18 0.0000 85.22 37.146 748.13 366.0 0.4412 1.39307 +FS_25 Duct2.Fl_O 201.08 42.331 776.81 186.18 0.0000 85.43 37.053 748.13 366.9 0.4412 1.39307 +FS_3 HPC.Fl_O 201.08 233.438 1315.09 320.85 0.0000 20.16 219.366 1293.55 119.9 0.3034 1.36097 +FS_36 Bld3.Fl_O 182.98 233.438 1315.09 320.85 0.0000 18.34 219.366 1293.55 109.1 0.3034 1.36097 +FS_4 Burner.Fl_O 186.58 220.599 2518.89 667.70 0.0197 27.39 219.178 2515.14 483.4 0.0997 1.29992 +FS_45 HPT.Fl_O 204.68 81.124 1963.66 504.73 0.0179 72.15 76.459 1935.85 439.1 0.3008 1.31683 +FS_48 Duct3.Fl_O 204.68 80.718 1963.66 504.73 0.0179 72.51 76.077 1935.85 441.4 0.3008 1.31683 +FS_5 LPT.Fl_O 204.68 18.878 1414.66 352.61 0.0179 263.15 17.587 1389.28 1477.4 0.3261 1.34265 +FS_7 Duct4.Fl_O 204.68 18.689 1414.66 352.61 0.0179 265.81 18.017 1401.49 2018.9 0.2340 1.34265 +FS_9 Core_Nozz.Fl_O 204.68 18.689 1414.66 352.61 0.0179 265.81 13.664 1305.25 862.8 0.6953 1.34265 +FS_15 BypBld.Fl_O 1117.27 20.358 611.51 146.24 0.0000 875.77 17.875 589.24 3795.6 0.4352 1.39885 +FS_17 Duct5.Fl_O 1117.27 20.205 611.51 146.24 0.0000 882.39 17.741 589.24 3824.3 0.4352 1.39885 +FS_19 Byp_Nozz.Fl_O 1117.27 20.205 611.51 146.24 0.0000 882.39 13.664 546.90 2706.4 0.7690 1.39885 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1456.43 1.502 0.9087 3388.006 1.1355 0.9138 -32690.7 33.42 16.02 +LPC 158.01 2.090 0.8609 3179.428 1.2703 0.8743 -11361.1 29.24 19.64 +HPC 85.43 5.515 0.8640 6321.367 1.6929 0.8910 -38313.3 22.28 22.35 +HPT 27.39 2.719 0.9146 154.142 1.2363 0.9047 38313.4 +LPT 72.51 4.276 0.9249 77.906 1.3881 0.9108 44051.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2792.49 1.349 0.9388 0.859 1.8706 0.5215 1.4369 0.9679 3943.9586 +LPC 169.49 1.334 0.8967 0.868 1.7216 0.9323 3.2631 0.9600 3662.6571 +HPC 203.10 21.870 0.8524 0.994 2.1143 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.047 0.9330 100.673 5.0465 1.4085 0.4249 0.9803 1.5311 +LPT 150.67 5.570 0.9237 96.049 5.5697 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 969.08 233.31 70.328 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 969.08 233.31 70.328 +Duct1 0.0025 0.4076 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 969.08 233.31 70.328 +Duct2 0.0025 0.4412 365.99 +Duct3 0.0050 0.3008 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3261 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.0377 1315.09 320.85 233.438 +Duct5 0.0075 0.4352 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.0593 1315.09 320.85 233.438 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 611.51 146.24 20.358 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5564 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7736.1 26011.2 38313.4 +LP_Shaft 3452.3 67017.3 44051.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2518.89 0.9940 0.0550 3.60050 0.01968 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.479 0.9975 1.0000 0.9975 2706.36 0.769 879.3 30535.1 +Core_Nozz 1.368 0.9999 1.0000 0.9999 862.88 0.695 1208.6 7688.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 46 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 2000.0 27.00 1150.24 28667.8 0.3257 9336.37 5.8899 0.00 13.520 2298.6 2242.7 1781.9 + core size:20.44 Q: 0.00 Maximum Thrust: 47779.6 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1150.24 13.664 538.54 128.72 0.0000 1260.55 13.664 538.54 -----.- 0.0000 1.40014 +FS_2 Inlet.Fl_O 1150.24 13.555 538.54 128.72 0.0000 1270.71 12.169 522.19 5943.4 0.3954 1.40014 +FS_21 Fan.Fl_O 1150.24 18.701 596.03 142.52 0.0000 968.99 16.772 577.81 4515.2 0.3974 1.39910 +FS_13 Splitter.Fl_O2 983.30 18.701 596.03 142.52 0.0000 828.35 16.697 577.06 3795.6 0.4057 1.39910 +FS_22 Splitter.Fl_O1 166.95 18.701 596.03 142.52 0.0000 140.64 17.138 581.37 719.5 0.3553 1.39910 +FS_23 Duct1.Fl_O 166.95 18.654 596.03 142.52 0.0000 140.99 17.095 581.37 721.3 0.3553 1.39910 +FS_24 LPC.Fl_O 166.95 34.768 731.14 175.10 0.0000 83.78 30.604 705.18 366.0 0.4314 1.39498 +FS_25 Duct2.Fl_O 166.95 34.681 731.14 175.10 0.0000 83.99 30.527 705.18 366.9 0.4314 1.39498 +FS_3 HPC.Fl_O 166.95 184.744 1229.25 298.78 0.0000 20.44 173.265 1208.27 119.9 0.3076 1.36631 +FS_36 Bld3.Fl_O 151.92 184.744 1229.25 298.78 0.0000 18.60 173.265 1208.27 109.1 0.3076 1.36631 +FS_4 Burner.Fl_O 154.51 174.583 2298.62 600.84 0.0171 27.38 173.459 2295.14 483.4 0.0994 1.30708 +FS_45 HPT.Fl_O 169.54 63.497 1781.94 452.28 0.0155 72.73 59.784 1755.72 439.1 0.3025 1.32579 +FS_48 Duct3.Fl_O 169.54 63.180 1781.94 452.28 0.0155 73.10 59.485 1755.72 441.4 0.3025 1.32579 +FS_5 LPT.Fl_O 169.54 17.001 1319.56 326.55 0.0155 233.76 16.101 1301.06 1477.4 0.2848 1.34993 +FS_7 Duct4.Fl_O 169.54 16.831 1319.56 326.55 0.0155 236.12 16.358 1309.84 2018.9 0.2059 1.34993 +FS_9 Core_Nozz.Fl_O 169.54 16.831 1319.56 326.55 0.0155 236.12 13.664 1249.83 862.9 0.5625 1.34993 +FS_15 BypBld.Fl_O 983.30 18.701 596.03 142.52 0.0000 828.35 16.697 577.06 3795.6 0.4057 1.39910 +FS_17 Duct5.Fl_O 983.30 18.560 596.03 142.52 0.0000 834.61 16.572 577.06 3824.3 0.4057 1.39910 +FS_19 Byp_Nozz.Fl_O 983.30 18.560 596.03 142.52 0.0000 834.61 13.664 546.12 2706.4 0.6763 1.39910 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1270.71 1.380 0.9017 3009.886 1.1068 0.9061 -22465.1 35.98 14.89 +LPC 140.99 1.864 0.8546 2861.041 1.2267 0.8667 -7695.1 29.70 17.03 +HPC 83.99 5.327 0.8644 6287.546 1.6813 0.8909 -29214.4 25.09 25.20 +HPT 27.38 2.749 0.9149 155.704 1.2445 0.9049 29214.4 +LPT 73.10 3.716 0.9201 72.655 1.3504 0.9067 30159.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2436.42 1.264 0.9316 0.763 1.7824 0.5215 1.4369 0.9679 3943.9586 +LPC 151.23 1.265 0.8902 0.781 1.7000 0.9323 3.2631 0.9600 3662.6571 +HPC 199.68 21.002 0.8528 0.989 2.1536 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.118 0.9333 101.693 5.1175 1.4085 0.4249 0.9803 1.5311 +LPT 151.89 4.789 0.9189 89.575 4.7891 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 908.60 218.39 56.665 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 908.60 218.39 56.665 +Duct1 0.0025 0.3553 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 908.60 218.39 56.665 +Duct2 0.0025 0.4314 365.99 +Duct3 0.0050 0.3025 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2848 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.8431 1229.25 298.78 184.744 +Duct5 0.0075 0.4057 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.1821 1229.25 298.78 184.744 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 596.03 142.52 18.701 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.8899 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7465.1 20554.0 29214.4 +LP_Shaft 3067.0 51647.6 30159.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2298.62 0.9940 0.0550 2.59344 0.01707 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.358 0.9975 1.0000 0.9975 2706.36 0.676 772.8 23616.9 +Core_Nozz 1.232 0.9999 1.0000 0.9999 862.88 0.562 958.6 5050.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 47 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 8/ 18/ 1/ 6 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 2000.0 27.00 946.09 19111.9 0.3175 6068.81 6.1824 0.00 10.007 2032.4 1984.5 1564.9 + core size:20.84 Q: 0.00 Maximum Thrust: 47779.6 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 946.09 13.664 538.54 128.72 0.0000 1036.82 13.664 538.54 -----.- 0.0000 1.40014 +FS_2 Inlet.Fl_O 946.09 13.555 538.54 128.72 0.0000 1045.18 12.656 528.08 5943.4 0.3145 1.40014 +FS_21 Fan.Fl_O 946.09 17.026 579.00 138.43 0.0000 862.79 15.673 565.47 4515.2 0.3460 1.39938 +FS_13 Splitter.Fl_O2 814.37 17.026 579.00 138.43 0.0000 742.67 15.600 564.72 3795.6 0.3557 1.39938 +FS_22 Splitter.Fl_O1 131.72 17.026 579.00 138.43 0.0000 120.13 16.017 568.99 719.5 0.2968 1.39938 +FS_23 Duct1.Fl_O 131.72 16.984 579.00 138.43 0.0000 120.43 15.977 568.99 721.3 0.2968 1.39938 +FS_24 LPC.Fl_O 131.72 27.277 677.95 162.24 0.0000 81.14 24.246 655.63 366.0 0.4140 1.39678 +FS_25 Duct2.Fl_O 131.72 27.209 677.95 162.24 0.0000 81.34 24.186 655.63 366.9 0.4140 1.39678 +FS_3 HPC.Fl_O 131.72 136.745 1124.50 272.17 0.0000 20.84 127.889 1104.21 119.9 0.3136 1.37290 +FS_36 Bld3.Fl_O 119.87 136.745 1124.50 272.17 0.0000 18.97 127.889 1104.21 109.1 0.3136 1.37290 +FS_4 Burner.Fl_O 121.56 129.224 2032.42 522.12 0.0141 27.36 128.393 2029.26 483.4 0.0990 1.31700 +FS_45 HPT.Fl_O 133.41 46.488 1564.87 391.37 0.0128 73.26 43.729 1540.85 439.1 0.3034 1.33793 +FS_48 Duct3.Fl_O 133.41 46.256 1564.87 391.37 0.0128 73.62 43.510 1540.85 441.4 0.3034 1.33793 +FS_5 LPT.Fl_O 133.41 15.613 1217.25 298.99 0.0128 192.38 15.064 1205.82 1477.4 0.2299 1.35818 +FS_7 Duct4.Fl_O 133.41 15.456 1217.25 298.99 0.0128 194.32 15.165 1211.16 2018.9 0.1675 1.35818 +FS_9 Core_Nozz.Fl_O 133.41 15.456 1217.25 298.99 0.0128 194.32 13.664 1178.29 862.9 0.4287 1.35818 +FS_15 BypBld.Fl_O 814.37 17.026 579.00 138.43 0.0000 742.67 15.600 564.72 3795.6 0.3557 1.39938 +FS_17 Duct5.Fl_O 814.37 16.898 579.00 138.43 0.0000 748.28 15.483 564.72 3824.3 0.3557 1.39938 +FS_19 Byp_Nozz.Fl_O 814.37 16.898 579.00 138.43 0.0000 748.28 13.664 544.90 2706.4 0.5594 1.39938 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1045.18 1.256 0.8959 2536.079 1.0751 0.8992 -13000.1 34.37 12.15 +LPC 120.43 1.606 0.8455 2445.866 1.1709 0.8555 -4438.4 33.66 14.38 +HPC 81.34 5.026 0.8641 6236.070 1.6587 0.8904 -20487.3 29.50 29.68 +HPT 27.36 2.780 0.9155 158.146 1.2550 0.9051 20487.3 +LPT 73.62 2.963 0.9088 65.326 1.2856 0.8960 17438.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2004.00 1.178 0.9255 0.643 1.6996 0.5215 1.4369 0.9679 3943.9586 +LPC 129.18 1.186 0.8807 0.668 1.7241 0.9323 3.2631 0.9600 3662.6571 +HPC 193.38 19.610 0.8525 0.981 2.1884 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.189 0.9339 103.288 5.1888 1.4085 0.4249 0.9803 1.5311 +LPT 152.98 3.738 0.9076 80.539 3.7379 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 836.51 200.72 43.256 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 836.51 200.72 43.256 +Duct1 0.0025 0.2968 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 836.51 200.72 43.256 +Duct2 0.0025 0.4140 365.99 +Duct3 0.0050 0.3034 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2299 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.6104 1124.50 272.17 136.745 +Duct5 0.0075 0.3557 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.2448 1124.50 272.17 136.745 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 579.00 138.43 17.026 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.1824 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7129.6 15092.2 20487.3 +LP_Shaft 2584.2 35441.5 17438.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2032.42 0.9940 0.0550 1.68578 0.01406 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.237 0.9975 1.0000 0.9975 2706.36 0.559 638.6 16163.2 +Core_Nozz 1.131 0.9999 1.0000 0.9999 862.88 0.429 711.1 2948.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 48 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 2000.0 27.00 675.15 9555.7 0.3298 3151.85 6.1542 0.00 6.488 1672.9 1636.1 1276.8 + core size:21.57 Q: 0.00 Maximum Thrust: 47779.6 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 675.15 13.664 538.54 128.72 0.0000 739.90 13.664 538.54 -----.- 0.0000 1.40014 +FS_2 Inlet.Fl_O 675.15 13.555 538.54 128.72 0.0000 745.86 13.115 533.48 5943.4 0.2177 1.40014 +FS_21 Fan.Fl_O 675.15 15.358 560.54 134.00 0.0000 671.61 14.646 552.99 4515.2 0.2613 1.39970 +FS_13 Splitter.Fl_O2 580.78 15.358 560.54 134.00 0.0000 577.73 14.611 552.61 3795.6 0.2679 1.39970 +FS_22 Splitter.Fl_O1 94.37 15.358 560.54 134.00 0.0000 93.88 14.817 554.83 719.5 0.2269 1.39970 +FS_23 Duct1.Fl_O 94.37 15.320 560.54 134.00 0.0000 94.11 14.780 554.83 721.3 0.2269 1.39970 +FS_24 LPC.Fl_O 94.37 19.942 613.52 146.72 0.0000 75.64 18.055 596.37 366.0 0.3797 1.39881 +FS_25 Duct2.Fl_O 94.37 19.892 613.52 146.72 0.0000 75.83 18.010 596.37 366.9 0.3797 1.39881 +FS_3 HPC.Fl_O 94.37 88.656 985.94 237.49 0.0000 21.57 82.475 966.43 119.9 0.3249 1.38159 +FS_36 Bld3.Fl_O 85.88 88.656 985.94 237.49 0.0000 19.63 82.475 966.43 109.1 0.3249 1.38159 +FS_4 Burner.Fl_O 86.75 83.780 1672.86 419.73 0.0102 27.33 83.242 1670.16 483.4 0.0982 1.33443 +FS_45 HPT.Fl_O 95.25 29.851 1276.75 313.54 0.0093 73.57 28.065 1256.17 439.1 0.3026 1.35680 +FS_48 Duct3.Fl_O 95.25 29.702 1276.75 313.54 0.0093 73.94 27.925 1256.17 441.4 0.3026 1.35680 +FS_5 LPT.Fl_O 95.25 14.614 1082.38 263.51 0.0093 138.36 14.354 1077.15 1477.4 0.1622 1.36916 +FS_7 Duct4.Fl_O 95.25 14.468 1082.38 263.51 0.0093 139.76 14.328 1079.56 2018.9 0.1190 1.36916 +FS_9 Core_Nozz.Fl_O 95.25 14.468 1082.38 263.51 0.0093 139.76 13.664 1065.80 862.9 0.2901 1.36916 +FS_15 BypBld.Fl_O 580.78 15.358 560.54 134.00 0.0000 577.73 14.611 552.61 3795.6 0.2679 1.39970 +FS_17 Duct5.Fl_O 580.78 15.243 560.54 134.00 0.0000 582.10 14.501 552.61 3824.3 0.2679 1.39970 +FS_19 Byp_Nozz.Fl_O 580.78 15.243 560.54 134.00 0.0000 582.10 13.664 543.30 2706.4 0.3984 1.39970 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 745.86 1.133 0.8894 1873.424 1.0409 0.8914 -5043.2 35.47 7.01 +LPC 94.11 1.302 0.8270 1836.290 1.0945 0.8333 -1699.6 46.99 12.53 +HPC 75.83 4.457 0.8619 6136.422 1.6070 0.8870 -12119.3 38.54 39.06 +HPT 27.33 2.807 0.9166 163.175 1.2703 0.9057 12119.6 +LPT 73.94 2.032 0.8845 53.425 1.1796 0.8746 6742.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1430.09 1.093 0.9189 0.475 1.6182 0.5215 1.4369 0.9679 3943.9586 +LPC 100.95 1.092 0.8614 0.501 1.8927 0.9323 3.2631 0.9600 3662.6571 +HPC 180.27 16.980 0.8503 0.965 2.2560 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.252 0.9350 106.573 5.2520 1.4085 0.4249 0.9803 1.5311 +LPT 153.64 2.440 0.8834 65.866 2.4402 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 745.15 178.49 29.966 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 745.15 178.49 29.966 +Duct1 0.0025 0.2269 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 745.15 178.49 29.966 +Duct2 0.0025 0.3797 365.99 +Duct3 0.0050 0.3026 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1622 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.3030 985.94 237.49 88.656 +Duct5 0.0075 0.2679 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.1904 985.94 237.49 88.656 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 560.54 134.00 15.358 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.1542 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6674.0 9537.6 12119.6 +LP_Shaft 1909.0 18550.4 6742.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1672.86 0.9940 0.0550 0.87551 0.01019 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.116 0.9975 1.0000 0.9975 2706.36 0.398 454.1 8196.3 +Core_Nozz 1.059 0.9999 1.0000 0.9999 862.88 0.290 459.2 1359.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 49 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 2000.0 27.00 1469.85 43207.5 0.3986 17222.71 5.2352 113.77 20.752 2730.0 2661.2 2138.2 + core size:19.90 Q: 13.78 Maximum Thrust: 43207.5 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1469.85 13.760 539.61 128.97 0.0000 1601.18 13.664 538.54 27165.8 0.1000 1.40012 +FS_2 Inlet.Fl_O 1469.85 13.664 539.61 128.97 0.0000 1612.47 11.176 509.48 5943.4 0.5434 1.40012 +FS_21 Fan.Fl_O 1469.85 22.093 627.70 150.13 0.0000 1075.58 19.187 602.96 4515.2 0.4536 1.39848 +FS_13 Splitter.Fl_O2 1234.11 22.093 627.70 150.13 0.0000 903.08 19.195 603.03 3795.6 0.4529 1.39848 +FS_22 Splitter.Fl_O1 235.73 22.093 627.70 150.13 0.0000 172.50 19.142 602.55 719.5 0.4574 1.39848 +FS_23 Duct1.Fl_O 235.73 22.038 627.70 150.13 0.0000 172.93 19.094 602.55 721.3 0.4574 1.39848 +FS_24 LPC.Fl_O 235.73 50.311 818.56 196.34 0.0000 86.50 43.810 787.29 366.0 0.4502 1.39106 +FS_25 Duct2.Fl_O 235.73 50.186 818.56 196.34 0.0000 86.72 43.700 787.29 366.9 0.4502 1.39106 +FS_3 HPC.Fl_O 235.73 285.549 1394.87 341.57 0.0000 19.90 268.807 1372.88 119.9 0.2995 1.35620 +FS_36 Bld3.Fl_O 214.52 285.549 1394.87 341.57 0.0000 18.11 268.807 1372.88 109.1 0.2995 1.35620 +FS_4 Burner.Fl_O 219.30 269.843 2730.00 733.23 0.0223 27.40 268.104 2726.00 483.4 0.1000 1.29374 +FS_45 HPT.Fl_O 240.52 100.155 2138.23 556.34 0.0203 71.66 94.478 2108.92 439.1 0.2995 1.30934 +FS_48 Duct3.Fl_O 240.52 99.655 2138.23 556.34 0.0203 72.02 94.006 2108.92 441.4 0.2995 1.30934 +FS_5 LPT.Fl_O 240.52 21.492 1519.23 381.74 0.0203 281.48 19.787 1487.97 1477.4 0.3534 1.33531 +FS_7 Duct4.Fl_O 240.52 21.277 1519.23 381.74 0.0203 284.32 20.396 1503.17 2018.9 0.2523 1.33531 +FS_9 Core_Nozz.Fl_O 240.52 21.277 1519.23 381.74 0.0203 284.32 13.664 1357.91 862.9 0.8347 1.33531 +FS_15 BypBld.Fl_O 1234.11 22.093 627.70 150.13 0.0000 903.08 19.195 603.03 3795.6 0.4529 1.39848 +FS_17 Duct5.Fl_O 1234.11 21.927 627.70 150.13 0.0000 909.90 19.051 603.03 3824.3 0.4529 1.39848 +FS_19 Byp_Nozz.Fl_O 1234.11 21.927 627.70 150.13 0.0000 909.90 13.664 548.44 2706.4 0.8506 1.39848 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1612.47 1.617 0.9006 3703.463 1.1632 0.9071 -44003.3 27.17 16.30 +LPC 172.93 2.283 0.8664 3433.804 1.3041 0.8808 -15410.3 29.93 22.69 +HPC 86.72 5.690 0.8625 6358.524 1.7041 0.8901 -48438.8 19.76 19.73 +HPT 27.40 2.694 0.9143 152.881 1.2295 0.9048 48438.7 +LPT 72.02 4.637 0.9291 81.692 1.4074 0.9152 59413.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3091.70 1.429 0.9304 0.939 2.0438 0.5215 1.4369 0.9679 3943.9586 +LPC 185.49 1.393 0.9024 0.938 1.7728 0.9323 3.2631 0.9600 3662.6571 +HPC 206.17 22.680 0.8508 1.000 2.0724 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.988 0.9326 99.849 4.9876 1.4085 0.4249 0.9803 1.5311 +LPT 149.64 6.073 0.9279 100.715 6.0734 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 27165.80 5197.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1024.84 247.17 84.666 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1024.84 247.17 84.666 +Duct1 0.0025 0.4574 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1024.84 247.17 84.666 +Duct2 0.0025 0.4502 365.99 +Duct3 0.0050 0.2995 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3534 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.2507 1394.87 341.57 285.549 +Duct5 0.0075 0.4529 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.9653 1394.87 341.57 285.549 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 627.70 150.13 22.093 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.2352 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7988.0 31848.6 48438.7 +LP_Shaft 3777.5 82606.7 59413.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.00 0.9940 0.0550 4.78409 0.02230 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.605 0.9975 1.0000 0.9975 2706.36 0.851 974.0 37360.5 +Core_Nozz 1.557 0.9999 1.0000 0.9999 862.88 0.835 1477.4 11044.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 50 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 2000.0 27.00 1406.43 38886.6 0.3888 15119.97 5.3973 113.77 18.966 2627.6 2561.9 2053.2 + core size:20.03 Q: 13.78 Maximum Thrust: 43207.5 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1406.43 13.760 539.61 128.97 0.0000 1532.10 13.664 538.54 25993.7 0.1000 1.40012 +FS_2 Inlet.Fl_O 1406.43 13.664 539.61 128.97 0.0000 1542.90 11.444 512.94 5943.4 0.5096 1.40012 +FS_21 Fan.Fl_O 1406.43 21.345 620.34 148.36 0.0000 1058.97 18.639 596.82 4515.2 0.4445 1.39866 +FS_13 Splitter.Fl_O2 1186.58 21.345 620.34 148.36 0.0000 893.43 18.616 596.60 3795.6 0.4465 1.39866 +FS_22 Splitter.Fl_O1 219.85 21.345 620.34 148.36 0.0000 165.53 18.760 597.92 719.5 0.4336 1.39866 +FS_23 Duct1.Fl_O 219.85 21.292 620.34 148.36 0.0000 165.95 18.713 597.92 721.3 0.4336 1.39866 +FS_24 LPC.Fl_O 219.85 46.700 799.46 191.68 0.0000 85.89 40.766 769.41 366.0 0.4459 1.39197 +FS_25 Duct2.Fl_O 219.85 46.583 799.46 191.68 0.0000 86.11 40.665 769.41 366.9 0.4459 1.39197 +FS_3 HPC.Fl_O 219.85 260.980 1357.69 331.89 0.0000 20.03 245.459 1335.87 119.9 0.3015 1.35840 +FS_36 Bld3.Fl_O 200.06 260.980 1357.69 331.89 0.0000 18.23 245.459 1335.87 109.1 0.3015 1.35840 +FS_4 Burner.Fl_O 204.26 246.626 2627.58 701.24 0.0210 27.40 245.037 2623.69 483.4 0.0999 1.29662 +FS_45 HPT.Fl_O 224.05 91.115 2053.23 531.05 0.0191 71.90 85.914 2024.63 439.1 0.3002 1.31286 +FS_48 Duct3.Fl_O 224.05 90.659 2053.23 531.05 0.0191 72.26 85.484 2024.63 441.4 0.3002 1.31286 +FS_5 LPT.Fl_O 224.05 20.172 1465.90 366.83 0.0191 274.40 18.660 1437.22 1477.4 0.3426 1.33896 +FS_7 Duct4.Fl_O 224.05 19.971 1465.90 366.83 0.0191 277.17 19.187 1451.10 2018.9 0.2451 1.33896 +FS_9 Core_Nozz.Fl_O 224.05 19.971 1465.90 366.83 0.0191 277.17 13.664 1330.59 862.9 0.7690 1.33896 +FS_15 BypBld.Fl_O 1186.58 21.345 620.34 148.36 0.0000 893.43 18.616 596.60 3795.6 0.4465 1.39866 +FS_17 Duct5.Fl_O 1186.58 21.185 620.34 148.36 0.0000 900.18 18.476 596.60 3824.3 0.4465 1.39866 +FS_19 Byp_Nozz.Fl_O 1186.58 21.185 620.34 148.36 0.0000 900.18 13.664 547.35 2706.4 0.8170 1.39866 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1542.90 1.562 0.9079 3556.271 1.1496 0.9135 -38583.0 30.48 16.41 +LPC 165.95 2.193 0.8639 3316.825 1.2887 0.8779 -13474.5 29.54 21.17 +HPC 86.11 5.602 0.8634 6339.545 1.6983 0.8907 -43610.2 21.04 21.06 +HPT 27.40 2.707 0.9145 153.544 1.2329 0.9049 43609.1 +LPT 72.26 4.494 0.9272 80.052 1.4007 0.9131 52058.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2958.15 1.391 0.9379 0.902 1.9455 0.5215 1.4369 0.9679 3943.9586 +LPC 178.00 1.366 0.8998 0.906 1.7463 0.9323 3.2631 0.9600 3662.6571 +HPC 204.71 22.276 0.8517 0.997 2.0960 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.017 0.9329 100.282 5.0170 1.4085 0.4249 0.9803 1.5311 +LPT 150.15 5.874 0.9260 98.694 5.8744 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 25993.74 4973.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 999.07 240.75 77.992 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 999.07 240.75 77.992 +Duct1 0.0025 0.4336 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 999.07 240.75 77.992 +Duct2 0.0025 0.4459 365.99 +Duct3 0.0050 0.3002 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3426 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.6946 1357.69 331.89 260.980 +Duct5 0.0075 0.4465 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.0916 1357.69 331.89 260.980 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 620.34 148.36 21.345 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3973 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7870.6 29100.5 43609.1 +LP_Shaft 3627.4 75376.3 52058.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2627.58 0.9940 0.0550 4.19999 0.02099 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.550 0.9975 1.0000 0.9975 2706.36 0.817 934.6 34469.1 +Core_Nozz 1.462 0.9999 1.0000 0.9999 862.88 0.769 1348.5 9390.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 51 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 2000.0 27.00 1336.79 34566.0 0.3819 13199.45 5.5616 113.77 17.224 2528.7 2466.0 1971.9 + core size:20.15 Q: 13.78 Maximum Thrust: 43207.5 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1336.79 13.760 539.61 128.97 0.0000 1456.24 13.664 538.54 24706.7 0.1000 1.40012 +FS_2 Inlet.Fl_O 1336.79 13.664 539.61 128.97 0.0000 1466.51 11.707 516.29 5943.4 0.4750 1.40012 +FS_21 Fan.Fl_O 1336.79 20.570 613.13 146.63 0.0000 1038.37 18.081 590.99 4515.2 0.4333 1.39882 +FS_13 Splitter.Fl_O2 1133.06 20.570 613.13 146.63 0.0000 880.12 18.032 590.53 3795.6 0.4379 1.39882 +FS_22 Splitter.Fl_O1 203.73 20.570 613.13 146.63 0.0000 158.25 18.327 593.27 719.5 0.4097 1.39882 +FS_23 Duct1.Fl_O 203.73 20.519 613.13 146.63 0.0000 158.65 18.281 593.27 721.3 0.4097 1.39882 +FS_24 LPC.Fl_O 203.73 43.111 780.16 186.99 0.0000 85.17 37.742 751.39 366.0 0.4409 1.39291 +FS_25 Duct2.Fl_O 203.73 43.004 780.16 186.99 0.0000 85.39 37.648 751.39 366.9 0.4409 1.39291 +FS_3 HPC.Fl_O 203.73 237.004 1320.14 322.15 0.0000 20.15 222.721 1298.54 119.9 0.3033 1.36066 +FS_36 Bld3.Fl_O 185.40 237.004 1320.14 322.15 0.0000 18.34 222.721 1298.54 109.1 0.3033 1.36066 +FS_4 Burner.Fl_O 189.06 223.968 2528.73 670.71 0.0198 27.39 222.526 2524.96 483.4 0.0997 1.29963 +FS_45 HPT.Fl_O 207.40 82.407 1971.86 507.12 0.0180 72.12 77.673 1943.98 439.1 0.3007 1.31647 +FS_48 Duct3.Fl_O 207.40 81.995 1971.86 507.12 0.0180 72.48 77.285 1943.98 441.4 0.3007 1.31647 +FS_5 LPT.Fl_O 207.40 19.034 1418.46 353.66 0.0180 264.82 17.714 1392.66 1477.4 0.3285 1.34237 +FS_7 Duct4.Fl_O 207.40 18.843 1418.46 353.66 0.0180 267.49 18.157 1405.09 2018.9 0.2356 1.34237 +FS_9 Core_Nozz.Fl_O 207.40 18.843 1418.46 353.66 0.0180 267.49 13.664 1306.04 862.8 0.7047 1.34237 +FS_15 BypBld.Fl_O 1133.06 20.570 613.13 146.63 0.0000 880.12 18.032 590.53 3795.6 0.4379 1.39882 +FS_17 Duct5.Fl_O 1133.06 20.416 613.13 146.63 0.0000 886.77 17.897 590.53 3824.3 0.4379 1.39882 +FS_19 Byp_Nozz.Fl_O 1133.06 20.416 613.13 146.63 0.0000 886.77 13.664 546.73 2706.4 0.7797 1.39882 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1466.51 1.505 0.9094 3403.015 1.1362 0.9145 -33395.7 33.51 16.27 +LPC 158.65 2.101 0.8610 3192.481 1.2724 0.8745 -11632.8 29.13 19.68 +HPC 85.39 5.511 0.8641 6320.306 1.6921 0.8911 -38960.9 22.30 22.37 +HPT 27.39 2.718 0.9146 154.146 1.2360 0.9047 38961.1 +LPT 72.48 4.308 0.9251 78.167 1.3901 0.9109 45028.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2811.82 1.352 0.9395 0.863 1.8860 0.5215 1.4369 0.9679 3943.9586 +LPC 170.17 1.337 0.8968 0.872 1.7205 0.9323 3.2631 0.9600 3662.6571 +HPC 203.00 21.855 0.8524 0.994 2.1135 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.043 0.9330 100.676 5.0431 1.4085 0.4249 0.9803 1.5311 +LPT 150.60 5.614 0.9239 96.370 5.6144 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 24706.66 4726.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 973.05 234.30 71.425 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 973.05 234.30 71.425 +Duct1 0.0025 0.4097 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 973.05 234.30 71.425 +Duct2 0.0025 0.4409 365.99 +Duct3 0.0050 0.3007 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3285 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.1306 1320.14 322.15 237.004 +Duct5 0.0075 0.4379 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.2052 1320.14 322.15 237.004 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 613.13 146.63 20.570 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5616 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7751.5 26398.6 38961.1 +LP_Shaft 3471.0 68133.2 45028.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2528.73 0.9940 0.0550 3.66651 0.01978 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.494 0.9975 1.0000 0.9975 2706.36 0.780 891.5 31394.0 +Core_Nozz 1.379 0.9999 1.0000 0.9999 862.88 0.705 1225.4 7898.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 52 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 2000.0 27.00 1178.40 25924.0 0.3729 9668.13 5.8976 113.77 13.800 2318.1 2261.7 1798.1 + core size:20.43 Q: 13.78 Maximum Thrust: 43207.5 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1178.40 13.760 539.61 128.97 0.0000 1283.69 13.664 538.54 21779.3 0.1000 1.40012 +FS_2 Inlet.Fl_O 1178.40 13.664 539.61 128.97 0.0000 1292.75 12.211 522.55 5943.4 0.4039 1.40012 +FS_21 Fan.Fl_O 1178.40 18.974 598.28 143.06 0.0000 980.26 16.965 579.48 4515.2 0.4031 1.39907 +FS_13 Splitter.Fl_O2 1007.56 18.974 598.28 143.06 0.0000 838.15 16.885 578.70 3795.6 0.4117 1.39907 +FS_22 Splitter.Fl_O1 170.84 18.974 598.28 143.06 0.0000 142.12 17.351 583.22 719.5 0.3597 1.39907 +FS_23 Duct1.Fl_O 170.84 18.926 598.28 143.06 0.0000 142.47 17.308 583.22 721.3 0.3597 1.39907 +FS_24 LPC.Fl_O 170.84 35.717 736.76 176.46 0.0000 83.78 31.440 710.62 366.0 0.4314 1.39477 +FS_25 Duct2.Fl_O 170.84 35.628 736.76 176.46 0.0000 83.99 31.361 710.62 366.9 0.4314 1.39477 +FS_3 HPC.Fl_O 170.84 189.889 1238.37 301.11 0.0000 20.43 178.108 1217.28 119.9 0.3074 1.36573 +FS_36 Bld3.Fl_O 155.47 189.889 1238.37 301.11 0.0000 18.59 178.108 1217.28 109.1 0.3074 1.36573 +FS_4 Burner.Fl_O 158.15 179.445 2318.10 606.67 0.0173 27.38 178.290 2314.59 483.4 0.0995 1.30642 +FS_45 HPT.Fl_O 173.53 65.333 1798.09 456.88 0.0157 72.68 61.518 1771.72 439.1 0.3023 1.32496 +FS_48 Duct3.Fl_O 173.53 65.006 1798.09 456.88 0.0157 73.04 61.211 1771.72 441.4 0.3023 1.32496 +FS_5 LPT.Fl_O 173.53 17.173 1326.10 328.33 0.0157 237.44 16.233 1306.88 1477.4 0.2898 1.34940 +FS_7 Duct4.Fl_O 173.53 17.001 1326.10 328.33 0.0157 239.84 16.508 1316.01 2018.9 0.2093 1.34940 +FS_9 Core_Nozz.Fl_O 173.53 17.001 1326.10 328.33 0.0157 239.84 13.664 1252.78 863.0 0.5764 1.34940 +FS_15 BypBld.Fl_O 1007.56 18.974 598.28 143.06 0.0000 838.15 16.885 578.70 3795.6 0.4117 1.39907 +FS_17 Duct5.Fl_O 1007.56 18.832 598.28 143.06 0.0000 844.48 16.758 578.70 3824.3 0.4117 1.39907 +FS_19 Byp_Nozz.Fl_O 1007.56 18.832 598.28 143.06 0.0000 844.48 13.664 545.92 2706.4 0.6928 1.39907 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1292.75 1.389 0.9041 3045.739 1.1087 0.9085 -23487.4 36.55 15.35 +LPC 142.47 1.887 0.8550 2892.551 1.2315 0.8672 -8073.1 29.35 17.12 +HPC 83.99 5.330 0.8645 6287.494 1.6808 0.8910 -30130.0 25.00 25.12 +HPT 27.38 2.747 0.9149 155.643 1.2437 0.9049 30130.0 +LPT 73.04 3.785 0.9211 73.263 1.3559 0.9076 31559.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2478.66 1.270 0.9341 0.772 1.8047 0.5215 1.4369 0.9679 3943.9586 +LPC 152.82 1.272 0.8906 0.790 1.6958 0.9323 3.2631 0.9600 3662.6571 +HPC 199.67 21.015 0.8529 0.989 2.1510 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.111 0.9333 101.653 5.1109 1.4085 0.4249 0.9803 1.5311 +LPT 151.78 4.885 0.9199 90.324 4.8854 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 21779.26 4166.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 915.53 220.09 58.227 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 915.53 220.09 58.227 +Duct1 0.0025 0.3597 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 915.53 220.09 58.227 +Duct2 0.0025 0.4314 365.99 +Duct3 0.0050 0.3023 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2898 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.9794 1238.37 301.11 189.889 +Duct5 0.0075 0.4117 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.3963 1238.37 301.11 189.889 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 598.28 143.06 18.974 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.8976 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7493.7 21117.2 30130.0 +LP_Shaft 3106.6 53355.6 31559.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2318.10 0.9940 0.0550 2.68559 0.01727 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.378 0.9975 1.0000 0.9975 2706.36 0.693 791.5 24787.7 +Core_Nozz 1.244 0.9999 1.0000 0.9999 862.88 0.576 983.3 5303.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 53 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 2000.0 27.00 985.86 17282.8 0.3735 6454.96 6.2171 113.77 10.394 2066.4 2017.6 1592.8 + core size:20.80 Q: 13.78 Maximum Thrust: 43207.5 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 985.86 13.760 539.61 128.97 0.0000 1073.95 13.664 538.54 18220.7 0.1000 1.40012 +FS_2 Inlet.Fl_O 985.86 13.664 539.61 128.97 0.0000 1081.52 12.688 528.31 5943.4 0.3270 1.40012 +FS_21 Fan.Fl_O 985.86 17.334 581.82 139.11 0.0000 885.23 15.876 567.41 4515.2 0.3566 1.39933 +FS_13 Splitter.Fl_O2 849.26 17.334 581.82 139.11 0.0000 762.57 15.794 566.57 3795.6 0.3670 1.39933 +FS_22 Splitter.Fl_O1 136.60 17.334 581.82 139.11 0.0000 122.66 16.260 571.29 719.5 0.3038 1.39933 +FS_23 Duct1.Fl_O 136.60 17.291 581.82 139.11 0.0000 122.96 16.219 571.29 721.3 0.3038 1.39933 +FS_24 LPC.Fl_O 136.60 28.381 685.98 164.18 0.0000 81.35 25.209 663.26 366.0 0.4154 1.39650 +FS_25 Duct2.Fl_O 136.60 28.310 685.98 164.18 0.0000 81.55 25.146 663.26 366.9 0.4154 1.39650 +FS_3 HPC.Fl_O 136.60 143.030 1138.95 275.82 0.0000 20.80 133.811 1118.53 119.9 0.3129 1.37199 +FS_36 Bld3.Fl_O 124.31 143.030 1138.95 275.82 0.0000 18.93 133.811 1118.53 109.1 0.3129 1.37199 +FS_4 Burner.Fl_O 126.10 135.164 2066.44 532.04 0.0144 27.37 134.295 2063.24 483.4 0.0990 1.31561 +FS_45 HPT.Fl_O 138.39 48.712 1592.78 399.09 0.0131 73.17 45.828 1568.47 439.1 0.3032 1.33630 +FS_48 Duct3.Fl_O 138.39 48.468 1592.78 399.09 0.0131 73.53 45.599 1568.47 441.4 0.3032 1.33630 +FS_5 LPT.Fl_O 138.39 15.771 1229.14 302.16 0.0131 198.52 15.180 1216.83 1477.4 0.2379 1.35720 +FS_7 Duct4.Fl_O 138.39 15.614 1229.14 302.16 0.0131 200.52 15.300 1222.59 2018.9 0.1731 1.35720 +FS_9 Core_Nozz.Fl_O 138.39 15.614 1229.14 302.16 0.0131 200.52 13.664 1186.69 862.9 0.4464 1.35720 +FS_15 BypBld.Fl_O 849.26 17.334 581.82 139.11 0.0000 762.57 15.794 566.57 3795.6 0.3670 1.39933 +FS_17 Duct5.Fl_O 849.26 17.204 581.82 139.11 0.0000 768.33 15.676 566.57 3824.3 0.3670 1.39933 +FS_19 Byp_Nozz.Fl_O 849.26 17.204 581.82 139.11 0.0000 768.33 13.664 544.77 2706.4 0.5833 1.39933 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1081.52 1.269 0.8992 2599.659 1.0782 0.9026 -14132.7 35.57 13.09 +LPC 122.96 1.641 0.8466 2503.590 1.1790 0.8570 -4846.1 32.65 14.55 +HPC 81.55 5.052 0.8643 6239.803 1.6603 0.8905 -21576.6 29.05 29.22 +HPT 27.37 2.775 0.9154 157.859 1.2534 0.9050 21576.6 +LPT 73.53 3.073 0.9098 66.441 1.2958 0.8967 18978.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2073.67 1.187 0.9290 0.659 1.7327 0.5215 1.4369 0.9679 3943.9586 +LPC 131.90 1.197 0.8819 0.684 1.7112 0.9323 3.2631 0.9600 3662.6571 +HPC 193.87 19.733 0.8526 0.982 2.1836 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.177 0.9338 103.101 5.1771 1.4085 0.4249 0.9803 1.5311 +LPT 152.80 3.892 0.9086 81.913 3.8920 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 18220.68 3486.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 846.89 203.25 45.117 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 846.89 203.25 45.117 +Duct1 0.0025 0.3038 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 846.89 203.25 45.117 +Duct2 0.0025 0.4154 365.99 +Duct3 0.0050 0.3032 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2379 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.7810 1138.95 275.82 143.030 +Duct5 0.0075 0.3670 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.5131 1138.95 275.82 143.030 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 581.82 139.11 17.334 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.2171 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7176.0 15791.9 21576.6 +LP_Shaft 2651.6 37590.4 18978.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2066.44 0.9940 0.0550 1.79304 0.01442 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.259 0.9975 1.0000 0.9975 2706.36 0.583 665.8 17573.4 +Core_Nozz 1.143 0.9999 1.0000 0.9999 862.88 0.446 742.9 3195.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 54 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 2000.0 27.00 731.10 8641.0 0.4035 3486.58 6.3636 113.77 6.881 1723.0 1684.6 1316.6 + core size:21.45 Q: 13.78 Maximum Thrust: 43207.5 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 731.10 13.760 539.61 128.97 0.0000 796.43 13.664 538.54 13512.2 0.1000 1.40012 +FS_2 Inlet.Fl_O 731.10 13.664 539.61 128.97 0.0000 802.04 13.147 533.71 5943.4 0.2352 1.40012 +FS_21 Fan.Fl_O 731.10 15.663 563.55 134.72 0.0000 715.02 14.834 554.87 4515.2 0.2798 1.39965 +FS_13 Splitter.Fl_O2 631.81 15.663 563.55 134.72 0.0000 617.92 14.784 554.33 3795.6 0.2885 1.39965 +FS_22 Splitter.Fl_O1 99.29 15.663 563.55 134.72 0.0000 97.10 15.071 557.39 719.5 0.2353 1.39965 +FS_23 Duct1.Fl_O 99.29 15.624 563.55 134.72 0.0000 97.34 15.033 557.39 721.3 0.2353 1.39965 +FS_24 LPC.Fl_O 99.29 20.893 622.21 148.81 0.0000 76.49 18.865 604.35 366.0 0.3849 1.39862 +FS_25 Duct2.Fl_O 99.29 20.841 622.21 148.81 0.0000 76.68 18.818 604.35 366.9 0.3849 1.39862 +FS_3 HPC.Fl_O 99.29 94.685 1005.09 242.25 0.0000 21.45 88.162 985.49 119.9 0.3230 1.38040 +FS_36 Bld3.Fl_O 90.35 94.685 1005.09 242.25 0.0000 19.52 88.162 985.49 109.1 0.3230 1.38040 +FS_4 Burner.Fl_O 91.32 89.478 1722.98 433.71 0.0107 27.34 88.904 1720.22 483.4 0.0983 1.33173 +FS_45 HPT.Fl_O 100.25 31.919 1316.64 324.11 0.0098 73.54 30.011 1295.56 439.1 0.3028 1.35400 +FS_48 Duct3.Fl_O 100.25 31.760 1316.64 324.11 0.0098 73.91 29.861 1295.56 441.4 0.3028 1.35400 +FS_5 LPT.Fl_O 100.25 14.717 1100.65 268.26 0.0098 145.83 14.425 1094.74 1477.4 0.1714 1.36767 +FS_7 Duct4.Fl_O 100.25 14.570 1100.65 268.26 0.0098 147.30 14.414 1097.46 2018.9 0.1257 1.36767 +FS_9 Core_Nozz.Fl_O 100.25 14.570 1100.65 268.26 0.0098 147.30 13.664 1081.78 863.0 0.3077 1.36767 +FS_15 BypBld.Fl_O 631.81 15.663 563.55 134.72 0.0000 617.92 14.784 554.33 3795.6 0.2885 1.39965 +FS_17 Duct5.Fl_O 631.81 15.546 563.55 134.72 0.0000 622.58 14.673 554.33 3824.3 0.2885 1.39965 +FS_19 Byp_Nozz.Fl_O 631.81 15.546 563.55 134.72 0.0000 622.58 13.664 543.16 2706.4 0.4333 1.39965 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 802.04 1.146 0.8971 1959.762 1.0444 0.8991 -5942.1 38.27 8.29 +LPC 97.34 1.337 0.8307 1917.689 1.1041 0.8375 -1979.9 44.50 12.70 +HPC 76.68 4.543 0.8624 6152.624 1.6154 0.8877 -13125.5 37.06 37.50 +HPT 27.34 2.803 0.9164 162.346 1.2680 0.9056 13126.4 +LPT 73.91 2.158 0.8892 55.089 1.1962 0.8787 7921.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1537.81 1.102 0.9268 0.497 1.6881 0.5215 1.4369 0.9679 3943.9586 +LPC 104.42 1.103 0.8653 0.524 1.8578 0.9323 3.2631 0.9600 3662.6571 +HPC 182.30 17.380 0.8507 0.968 2.2405 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.244 0.9348 106.031 5.2441 1.4085 0.4249 0.9803 1.5311 +LPT 153.57 2.615 0.8880 67.918 2.6154 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 13512.23 2585.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 757.62 181.52 31.659 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 757.62 181.52 31.659 +Duct1 0.0025 0.2353 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 757.62 181.52 31.659 +Duct2 0.0025 0.3849 365.99 +Duct3 0.0050 0.3028 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1714 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.4750 1005.09 242.25 94.685 +Duct5 0.0075 0.2885 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.4607 1005.09 242.25 94.685 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 563.55 134.72 15.663 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.3636 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6738.8 10230.5 13126.4 +LP_Shaft 1998.9 20813.2 7921.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1722.98 0.9940 0.0550 0.96849 0.01072 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.138 0.9975 1.0000 0.9975 2706.36 0.433 493.8 9697.6 +Core_Nozz 1.066 0.9999 1.0000 0.9999 862.88 0.308 490.6 1528.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 55 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 2000.0 27.00 1495.92 39459.0 0.4404 17377.67 5.2753 227.53 20.551 2730.0 2661.4 2138.3 + core size:19.92 Q: 55.10 Maximum Thrust: 39459.0 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1495.92 14.051 542.85 129.75 0.0000 1600.67 13.664 538.54 13823.8 0.2000 1.40005 +FS_2 Inlet.Fl_O 1495.92 13.966 542.85 129.75 0.0000 1610.34 11.432 512.65 5943.4 0.5424 1.40005 +FS_21 Fan.Fl_O 1495.92 22.466 630.42 150.79 0.0000 1078.84 19.489 605.39 4515.2 0.4554 1.39841 +FS_13 Splitter.Fl_O2 1257.54 22.466 630.42 150.79 0.0000 906.92 19.489 605.38 3795.6 0.4554 1.39841 +FS_22 Splitter.Fl_O1 238.38 22.466 630.42 150.79 0.0000 171.92 19.489 605.39 719.5 0.4554 1.39841 +FS_23 Duct1.Fl_O 238.38 22.410 630.42 150.79 0.0000 172.35 19.440 605.39 721.3 0.4554 1.39841 +FS_24 LPC.Fl_O 238.38 51.103 821.85 197.14 0.0000 86.29 44.537 790.65 366.0 0.4488 1.39090 +FS_25 Duct2.Fl_O 238.38 50.975 821.85 197.14 0.0000 86.51 44.425 790.65 366.9 0.4488 1.39090 +FS_3 HPC.Fl_O 238.38 288.760 1398.03 342.39 0.0000 19.92 271.789 1375.94 119.9 0.2999 1.35601 +FS_36 Bld3.Fl_O 216.93 288.760 1398.03 342.39 0.0000 18.13 271.789 1375.94 109.1 0.2999 1.35601 +FS_4 Burner.Fl_O 221.76 272.878 2730.00 733.18 0.0223 27.40 271.119 2725.99 483.4 0.1000 1.29378 +FS_45 HPT.Fl_O 243.21 101.280 2138.34 556.34 0.0202 71.66 95.539 2109.03 439.1 0.2995 1.30936 +FS_48 Duct3.Fl_O 243.21 100.773 2138.34 556.34 0.0202 72.02 95.061 2109.03 441.4 0.2995 1.30936 +FS_5 LPT.Fl_O 243.21 21.670 1518.40 381.50 0.0202 282.21 19.941 1486.96 1477.4 0.3545 1.33538 +FS_7 Duct4.Fl_O 243.21 21.453 1518.40 381.50 0.0202 285.06 20.560 1502.25 2018.9 0.2530 1.33538 +FS_9 Core_Nozz.Fl_O 243.21 21.453 1518.40 381.50 0.0202 285.06 13.664 1354.27 862.9 0.8429 1.33538 +FS_15 BypBld.Fl_O 1257.54 22.466 630.42 150.79 0.0000 906.92 19.489 605.38 3795.6 0.4554 1.39841 +FS_17 Duct5.Fl_O 1257.54 22.297 630.42 150.79 0.0000 913.77 19.342 605.38 3824.3 0.4554 1.39841 +FS_19 Byp_Nozz.Fl_O 1257.54 22.297 630.42 150.79 0.0000 913.77 13.664 548.21 2706.4 0.8665 1.39841 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1610.34 1.609 0.9007 3692.626 1.1613 0.9071 -44530.5 27.86 16.68 +LPC 172.35 2.280 0.8660 3426.564 1.3037 0.8805 -15633.3 29.70 22.43 +HPC 86.51 5.665 0.8630 6351.431 1.7011 0.8904 -48990.3 20.08 20.06 +HPT 27.40 2.694 0.9144 153.018 1.2295 0.9049 48990.3 +LPT 72.02 4.650 0.9289 81.694 1.4083 0.9150 60163.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3087.61 1.424 0.9305 0.936 2.0601 0.5215 1.4369 0.9679 3943.9586 +LPC 184.87 1.392 0.9021 0.936 1.7659 0.9323 3.2631 0.9600 3662.6571 +HPC 205.67 22.564 0.8513 0.999 2.0758 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.988 0.9327 99.939 4.9877 1.4085 0.4249 0.9803 1.5311 +LPT 149.64 6.092 0.9277 100.719 6.0922 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 13823.84 10579.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1028.08 247.98 85.811 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1028.08 247.98 85.811 +Duct1 0.0025 0.4554 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1028.08 247.98 85.811 +Duct2 0.0025 0.4488 365.99 +Duct3 0.0050 0.2995 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3545 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.3434 1398.03 342.39 288.760 +Duct5 0.0075 0.4554 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 13.1111 1398.03 342.39 288.760 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 630.42 150.79 22.466 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.2753 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7995.1 32182.6 48990.3 +LP_Shaft 3777.7 83645.2 60163.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.00 0.9940 0.0550 4.82713 0.02225 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.632 0.9975 1.0000 0.9975 2706.36 0.867 992.1 38775.4 +Core_Nozz 1.570 0.9999 1.0000 0.9999 862.88 0.843 1489.9 11262.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 56 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 2000.0 27.00 1436.30 35512.9 0.4321 15343.42 5.4369 227.53 18.866 2631.5 2565.9 2056.7 + core size:20.05 Q: 55.10 Maximum Thrust: 39459.0 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1436.30 14.051 542.85 129.75 0.0000 1536.88 13.664 538.54 13272.9 0.2000 1.40005 +FS_2 Inlet.Fl_O 1436.30 13.966 542.85 129.75 0.0000 1546.16 11.685 515.87 5943.4 0.5111 1.40005 +FS_21 Fan.Fl_O 1436.30 21.744 623.37 149.09 0.0000 1064.25 18.954 599.44 4515.2 0.4473 1.39859 +FS_13 Splitter.Fl_O2 1213.17 21.744 623.37 149.09 0.0000 898.91 18.923 599.16 3795.6 0.4501 1.39859 +FS_22 Splitter.Fl_O1 223.14 21.744 623.37 149.09 0.0000 165.33 19.117 600.91 719.5 0.4329 1.39859 +FS_23 Duct1.Fl_O 223.14 21.689 623.37 149.09 0.0000 165.75 19.069 600.91 721.3 0.4329 1.39859 +FS_24 LPC.Fl_O 223.14 47.673 803.93 192.77 0.0000 85.64 41.659 773.95 366.0 0.4442 1.39176 +FS_25 Duct2.Fl_O 223.14 47.554 803.93 192.77 0.0000 85.85 41.555 773.95 366.9 0.4442 1.39176 +FS_3 HPC.Fl_O 223.14 265.083 1362.59 333.16 0.0000 20.05 249.283 1340.66 119.9 0.3019 1.35810 +FS_36 Bld3.Fl_O 203.05 265.083 1362.59 333.16 0.0000 18.25 249.283 1340.66 109.1 0.3019 1.35810 +FS_4 Burner.Fl_O 207.31 250.504 2631.54 702.43 0.0210 27.40 248.890 2627.66 483.4 0.0999 1.29654 +FS_45 HPT.Fl_O 227.40 92.575 2056.73 532.06 0.0191 71.88 87.293 2028.11 439.1 0.3001 1.31274 +FS_48 Duct3.Fl_O 227.40 92.112 2056.73 532.06 0.0191 72.25 86.856 2028.11 441.4 0.3001 1.31274 +FS_5 LPT.Fl_O 227.40 20.376 1466.61 367.02 0.0191 275.78 18.832 1437.58 1477.4 0.3446 1.33892 +FS_7 Duct4.Fl_O 227.40 20.173 1466.61 367.02 0.0191 278.57 19.372 1451.65 2018.9 0.2464 1.33892 +FS_9 Core_Nozz.Fl_O 227.40 20.173 1466.61 367.02 0.0191 278.57 13.664 1327.80 862.9 0.7796 1.33892 +FS_15 BypBld.Fl_O 1213.17 21.744 623.37 149.09 0.0000 898.91 18.923 599.16 3795.6 0.4501 1.39859 +FS_17 Duct5.Fl_O 1213.17 21.580 623.37 149.09 0.0000 905.70 18.781 599.16 3824.3 0.4501 1.39859 +FS_19 Byp_Nozz.Fl_O 1213.17 21.580 623.37 149.09 0.0000 905.70 13.664 547.14 2706.4 0.8351 1.39859 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1546.16 1.557 0.9080 3555.081 1.1483 0.9135 -39310.1 31.16 16.86 +LPC 165.75 2.198 0.8635 3317.526 1.2896 0.8777 -13789.4 29.24 20.93 +HPC 85.85 5.574 0.8637 6332.457 1.6949 0.8909 -44321.0 21.37 21.41 +HPT 27.40 2.706 0.9145 153.685 1.2328 0.9049 44320.9 +LPT 72.25 4.521 0.9272 80.196 1.4024 0.9131 53099.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2964.49 1.388 0.9380 0.901 1.9700 0.5215 1.4369 0.9679 3943.9586 +LPC 177.79 1.367 0.8995 0.906 1.7388 0.9323 3.2631 0.9600 3662.6571 +HPC 204.09 22.146 0.8521 0.996 2.0981 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.015 0.9329 100.374 5.0152 1.4085 0.4249 0.9803 1.5311 +LPT 150.12 5.911 0.9260 98.872 5.9110 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 13272.92 10157.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1003.71 241.91 79.422 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1003.71 241.91 79.422 +Duct1 0.0025 0.4329 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1003.71 241.91 79.422 +Duct2 0.0025 0.4442 365.99 +Duct3 0.0050 0.3001 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3446 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.8097 1362.59 333.16 265.083 +Duct5 0.0075 0.4501 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.2724 1362.59 333.16 265.083 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 623.37 149.09 21.744 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.4369 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7883.8 29526.2 44320.9 +LP_Shaft 3637.0 76680.2 53099.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2631.54 0.9940 0.0550 4.26206 0.02099 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.579 0.9975 1.0000 0.9975 2706.36 0.835 955.2 36017.5 +Core_Nozz 1.476 0.9999 1.0000 0.9999 862.88 0.780 1365.8 9652.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 57 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 2000.0 27.00 1370.87 31567.3 0.4266 13468.10 5.6056 227.53 17.208 2536.0 2473.3 1978.1 + core size:20.17 Q: 55.10 Maximum Thrust: 39459.0 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1370.87 14.051 542.85 129.75 0.0000 1466.86 13.664 538.54 12668.2 0.2000 1.40005 +FS_2 Inlet.Fl_O 1370.87 13.966 542.85 129.75 0.0000 1475.73 11.935 519.00 5943.4 0.4791 1.40005 +FS_21 Fan.Fl_O 1370.87 20.992 616.40 147.42 0.0000 1046.21 18.406 593.72 4515.2 0.4376 1.39875 +FS_13 Splitter.Fl_O2 1163.34 20.992 616.40 147.42 0.0000 887.83 18.348 593.18 3795.6 0.4429 1.39875 +FS_22 Splitter.Fl_O1 207.53 20.992 616.40 147.42 0.0000 158.38 18.698 596.39 719.5 0.4101 1.39875 +FS_23 Duct1.Fl_O 207.53 20.940 616.40 147.42 0.0000 158.78 18.651 596.39 721.3 0.4101 1.39875 +FS_24 LPC.Fl_O 207.53 44.202 785.49 188.29 0.0000 84.91 38.737 756.77 366.0 0.4392 1.39265 +FS_25 Duct2.Fl_O 207.53 44.092 785.49 188.29 0.0000 85.12 38.641 756.77 366.9 0.4392 1.39265 +FS_3 HPC.Fl_O 207.53 241.789 1326.52 323.80 0.0000 20.17 227.189 1304.79 119.9 0.3037 1.36028 +FS_36 Bld3.Fl_O 188.85 241.789 1326.52 323.80 0.0000 18.36 227.189 1304.79 109.1 0.3037 1.36028 +FS_4 Burner.Fl_O 192.59 228.490 2536.00 672.90 0.0198 27.39 227.019 2532.23 483.4 0.0998 1.29945 +FS_45 HPT.Fl_O 211.27 84.114 1978.11 508.92 0.0180 72.09 79.287 1950.18 439.1 0.3006 1.31622 +FS_48 Duct3.Fl_O 211.27 83.694 1978.11 508.92 0.0180 72.45 78.890 1950.18 441.4 0.3006 1.31622 +FS_5 LPT.Fl_O 211.27 19.246 1420.17 354.13 0.0180 266.95 17.888 1393.87 1477.4 0.3315 1.34225 +FS_7 Duct4.Fl_O 211.27 19.053 1420.17 354.13 0.0180 269.65 18.347 1406.55 2018.9 0.2377 1.34225 +FS_9 Core_Nozz.Fl_O 211.27 19.053 1420.17 354.13 0.0180 269.65 13.664 1303.89 862.8 0.7173 1.34225 +FS_15 BypBld.Fl_O 1163.34 20.992 616.40 147.42 0.0000 887.83 18.348 593.18 3795.6 0.4429 1.39875 +FS_17 Duct5.Fl_O 1163.34 20.835 616.40 147.42 0.0000 894.54 18.211 593.18 3824.3 0.4429 1.39875 +FS_19 Byp_Nozz.Fl_O 1163.34 20.835 616.40 147.42 0.0000 894.54 13.664 546.47 2706.4 0.8003 1.39875 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1475.73 1.503 0.9105 3409.774 1.1355 0.9155 -34268.0 34.24 16.85 +LPC 158.78 2.111 0.8607 3199.867 1.2743 0.8744 -11999.8 28.78 19.48 +HPC 85.12 5.484 0.8644 6313.774 1.6888 0.8913 -39791.6 22.62 22.69 +HPT 27.39 2.716 0.9147 154.291 1.2357 0.9047 39791.7 +LPT 72.45 4.349 0.9251 78.432 1.3929 0.9109 46267.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2829.50 1.350 0.9407 0.865 1.9155 0.5215 1.4369 0.9679 3943.9586 +LPC 170.31 1.340 0.8965 0.874 1.7129 0.9323 3.2631 0.9600 3662.6571 +HPC 202.37 21.727 0.8527 0.993 2.1148 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.040 0.9330 100.770 5.0398 1.4085 0.4249 0.9803 1.5311 +LPT 150.54 5.671 0.9239 96.697 5.6713 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 12668.24 9694.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 978.78 235.72 73.054 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 978.78 235.72 73.054 +Duct1 0.0025 0.4101 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 978.78 235.72 73.054 +Duct2 0.0025 0.4392 365.99 +Duct3 0.0050 0.3006 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3315 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.2636 1326.52 323.80 241.789 +Duct5 0.0075 0.4429 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.4142 1326.52 323.80 241.789 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 616.40 147.42 20.992 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.6056 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7769.9 26897.5 39791.7 +LP_Shaft 3488.3 69661.3 46267.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2536.00 0.9940 0.0550 3.74114 0.01981 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.525 0.9975 1.0000 0.9975 2706.36 0.800 914.9 33078.7 +Core_Nozz 1.394 0.9999 1.0000 0.9999 862.88 0.717 1246.2 8183.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 58 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 2000.0 27.00 1222.02 23675.2 0.4219 9988.65 5.9653 227.53 13.923 2332.1 2275.5 1810.0 + core size:20.44 Q: 55.10 Maximum Thrust: 39459.0 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1222.02 14.051 542.85 129.75 0.0000 1307.59 13.664 538.54 11292.7 0.2000 1.40005 +FS_2 Inlet.Fl_O 1222.02 13.966 542.85 129.75 0.0000 1315.49 12.421 524.95 5943.4 0.4127 1.40005 +FS_21 Fan.Fl_O 1222.02 19.433 601.97 143.95 0.0000 995.59 17.301 582.33 4515.2 0.4110 1.39901 +FS_13 Splitter.Fl_O2 1046.58 19.433 601.97 143.95 0.0000 852.66 17.207 581.43 3795.6 0.4206 1.39901 +FS_22 Splitter.Fl_O1 175.44 19.433 601.97 143.95 0.0000 142.94 17.749 586.61 719.5 0.3622 1.39901 +FS_23 Duct1.Fl_O 175.44 19.384 601.97 143.95 0.0000 143.29 17.705 586.61 721.3 0.3622 1.39901 +FS_24 LPC.Fl_O 175.44 36.993 743.98 178.21 0.0000 83.47 32.601 717.82 366.0 0.4295 1.39450 +FS_25 Duct2.Fl_O 175.44 36.901 743.98 178.21 0.0000 83.68 32.519 717.82 366.9 0.4295 1.39450 +FS_3 HPC.Fl_O 175.44 195.621 1247.75 303.52 0.0000 20.44 183.468 1226.50 119.9 0.3077 1.36515 +FS_36 Bld3.Fl_O 159.65 195.621 1247.75 303.52 0.0000 18.60 183.468 1226.50 109.1 0.3077 1.36515 +FS_4 Burner.Fl_O 162.43 184.862 2332.14 610.85 0.0174 27.38 183.672 2328.61 483.4 0.0995 1.30597 +FS_45 HPT.Fl_O 178.22 67.383 1810.05 460.27 0.0158 72.61 63.457 1783.59 439.1 0.3021 1.32438 +FS_48 Duct3.Fl_O 178.22 67.046 1810.05 460.27 0.0158 72.98 63.139 1783.59 441.4 0.3021 1.32438 +FS_5 LPT.Fl_O 178.22 17.372 1329.25 329.19 0.0158 241.35 16.387 1309.30 1477.4 0.2952 1.34915 +FS_7 Duct4.Fl_O 178.22 17.198 1329.25 329.19 0.0158 243.79 16.682 1318.80 2018.9 0.2130 1.34915 +FS_9 Core_Nozz.Fl_O 178.22 17.198 1329.25 329.19 0.0158 243.79 13.664 1252.03 862.9 0.5918 1.34915 +FS_15 BypBld.Fl_O 1046.58 19.433 601.97 143.95 0.0000 852.66 17.207 581.43 3795.6 0.4206 1.39901 +FS_17 Duct5.Fl_O 1046.58 19.287 601.97 143.95 0.0000 859.10 17.078 581.43 3824.3 0.4206 1.39901 +FS_19 Byp_Nozz.Fl_O 1046.58 19.287 601.97 143.95 0.0000 859.10 13.664 545.55 2706.4 0.7194 1.39901 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1315.49 1.391 0.9083 3071.006 1.1089 0.9125 -24546.3 37.94 16.23 +LPC 143.29 1.908 0.8548 2916.308 1.2359 0.8672 -8504.6 28.72 16.94 +HPC 83.68 5.301 0.8647 6281.036 1.6771 0.8911 -31104.5 25.31 25.43 +HPT 27.38 2.743 0.9149 155.772 1.2431 0.9050 31104.5 +LPT 72.98 3.859 0.9216 73.846 1.3617 0.9080 33050.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2522.27 1.272 0.9384 0.779 1.8467 0.5215 1.4369 0.9679 3943.9586 +LPC 153.70 1.278 0.8903 0.796 1.6839 0.9323 3.2631 0.9600 3662.6571 +HPC 198.94 20.884 0.8531 0.988 2.1499 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.103 0.9333 101.737 5.1034 1.4085 0.4249 0.9803 1.5311 +LPT 151.64 4.989 0.9204 91.043 4.9888 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 11292.72 8642.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 923.56 222.07 60.154 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 923.56 222.07 60.154 +Duct1 0.0025 0.3622 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 923.56 222.07 60.154 +Duct2 0.0025 0.4295 365.99 +Duct3 0.0050 0.3021 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2952 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.1405 1247.75 303.52 195.621 +Duct5 0.0075 0.4206 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.6494 1247.75 303.52 195.621 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 601.97 143.95 19.433 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9653 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7522.6 21716.6 31104.5 +LP_Shaft 3141.8 55250.5 33050.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2332.14 0.9940 0.0550 2.77462 0.01738 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.411 0.9975 1.0000 0.9975 2706.36 0.719 821.6 26726.5 +Core_Nozz 1.259 0.9999 1.0000 0.9999 862.88 0.592 1009.4 5590.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 59 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 8/ 18/ 1/ 6 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 2000.0 27.00 1041.13 15783.6 0.4307 6797.93 6.3451 227.53 10.627 2090.8 2041.4 1613.0 + core size:20.79 Q: 55.10 Maximum Thrust: 39459.0 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1041.13 14.051 542.85 129.75 0.0000 1114.03 13.664 538.54 9621.1 0.2000 1.40005 +FS_2 Inlet.Fl_O 1041.13 13.966 542.85 129.75 0.0000 1120.76 12.888 530.52 5943.4 0.3407 1.40005 +FS_21 Fan.Fl_O 1041.13 17.806 585.91 140.09 0.0000 913.30 16.200 570.32 4515.2 0.3700 1.39926 +FS_13 Splitter.Fl_O2 899.38 17.806 585.91 140.09 0.0000 788.96 16.098 569.30 3795.6 0.3823 1.39926 +FS_22 Splitter.Fl_O1 141.74 17.806 585.91 140.09 0.0000 124.34 16.669 574.99 719.5 0.3085 1.39926 +FS_23 Duct1.Fl_O 141.74 17.761 585.91 140.09 0.0000 124.65 16.627 574.99 721.3 0.3085 1.39926 +FS_24 LPC.Fl_O 141.74 29.696 694.92 166.34 0.0000 81.20 26.390 672.02 366.0 0.4145 1.39618 +FS_25 Duct2.Fl_O 141.74 29.622 694.92 166.34 0.0000 81.40 26.324 672.02 366.9 0.4145 1.39618 +FS_3 HPC.Fl_O 141.74 149.322 1152.33 279.21 0.0000 20.79 139.701 1131.71 119.9 0.3129 1.37115 +FS_36 Bld3.Fl_O 128.99 149.322 1152.33 279.21 0.0000 18.92 139.701 1131.71 109.1 0.3129 1.37115 +FS_4 Burner.Fl_O 130.88 141.109 2090.81 539.14 0.0146 27.37 140.202 2087.58 483.4 0.0991 1.31466 +FS_45 HPT.Fl_O 143.63 50.927 1612.99 404.67 0.0133 73.09 47.918 1588.49 439.1 0.3030 1.33516 +FS_48 Duct3.Fl_O 143.63 50.672 1612.99 404.67 0.0133 73.46 47.679 1588.49 441.4 0.3030 1.33516 +FS_5 LPT.Fl_O 143.63 15.937 1235.32 303.82 0.0133 204.41 15.301 1222.16 1477.4 0.2455 1.35668 +FS_7 Duct4.Fl_O 143.63 15.778 1235.32 303.82 0.0133 206.47 15.441 1228.33 2018.9 0.1785 1.35668 +FS_9 Core_Nozz.Fl_O 143.63 15.778 1235.32 303.82 0.0133 206.47 13.664 1189.42 862.9 0.4640 1.35668 +FS_15 BypBld.Fl_O 899.38 17.806 585.91 140.09 0.0000 788.96 16.098 569.30 3795.6 0.3823 1.39926 +FS_17 Duct5.Fl_O 899.38 17.672 585.91 140.09 0.0000 794.92 15.978 569.30 3824.3 0.3823 1.39926 +FS_19 Byp_Nozz.Fl_O 899.38 17.672 585.91 140.09 0.0000 794.92 13.664 544.41 2706.4 0.6176 1.39926 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1120.76 1.275 0.9055 2647.412 1.0793 0.9087 -15230.7 38.16 14.59 +LPC 124.65 1.672 0.8470 2548.258 1.1860 0.8577 -5264.4 31.51 14.47 +HPC 81.40 5.041 0.8644 6237.165 1.6582 0.8905 -22635.0 29.13 29.31 +HPT 27.37 2.771 0.9154 157.889 1.2523 0.9050 22635.0 +LPT 73.46 3.180 0.9107 67.437 1.3057 0.8973 20495.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2148.91 1.191 0.9355 0.671 1.7977 0.5215 1.4369 0.9679 3943.9586 +LPC 133.71 1.206 0.8823 0.696 1.6931 0.9323 3.2631 0.9600 3662.6571 +HPC 193.52 19.681 0.8527 0.981 2.1812 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.168 0.9338 103.120 5.1678 1.4085 0.4249 0.9803 1.5311 +LPT 152.65 4.040 0.9096 83.142 4.0404 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 9621.10 7362.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 857.47 205.84 47.158 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 857.47 205.84 47.158 +Duct1 0.0025 0.3085 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 857.47 205.84 47.158 +Duct2 0.0025 0.4145 365.99 +Duct3 0.0050 0.3030 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2455 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.9611 1152.33 279.21 149.322 +Duct5 0.0075 0.3823 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.7960 1152.33 279.21 149.322 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 585.91 140.09 17.806 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.3451 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7219.5 16466.6 22635.0 +LP_Shaft 2708.4 39743.5 20495.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2090.81 0.9940 0.0550 1.88831 0.01464 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.293 0.9975 1.0000 0.9975 2706.36 0.618 704.6 19696.3 +Core_Nozz 1.155 0.9999 1.0000 0.9999 862.88 0.464 772.9 3450.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 60 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 2000.0 27.00 803.65 7891.7 0.4786 3777.03 6.7005 227.53 7.160 1759.3 1720.0 1345.8 + core size:21.41 Q: 55.10 Maximum Thrust: 39459.0 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 803.65 14.051 542.85 129.75 0.0000 859.93 13.664 538.54 7426.6 0.2000 1.40005 +FS_2 Inlet.Fl_O 803.65 13.966 542.85 129.75 0.0000 865.12 13.348 535.86 5943.4 0.2552 1.40005 +FS_21 Fan.Fl_O 803.65 16.113 567.83 135.75 0.0000 766.93 15.122 557.63 4515.2 0.3025 1.39957 +FS_13 Splitter.Fl_O2 699.29 16.113 567.83 135.75 0.0000 667.34 15.045 556.82 3795.6 0.3145 1.39957 +FS_22 Splitter.Fl_O1 104.36 16.113 567.83 135.75 0.0000 99.60 15.471 561.27 719.5 0.2418 1.39957 +FS_23 Duct1.Fl_O 104.36 16.073 567.83 135.75 0.0000 99.84 15.432 561.27 721.3 0.2418 1.39957 +FS_24 LPC.Fl_O 104.36 22.073 632.47 151.28 0.0000 76.73 19.914 614.19 366.0 0.3864 1.39836 +FS_25 Duct2.Fl_O 104.36 22.018 632.47 151.28 0.0000 76.92 19.865 614.19 366.9 0.3864 1.39836 +FS_3 HPC.Fl_O 104.36 100.599 1022.80 246.66 0.0000 21.41 93.698 1002.98 119.9 0.3224 1.37929 +FS_36 Bld3.Fl_O 94.97 100.599 1022.80 246.66 0.0000 19.48 93.698 1002.98 109.1 0.3224 1.37929 +FS_4 Burner.Fl_O 96.02 95.066 1759.27 443.87 0.0110 27.34 94.457 1756.46 483.4 0.0984 1.32987 +FS_45 HPT.Fl_O 105.41 33.947 1345.83 331.86 0.0101 73.51 31.919 1324.39 439.1 0.3029 1.35202 +FS_48 Duct3.Fl_O 105.41 33.777 1345.83 331.86 0.0101 73.88 31.759 1324.39 441.4 0.3029 1.35202 +FS_5 LPT.Fl_O 105.41 14.824 1110.25 270.78 0.0101 152.89 14.500 1103.69 1477.4 0.1800 1.36685 +FS_7 Duct4.Fl_O 105.41 14.676 1110.25 270.78 0.0101 154.44 14.503 1106.72 2018.9 0.1319 1.36685 +FS_9 Core_Nozz.Fl_O 105.41 14.676 1110.25 270.78 0.0101 154.44 13.664 1089.12 862.8 0.3248 1.36685 +FS_15 BypBld.Fl_O 699.29 16.113 567.83 135.75 0.0000 667.34 15.045 556.82 3795.6 0.3145 1.39957 +FS_17 Duct5.Fl_O 699.29 15.992 567.83 135.75 0.0000 672.38 14.932 556.82 3824.3 0.3145 1.39957 +FS_19 Byp_Nozz.Fl_O 699.29 15.992 567.83 135.75 0.0000 672.38 13.664 542.87 2706.4 0.4795 1.39957 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 865.12 1.154 0.9061 2036.314 1.0460 0.9080 -6817.2 42.84 10.48 +LPC 99.84 1.373 0.8320 1991.019 1.1138 0.8393 -2294.0 41.69 12.56 +HPC 76.92 4.569 0.8625 6157.240 1.6172 0.8879 -14083.8 36.60 37.03 +HPT 27.34 2.800 0.9164 162.104 1.2664 0.9055 14084.3 +LPT 73.88 2.279 0.8946 56.786 1.2122 0.8838 9110.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1658.75 1.107 0.9361 0.516 1.7964 0.5215 1.4369 0.9679 3943.9586 +LPC 107.10 1.114 0.8666 0.544 1.8144 0.9323 3.2631 0.9600 3662.6571 +HPC 182.87 17.499 0.8509 0.969 2.2355 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.238 0.9347 105.873 5.2376 1.4085 0.4249 0.9803 1.5311 +LPT 153.51 2.783 0.8935 70.010 2.7835 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 7426.57 5683.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 770.59 184.66 33.530 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 770.59 184.66 33.530 +Duct1 0.0025 0.2418 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 770.59 184.66 33.530 +Duct2 0.0025 0.3864 365.99 +Duct3 0.0050 0.3029 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1800 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.6527 1022.80 246.66 100.599 +Duct5 0.0075 0.3145 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.7400 1022.80 246.66 100.599 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 567.83 135.75 16.113 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.7005 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6799.2 10879.5 14084.3 +LP_Shaft 2083.2 22969.9 9110.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1759.27 0.9940 0.0550 1.04917 0.01105 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.170 0.9975 1.0000 0.9975 2706.36 0.479 546.3 11873.4 +Core_Nozz 1.074 0.9999 1.0000 0.9999 862.88 0.325 519.4 1701.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:44 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 61 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 2/ 12/ 1/ 0 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 2000.0 27.00 1513.94 37805.1 0.4623 17477.00 5.3043 284.42 20.384 2730.0 2661.5 2138.4 + core size:19.93 Q: 86.09 Maximum Thrust: 37805.1 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1513.94 14.271 545.27 130.33 0.0000 1598.45 13.664 538.54 11192.3 0.2500 1.40000 +FS_2 Inlet.Fl_O 1513.94 14.186 545.27 130.33 0.0000 1608.11 11.621 515.06 5943.4 0.5413 1.40000 +FS_21 Fan.Fl_O 1513.94 22.732 632.47 151.28 0.0000 1080.77 19.707 607.24 4515.2 0.4565 1.39836 +FS_13 Splitter.Fl_O2 1273.79 22.732 632.47 151.28 0.0000 909.33 19.701 607.18 3795.6 0.4570 1.39836 +FS_22 Splitter.Fl_O1 240.14 22.732 632.47 151.28 0.0000 171.43 19.740 607.53 719.5 0.4537 1.39836 +FS_23 Duct1.Fl_O 240.14 22.676 632.47 151.28 0.0000 171.86 19.691 607.53 721.3 0.4537 1.39836 +FS_24 LPC.Fl_O 240.14 51.649 824.24 197.72 0.0000 86.14 45.041 793.10 366.0 0.4477 1.39079 +FS_25 Duct2.Fl_O 240.14 51.520 824.24 197.72 0.0000 86.35 44.928 793.10 366.9 0.4477 1.39079 +FS_3 HPC.Fl_O 240.14 290.913 1400.37 343.00 0.0000 19.93 273.787 1378.22 119.9 0.3002 1.35588 +FS_36 Bld3.Fl_O 218.53 290.913 1400.37 343.00 0.0000 18.14 273.787 1378.22 109.1 0.3002 1.35588 +FS_4 Burner.Fl_O 223.39 274.913 2730.00 733.15 0.0222 27.40 273.142 2726.00 483.4 0.1000 1.29380 +FS_45 HPT.Fl_O 245.00 102.026 2138.39 556.33 0.0202 71.66 96.243 2109.08 439.1 0.2995 1.30938 +FS_48 Duct3.Fl_O 245.00 101.516 2138.39 556.33 0.0202 72.02 95.762 2109.08 441.4 0.2995 1.30938 +FS_5 LPT.Fl_O 245.00 21.790 1517.89 381.35 0.0202 282.67 20.046 1486.35 1477.4 0.3552 1.33543 +FS_7 Duct4.Fl_O 245.00 21.572 1517.89 381.35 0.0202 285.52 20.671 1501.69 2018.9 0.2534 1.33543 +FS_9 Core_Nozz.Fl_O 245.00 21.572 1517.89 381.35 0.0202 285.52 13.664 1351.88 862.8 0.8483 1.33543 +FS_15 BypBld.Fl_O 1273.79 22.732 632.47 151.28 0.0000 909.33 19.701 607.18 3795.6 0.4570 1.39836 +FS_17 Duct5.Fl_O 1273.79 22.562 632.47 151.28 0.0000 916.21 19.553 607.18 3824.3 0.4570 1.39836 +FS_19 Byp_Nozz.Fl_O 1273.79 22.562 632.47 151.28 0.0000 916.21 13.664 548.14 2706.4 0.8777 1.39836 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1608.11 1.602 0.9008 3683.630 1.1599 0.9071 -44876.5 28.35 16.93 +LPC 171.86 2.278 0.8658 3420.288 1.3032 0.8803 -15779.2 29.53 22.22 +HPC 86.35 5.647 0.8632 6346.871 1.6990 0.8905 -49362.0 20.30 20.30 +HPT 27.40 2.695 0.9144 153.130 1.2296 0.9050 49360.2 +LPT 72.02 4.659 0.9288 81.676 1.4088 0.9148 60655.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3083.31 1.419 0.9306 0.934 2.0689 0.5215 1.4369 0.9679 3943.9586 +LPC 184.35 1.392 0.9018 0.934 1.7608 0.9323 3.2631 0.9600 3662.6571 +HPC 205.30 22.481 0.8516 0.998 2.0783 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 4.988 0.9328 100.012 4.9883 1.4085 0.4249 0.9803 1.5311 +LPT 149.65 6.104 0.9276 100.696 6.1039 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 11192.25 13383.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1030.46 248.57 86.591 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1030.46 248.57 86.591 +Duct1 0.0025 0.4537 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1030.46 248.57 86.591 +Duct2 0.0025 0.4477 365.99 +Duct3 0.0050 0.2995 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3552 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.4050 1400.37 343.00 290.913 +Duct5 0.0075 0.4570 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 13.2079 1400.37 343.00 290.913 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 632.47 151.28 22.732 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3043 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 8000.9 32401.8 49360.2 +LP_Shaft 3776.9 84346.9 60655.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.00 0.9940 0.0550 4.85472 0.02222 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.651 0.9975 1.0000 0.9975 2706.36 0.878 1004.8 39778.9 +Core_Nozz 1.579 0.9999 1.0000 0.9999 862.88 0.848 1498.3 11409.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 62 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 2000.0 27.00 1456.18 34024.4 0.4547 15472.34 5.4660 284.42 18.753 2633.3 2567.7 2058.3 + core size:20.07 Q: 86.09 Maximum Thrust: 37805.1 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1456.18 14.271 545.27 130.33 0.0000 1537.47 13.664 538.54 10765.3 0.2500 1.40000 +FS_2 Inlet.Fl_O 1456.18 14.186 545.27 130.33 0.0000 1546.76 11.866 518.14 5943.4 0.5114 1.40000 +FS_21 Fan.Fl_O 1456.18 22.020 625.57 149.62 0.0000 1067.32 19.176 601.38 4515.2 0.4490 1.39854 +FS_13 Splitter.Fl_O2 1230.98 22.020 625.57 149.62 0.0000 902.26 19.137 601.04 3795.6 0.4523 1.39854 +FS_22 Splitter.Fl_O1 225.20 22.020 625.57 149.62 0.0000 165.07 19.370 603.12 719.5 0.4320 1.39854 +FS_23 Duct1.Fl_O 225.20 21.965 625.57 149.62 0.0000 165.48 19.322 603.12 721.3 0.4320 1.39854 +FS_24 LPC.Fl_O 225.20 48.318 807.00 193.52 0.0000 85.44 42.256 777.08 366.0 0.4429 1.39161 +FS_25 Duct2.Fl_O 225.20 48.197 807.00 193.52 0.0000 85.65 42.150 777.08 366.9 0.4429 1.39161 +FS_3 HPC.Fl_O 225.20 267.633 1365.78 333.99 0.0000 20.07 251.652 1343.76 119.9 0.3022 1.35791 +FS_36 Bld3.Fl_O 204.94 267.633 1365.78 333.99 0.0000 18.26 251.652 1343.76 109.1 0.3022 1.35791 +FS_4 Burner.Fl_O 209.23 252.913 2633.26 702.93 0.0210 27.39 251.284 2629.37 483.4 0.0999 1.29652 +FS_45 HPT.Fl_O 229.50 93.478 2058.32 532.51 0.0191 71.88 88.146 2029.68 439.1 0.3001 1.31270 +FS_48 Duct3.Fl_O 229.50 93.011 2058.32 532.51 0.0191 72.24 87.705 2029.68 441.4 0.3001 1.31270 +FS_5 LPT.Fl_O 229.50 20.505 1466.67 367.03 0.0191 276.60 18.941 1437.45 1477.4 0.3458 1.33893 +FS_7 Duct4.Fl_O 229.50 20.300 1466.67 367.03 0.0191 279.39 19.490 1451.62 2018.9 0.2472 1.33893 +FS_9 Core_Nozz.Fl_O 229.50 20.300 1466.67 367.03 0.0191 279.39 13.664 1325.70 862.9 0.7862 1.33893 +FS_15 BypBld.Fl_O 1230.98 22.020 625.57 149.62 0.0000 902.26 19.137 601.04 3795.6 0.4523 1.39854 +FS_17 Duct5.Fl_O 1230.98 21.855 625.57 149.62 0.0000 909.07 18.994 601.04 3824.3 0.4523 1.39854 +FS_19 Byp_Nozz.Fl_O 1230.98 21.855 625.57 149.62 0.0000 909.07 13.664 547.10 2706.4 0.8474 1.39854 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1546.76 1.552 0.9080 3551.692 1.1473 0.9135 -39744.9 31.67 17.16 +LPC 165.48 2.200 0.8633 3315.917 1.2900 0.8774 -13987.0 29.01 20.73 +HPC 85.65 5.553 0.8640 6327.234 1.6924 0.8911 -44758.1 21.63 21.68 +HPT 27.39 2.706 0.9146 153.800 1.2327 0.9049 44758.1 +LPT 72.24 4.536 0.9272 80.268 1.4034 0.9130 53731.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2965.62 1.384 0.9380 0.901 1.9841 0.5215 1.4369 0.9679 3943.9586 +LPC 177.50 1.368 0.8992 0.905 1.7330 0.9323 3.2631 0.9600 3662.6571 +HPC 203.63 22.047 0.8524 0.995 2.0999 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.014 0.9329 100.450 5.0143 1.4085 0.4249 0.9803 1.5311 +LPT 150.10 5.933 0.9260 98.960 5.9326 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 10765.30 12872.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1006.83 242.68 80.345 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1006.83 242.68 80.345 +Duct1 0.0025 0.4320 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1006.83 242.68 80.345 +Duct2 0.0025 0.4429 365.99 +Duct3 0.0050 0.3001 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3458 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.8822 1365.78 333.99 267.633 +Duct5 0.0075 0.4523 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.3863 1365.78 333.99 267.633 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 625.57 149.62 22.020 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.4660 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7892.3 29785.3 44758.1 +LP_Shaft 3641.6 77494.3 53731.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2633.26 0.9940 0.0550 4.29787 0.02097 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.599 0.9975 1.0000 0.9975 2706.36 0.847 969.2 37080.0 +Core_Nozz 1.486 0.9999 1.0000 0.9999 862.88 0.786 1376.3 9817.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 63 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 2000.0 27.00 1392.84 30244.1 0.4502 13615.34 5.6388 284.42 17.139 2539.3 2476.6 1981.0 + core size:20.19 Q: 86.09 Maximum Thrust: 37805.1 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1392.84 14.271 545.27 130.33 0.0000 1470.59 13.664 538.54 10297.0 0.2500 1.40000 +FS_2 Inlet.Fl_O 1392.84 14.186 545.27 130.33 0.0000 1479.48 12.110 521.16 5943.4 0.4807 1.40000 +FS_21 Fan.Fl_O 1392.84 21.278 618.71 147.97 0.0000 1050.68 18.630 595.71 4515.2 0.4400 1.39870 +FS_13 Splitter.Fl_O2 1183.03 21.278 618.71 147.97 0.0000 892.41 18.565 595.11 3795.6 0.4459 1.39870 +FS_22 Splitter.Fl_O1 209.80 21.278 618.71 147.97 0.0000 158.26 18.956 598.66 719.5 0.4097 1.39870 +FS_23 Duct1.Fl_O 209.80 21.225 618.71 147.97 0.0000 158.66 18.909 598.66 721.3 0.4097 1.39870 +FS_24 LPC.Fl_O 209.80 44.891 788.95 189.13 0.0000 84.71 39.372 760.27 366.0 0.4379 1.39248 +FS_25 Duct2.Fl_O 209.80 44.779 788.95 189.13 0.0000 84.92 39.274 760.27 366.9 0.4379 1.39248 +FS_3 HPC.Fl_O 209.80 244.603 1330.39 324.80 0.0000 20.19 229.808 1308.56 119.9 0.3040 1.36004 +FS_36 Bld3.Fl_O 190.92 244.603 1330.39 324.80 0.0000 18.37 229.808 1308.56 109.1 0.3040 1.36004 +FS_4 Burner.Fl_O 194.70 231.150 2539.28 673.87 0.0198 27.39 229.661 2535.50 483.4 0.0998 1.29937 +FS_45 HPT.Fl_O 213.59 85.114 1980.98 509.74 0.0180 72.07 80.231 1953.03 439.1 0.3006 1.31611 +FS_48 Duct3.Fl_O 213.59 84.689 1980.98 509.74 0.0180 72.43 79.830 1953.03 441.4 0.3006 1.31611 +FS_5 LPT.Fl_O 213.59 19.373 1420.67 354.27 0.0180 268.15 17.992 1394.10 1477.4 0.3333 1.34222 +FS_7 Duct4.Fl_O 213.59 19.179 1420.67 354.27 0.0180 270.86 18.462 1406.92 2018.9 0.2388 1.34222 +FS_9 Core_Nozz.Fl_O 213.59 19.179 1420.67 354.27 0.0180 270.86 13.664 1302.15 862.8 0.7246 1.34222 +FS_15 BypBld.Fl_O 1183.03 21.278 618.71 147.97 0.0000 892.41 18.565 595.11 3795.6 0.4459 1.39870 +FS_17 Duct5.Fl_O 1183.03 21.118 618.71 147.97 0.0000 899.16 18.425 595.11 3824.3 0.4459 1.39870 +FS_19 Byp_Nozz.Fl_O 1183.03 21.118 618.71 147.97 0.0000 899.16 13.664 546.41 2706.4 0.8138 1.39870 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1479.48 1.500 0.9110 3410.127 1.1347 0.9159 -34765.4 34.79 17.21 +LPC 158.66 2.115 0.8604 3201.345 1.2751 0.8742 -12215.8 28.53 19.30 +HPC 84.92 5.462 0.8646 6308.925 1.6863 0.8914 -40275.0 22.87 22.96 +HPT 27.39 2.716 0.9147 154.411 1.2356 0.9047 40275.1 +LPT 72.43 4.372 0.9251 78.558 1.3944 0.9108 46980.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2836.69 1.348 0.9411 0.865 1.9333 0.5215 1.4369 0.9679 3943.9586 +LPC 170.18 1.342 0.8962 0.874 1.7069 0.9323 3.2631 0.9600 3662.6571 +HPC 201.89 21.629 0.8529 0.992 2.1161 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.038 0.9330 100.849 5.0382 1.4085 0.4249 0.9803 1.5311 +LPT 150.51 5.703 0.9239 96.852 5.7032 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 10296.99 12312.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 982.40 236.61 74.053 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 982.40 236.61 74.053 +Duct1 0.0025 0.4097 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 982.40 236.61 74.053 +Duct2 0.0025 0.4379 365.99 +Duct3 0.0050 0.3006 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3333 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.3431 1330.39 324.80 244.603 +Duct5 0.0075 0.4459 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.5392 1330.39 324.80 244.603 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 618.71 147.97 21.278 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.6388 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7781.0 27185.5 40275.1 +LP_Shaft 3496.5 70570.7 46980.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2539.28 0.9940 0.0550 3.78204 0.01981 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.545 0.9975 1.0000 0.9975 2706.36 0.814 930.2 34204.5 +Core_Nozz 1.404 0.9999 1.0000 0.9999 862.88 0.725 1258.2 8352.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 64 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 2000.0 27.00 1248.79 22682.9 0.4477 10154.07 6.0142 284.42 13.929 2338.4 2281.7 1815.4 + core size:20.46 Q: 86.09 Maximum Thrust: 37805.1 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1248.79 14.271 545.27 130.33 0.0000 1318.51 13.664 538.54 9232.1 0.2500 1.40000 +FS_2 Inlet.Fl_O 1248.79 14.186 545.27 130.33 0.0000 1326.47 12.585 526.93 5943.4 0.4170 1.40000 +FS_21 Fan.Fl_O 1248.79 19.731 604.46 144.55 0.0000 1004.09 17.523 584.34 4515.2 0.4153 1.39897 +FS_13 Splitter.Fl_O2 1070.76 19.731 604.46 144.55 0.0000 860.94 17.419 583.34 3795.6 0.4258 1.39897 +FS_22 Splitter.Fl_O1 178.04 19.731 604.46 144.55 0.0000 143.15 18.016 588.98 719.5 0.3628 1.39897 +FS_23 Duct1.Fl_O 178.04 19.682 604.46 144.55 0.0000 143.51 17.971 588.98 721.3 0.3628 1.39897 +FS_24 LPC.Fl_O 178.04 37.756 748.32 179.26 0.0000 83.24 33.302 722.20 366.0 0.4279 1.39433 +FS_25 Duct2.Fl_O 178.04 37.662 748.32 179.26 0.0000 83.45 33.219 722.20 366.9 0.4279 1.39433 +FS_3 HPC.Fl_O 178.04 198.793 1252.99 304.86 0.0000 20.46 186.424 1231.63 119.9 0.3080 1.36482 +FS_36 Bld3.Fl_O 162.01 198.793 1252.99 304.86 0.0000 18.62 186.424 1231.63 109.1 0.3080 1.36482 +FS_4 Burner.Fl_O 164.84 187.859 2338.37 612.70 0.0174 27.38 186.650 2334.84 483.4 0.0995 1.30578 +FS_45 HPT.Fl_O 180.86 68.514 1815.43 461.79 0.0158 72.58 64.525 1788.94 439.1 0.3019 1.32413 +FS_48 Duct3.Fl_O 180.86 68.171 1815.43 461.79 0.0158 72.94 64.203 1788.94 441.4 0.3019 1.32413 +FS_5 LPT.Fl_O 180.86 17.485 1330.27 329.47 0.0158 243.45 16.475 1309.91 1477.4 0.2980 1.34907 +FS_7 Duct4.Fl_O 180.86 17.310 1330.27 329.47 0.0158 245.90 16.781 1319.61 2018.9 0.2149 1.34907 +FS_9 Core_Nozz.Fl_O 180.86 17.310 1330.27 329.47 0.0158 245.90 13.664 1250.88 862.9 0.6003 1.34907 +FS_15 BypBld.Fl_O 1070.76 19.731 604.46 144.55 0.0000 860.94 17.419 583.34 3795.6 0.4258 1.39897 +FS_17 Duct5.Fl_O 1070.76 19.583 604.46 144.55 0.0000 867.44 17.289 583.34 3824.3 0.4258 1.39897 +FS_19 Byp_Nozz.Fl_O 1070.76 19.583 604.46 144.55 0.0000 867.44 13.664 545.43 2706.4 0.7359 1.39897 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1326.47 1.391 0.9102 3080.540 1.1085 0.9143 -25114.3 38.83 16.78 +LPC 143.51 1.918 0.8545 2925.839 1.2380 0.8670 -8745.1 28.33 16.77 +HPC 83.45 5.278 0.8649 6276.178 1.6744 0.8911 -31637.3 25.57 25.70 +HPT 27.38 2.742 0.9150 155.897 1.2428 0.9050 31637.3 +LPT 72.94 3.899 0.9217 74.131 1.3647 0.9080 33858.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2543.33 1.272 0.9404 0.781 1.8722 0.5215 1.4369 0.9679 3943.9586 +LPC 153.94 1.281 0.8900 0.799 1.6759 0.9323 3.2631 0.9600 3662.6571 +HPC 198.38 20.778 0.8532 0.987 2.1500 0.4206 0.2163 1.0137 6357.1603 +HPT 30.12 5.100 0.9333 101.819 5.0998 1.4085 0.4249 0.9803 1.5311 +LPT 151.57 5.044 0.9205 91.394 5.0439 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 9232.11 11039.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 928.24 223.22 61.268 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 928.24 223.22 61.268 +Duct1 0.0025 0.3628 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 928.24 223.22 61.268 +Duct2 0.0025 0.4279 365.99 +Duct3 0.0050 0.3019 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2980 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.2313 1252.99 304.86 198.793 +Duct5 0.0075 0.4258 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.7921 1252.99 304.86 198.793 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 604.46 144.55 19.731 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.0142 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7538.7 22041.4 31637.3 +LP_Shaft 3158.5 56301.0 33858.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2338.37 0.9940 0.0550 2.82057 0.01741 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.433 0.9975 1.0000 0.9975 2706.36 0.736 840.4 27969.6 +Core_Nozz 1.267 0.9999 1.0000 0.9999 862.88 0.600 1023.4 5752.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 65 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 2000.0 27.00 1073.94 15121.8 0.4606 6965.25 6.4303 284.42 10.696 2101.1 2051.5 1621.6 + core size:20.80 Q: 86.09 Maximum Thrust: 37805.1 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1073.94 14.271 545.27 130.33 0.0000 1133.89 13.664 538.54 7939.4 0.2500 1.40000 +FS_2 Inlet.Fl_O 1073.94 14.186 545.27 130.33 0.0000 1140.74 13.047 532.39 5943.4 0.3477 1.40000 +FS_21 Fan.Fl_O 1073.94 18.106 588.58 140.73 0.0000 928.56 16.411 572.30 4515.2 0.3774 1.39922 +FS_13 Splitter.Fl_O2 929.40 18.106 588.58 140.73 0.0000 803.59 16.296 571.15 3795.6 0.3909 1.39922 +FS_22 Splitter.Fl_O1 144.54 18.106 588.58 140.73 0.0000 124.97 16.938 577.48 719.5 0.3102 1.39922 +FS_23 Duct1.Fl_O 144.54 18.061 588.58 140.73 0.0000 125.28 16.895 577.48 721.3 0.3102 1.39922 +FS_24 LPC.Fl_O 144.54 30.467 700.12 167.60 0.0000 81.00 27.095 677.19 366.0 0.4133 1.39600 +FS_25 Duct2.Fl_O 144.54 30.391 700.12 167.60 0.0000 81.20 27.027 677.19 366.9 0.4133 1.39600 +FS_3 HPC.Fl_O 144.54 152.651 1159.32 280.98 0.0000 20.80 142.805 1138.58 119.9 0.3131 1.37071 +FS_36 Bld3.Fl_O 131.53 152.651 1159.32 280.98 0.0000 18.93 142.805 1138.58 109.1 0.3131 1.37071 +FS_4 Burner.Fl_O 133.46 144.255 2101.07 542.13 0.0147 27.37 143.328 2097.83 483.4 0.0991 1.31429 +FS_45 HPT.Fl_O 146.47 52.097 1621.59 407.05 0.0134 73.06 49.023 1597.01 439.1 0.3029 1.33470 +FS_48 Duct3.Fl_O 146.47 51.836 1621.59 407.05 0.0134 73.42 48.777 1597.01 441.4 0.3029 1.33470 +FS_5 LPT.Fl_O 146.47 16.026 1237.06 304.29 0.0134 207.43 15.367 1223.47 1477.4 0.2494 1.35652 +FS_7 Duct4.Fl_O 146.47 15.866 1237.06 304.29 0.0134 209.52 15.517 1229.85 2018.9 0.1812 1.35652 +FS_9 Core_Nozz.Fl_O 146.47 15.866 1237.06 304.29 0.0134 209.52 13.664 1189.35 863.0 0.4731 1.35652 +FS_15 BypBld.Fl_O 929.40 18.106 588.58 140.73 0.0000 803.59 16.296 571.15 3795.6 0.3909 1.39922 +FS_17 Duct5.Fl_O 929.40 17.970 588.58 140.73 0.0000 809.66 16.174 571.15 3824.3 0.3909 1.39922 +FS_19 Byp_Nozz.Fl_O 929.40 17.970 588.58 140.73 0.0000 809.66 13.664 544.28 2706.4 0.6381 1.39922 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1140.74 1.276 0.9087 2668.363 1.0794 0.9119 -15801.5 39.72 15.47 +LPC 125.28 1.687 0.8469 2568.309 1.1895 0.8578 -5494.0 30.83 14.34 +HPC 81.20 5.023 0.8644 6233.734 1.6559 0.8904 -23185.7 29.35 29.54 +HPT 27.37 2.769 0.9154 158.005 1.2518 0.9050 23185.8 +LPT 73.42 3.234 0.9113 67.941 1.3108 0.8978 21295.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2187.21 1.192 0.9388 0.677 1.8367 0.5215 1.4369 0.9679 3943.9586 +LPC 134.38 1.211 0.8821 0.701 1.6814 0.9323 3.2631 0.9600 3662.6571 +HPC 193.05 19.597 0.8528 0.981 2.1807 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.163 0.9338 103.196 5.1635 1.4085 0.4249 0.9803 1.5311 +LPT 152.57 4.117 0.9101 83.763 4.1170 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 7939.43 9493.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 863.34 207.28 48.302 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 863.34 207.28 48.302 +Duct1 0.0025 0.3102 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 863.34 207.28 48.302 +Duct2 0.0025 0.4133 365.99 +Duct3 0.0050 0.3029 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2494 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.0587 1159.32 280.98 152.651 +Duct5 0.0075 0.3909 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.9494 1159.32 280.98 152.651 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 588.58 140.73 18.106 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.4303 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7242.5 16813.8 23185.8 +LP_Shaft 2735.9 40879.5 21295.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2101.07 0.9940 0.0550 1.93479 0.01471 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.315 0.9975 1.0000 0.9975 2706.36 0.638 728.0 21028.2 +Core_Nozz 1.161 0.9999 1.0000 0.9999 862.88 0.473 788.0 3587.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 66 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 2000.0 27.00 845.51 7560.9 0.5195 3927.70 6.8921 284.42 7.273 1776.5 1736.8 1359.9 + core size:21.40 Q: 86.09 Maximum Thrust: 37805.1 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 845.51 14.271 545.27 130.33 0.0000 892.71 13.664 538.54 6250.7 0.2500 1.40000 +FS_2 Inlet.Fl_O 845.51 14.186 545.27 130.33 0.0000 898.10 13.506 537.67 5943.4 0.2658 1.40000 +FS_21 Fan.Fl_O 845.51 16.399 570.63 136.42 0.0000 794.74 15.310 559.54 4515.2 0.3149 1.39952 +FS_13 Splitter.Fl_O2 738.38 16.399 570.63 136.42 0.0000 694.04 15.216 558.55 3795.6 0.3289 1.39952 +FS_22 Splitter.Fl_O1 107.13 16.399 570.63 136.42 0.0000 100.70 15.730 563.88 719.5 0.2446 1.39952 +FS_23 Duct1.Fl_O 107.13 16.358 570.63 136.42 0.0000 100.95 15.691 563.88 721.3 0.2446 1.39952 +FS_24 LPC.Fl_O 107.13 22.768 638.42 152.72 0.0000 76.72 20.542 619.98 366.0 0.3863 1.39819 +FS_25 Duct2.Fl_O 107.13 22.711 638.42 152.72 0.0000 76.91 20.491 619.98 366.9 0.3863 1.39819 +FS_3 HPC.Fl_O 107.13 103.789 1032.15 248.99 0.0000 21.40 96.676 1012.19 119.9 0.3223 1.37870 +FS_36 Bld3.Fl_O 97.49 103.789 1032.15 248.99 0.0000 19.47 96.676 1012.19 109.1 0.3223 1.37870 +FS_4 Burner.Fl_O 98.58 98.081 1776.52 448.71 0.0112 27.34 97.452 1773.70 483.4 0.0984 1.32900 +FS_45 HPT.Fl_O 108.23 35.053 1359.89 335.61 0.0102 73.47 32.961 1338.29 439.1 0.3029 1.35108 +FS_48 Duct3.Fl_O 108.23 34.878 1359.89 335.61 0.0102 73.84 32.796 1338.29 441.4 0.3029 1.35108 +FS_5 LPT.Fl_O 108.23 14.884 1114.65 271.93 0.0102 156.65 14.542 1107.73 1477.4 0.1847 1.36648 +FS_7 Duct4.Fl_O 108.23 14.735 1114.65 271.93 0.0102 158.23 14.552 1110.93 2018.9 0.1352 1.36648 +FS_9 Core_Nozz.Fl_O 108.23 14.735 1114.65 271.93 0.0102 158.23 13.664 1092.27 862.9 0.3340 1.36648 +FS_15 BypBld.Fl_O 738.38 16.399 570.63 136.42 0.0000 694.04 15.216 558.55 3795.6 0.3289 1.39952 +FS_17 Duct5.Fl_O 738.38 16.276 570.63 136.42 0.0000 699.29 15.102 558.55 3824.3 0.3289 1.39952 +FS_19 Byp_Nozz.Fl_O 738.38 16.276 570.63 136.42 0.0000 699.29 13.664 542.81 2706.4 0.5063 1.39952 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 898.10 1.156 0.9095 2072.782 1.0465 0.9114 -7280.6 45.51 11.84 +LPC 100.95 1.392 0.8322 2026.208 1.1188 0.8399 -2470.4 40.24 12.42 +HPC 76.91 4.570 0.8626 6157.061 1.6167 0.8879 -14593.6 36.55 36.98 +HPT 27.34 2.798 0.9163 162.068 1.2655 0.9055 14594.0 +LPT 73.84 2.343 0.8956 57.632 1.2200 0.8845 9750.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1721.99 1.109 0.9397 0.526 1.8597 0.5215 1.4369 0.9679 3943.9586 +LPC 108.29 1.120 0.8669 0.553 1.7914 0.9323 3.2631 0.9600 3662.6571 +HPC 182.85 17.503 0.8510 0.969 2.2344 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.232 0.9347 105.849 5.2319 1.4085 0.4249 0.9803 1.5311 +LPT 153.43 2.874 0.8944 71.053 2.8739 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 6250.70 7474.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 777.79 186.41 34.589 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 777.79 186.41 34.589 +Duct1 0.0025 0.2446 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 777.79 186.41 34.589 +Duct2 0.0025 0.3863 365.99 +Duct3 0.0050 0.3029 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1847 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.7497 1032.15 248.99 103.789 +Duct5 0.0075 0.3289 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.8924 1032.15 248.99 103.789 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 570.63 136.42 16.399 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.8921 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6831.0 11220.9 14594.0 +LP_Shaft 2125.3 24096.6 9750.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1776.52 0.9940 0.0550 1.09103 0.01119 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.191 0.9975 1.0000 0.9975 2706.36 0.506 576.8 13236.3 +Core_Nozz 1.078 0.9999 1.0000 0.9999 862.88 0.334 534.8 1798.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 67 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 2/ 12/ 1/ 0 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 2000.0 27.00 1535.79 36310.2 0.4847 17598.09 5.3386 341.30 20.181 2730.0 2661.6 2138.5 + core size:19.95 Q: 123.98 Maximum Thrust: 36310.2 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1535.79 14.545 548.23 131.04 0.0000 1595.39 13.664 538.54 9461.5 0.3000 1.39994 +FS_2 Inlet.Fl_O 1535.79 14.457 548.23 131.04 0.0000 1605.03 11.857 518.02 5943.4 0.5397 1.39994 +FS_21 Fan.Fl_O 1535.79 23.064 634.99 151.89 0.0000 1082.77 19.981 609.54 4515.2 0.4576 1.39829 +FS_13 Splitter.Fl_O2 1293.50 23.064 634.99 151.89 0.0000 911.95 19.966 609.42 3795.6 0.4587 1.39829 +FS_22 Splitter.Fl_O1 242.29 23.064 634.99 151.89 0.0000 170.82 20.054 610.18 719.5 0.4516 1.39829 +FS_23 Duct1.Fl_O 242.29 23.006 634.99 151.89 0.0000 171.25 20.004 610.18 721.3 0.4516 1.39829 +FS_24 LPC.Fl_O 242.29 52.321 827.16 198.43 0.0000 85.94 45.663 796.09 366.0 0.4464 1.39065 +FS_25 Duct2.Fl_O 242.29 52.190 827.16 198.43 0.0000 86.16 45.549 796.09 366.9 0.4464 1.39065 +FS_3 HPC.Fl_O 242.29 293.519 1403.19 343.74 0.0000 19.95 276.203 1380.95 119.9 0.3005 1.35571 +FS_36 Bld3.Fl_O 220.48 293.519 1403.19 343.74 0.0000 18.16 276.203 1380.95 109.1 0.3005 1.35571 +FS_4 Burner.Fl_O 225.37 277.376 2730.00 733.11 0.0222 27.39 275.589 2726.00 483.4 0.1000 1.29383 +FS_45 HPT.Fl_O 247.18 102.929 2138.48 556.34 0.0202 71.66 97.094 2109.16 439.1 0.2995 1.30941 +FS_48 Duct3.Fl_O 247.18 102.414 2138.48 556.34 0.0202 72.02 96.608 2109.16 441.4 0.2995 1.30941 +FS_5 LPT.Fl_O 247.18 21.938 1517.36 381.19 0.0202 283.21 20.174 1485.68 1477.4 0.3559 1.33548 +FS_7 Duct4.Fl_O 247.18 21.719 1517.36 381.19 0.0202 286.07 20.808 1501.09 2018.9 0.2539 1.33548 +FS_9 Core_Nozz.Fl_O 247.18 21.719 1517.36 381.19 0.0202 286.07 13.664 1349.04 862.8 0.8549 1.33548 +FS_15 BypBld.Fl_O 1293.50 23.064 634.99 151.89 0.0000 911.95 19.966 609.42 3795.6 0.4587 1.39829 +FS_17 Duct5.Fl_O 1293.50 22.891 634.99 151.89 0.0000 918.84 19.817 609.42 3824.3 0.4587 1.39829 +FS_19 Byp_Nozz.Fl_O 1293.50 22.891 634.99 151.89 0.0000 918.84 13.664 548.06 2706.4 0.8912 1.39829 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1605.03 1.595 0.9009 3672.399 1.1582 0.9072 -45295.9 28.93 17.21 +LPC 171.25 2.274 0.8654 3412.327 1.3026 0.8799 -15956.5 29.32 21.97 +HPC 86.16 5.624 0.8635 6341.283 1.6964 0.8907 -49811.7 20.58 20.59 +HPT 27.39 2.695 0.9145 153.265 1.2296 0.9050 49807.9 +LPT 72.02 4.668 0.9286 81.646 1.4093 0.9146 61252.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3077.40 1.414 0.9308 0.931 2.0775 0.5215 1.4369 0.9679 3943.9586 +LPC 183.69 1.390 0.9015 0.932 1.7544 0.9323 3.2631 0.9600 3662.6571 +HPC 204.84 22.376 0.8519 0.998 2.0813 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 4.989 0.9328 100.100 4.9890 1.4085 0.4249 0.9803 1.5311 +LPT 149.66 6.117 0.9274 100.659 6.1171 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 9461.49 16291.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1033.35 249.29 87.545 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1033.35 249.29 87.545 +Duct1 0.0025 0.4516 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1033.35 249.29 87.545 +Duct2 0.0025 0.4464 365.99 +Duct3 0.0050 0.2995 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3559 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.4802 1403.19 343.74 293.519 +Duct5 0.0075 0.4587 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 13.3260 1403.19 343.74 293.519 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 634.99 151.89 23.064 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3386 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 8008.0 32666.8 49807.9 +LP_Shaft 3775.6 85206.4 61252.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.00 0.9940 0.0550 4.88836 0.02217 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.675 0.9975 1.0000 0.9975 2706.36 0.891 1020.1 41012.8 +Core_Nozz 1.589 0.9999 1.0000 0.9999 862.88 0.855 1508.5 11588.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 68 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 2000.0 27.00 1479.86 32679.4 0.4779 15618.82 5.5013 341.30 18.605 2634.9 2569.5 2059.9 + core size:20.09 Q: 123.98 Maximum Thrust: 36310.2 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1479.86 14.545 548.23 131.04 0.0000 1537.29 13.664 538.54 9116.9 0.3000 1.39994 +FS_2 Inlet.Fl_O 1479.86 14.457 548.23 131.04 0.0000 1546.58 12.094 520.97 5943.4 0.5113 1.39994 +FS_21 Fan.Fl_O 1479.86 22.358 628.23 150.26 0.0000 1070.54 19.449 603.76 4515.2 0.4508 1.39847 +FS_13 Splitter.Fl_O2 1252.23 22.358 628.23 150.26 0.0000 905.87 19.403 603.36 3795.6 0.4547 1.39847 +FS_22 Splitter.Fl_O1 227.62 22.358 628.23 150.26 0.0000 164.67 19.683 605.82 719.5 0.4307 1.39847 +FS_23 Duct1.Fl_O 227.62 22.302 628.23 150.26 0.0000 165.08 19.634 605.82 721.3 0.4307 1.39847 +FS_24 LPC.Fl_O 227.62 49.082 810.58 194.39 0.0000 85.20 42.964 780.75 366.0 0.4413 1.39144 +FS_25 Duct2.Fl_O 227.62 48.959 810.58 194.39 0.0000 85.42 42.856 780.75 366.9 0.4413 1.39144 +FS_3 HPC.Fl_O 227.62 270.604 1369.46 334.95 0.0000 20.09 254.411 1347.35 119.9 0.3026 1.35770 +FS_36 Bld3.Fl_O 207.14 270.604 1369.46 334.95 0.0000 18.28 254.411 1347.35 109.1 0.3026 1.35770 +FS_4 Burner.Fl_O 211.48 255.721 2634.95 703.41 0.0209 27.39 254.074 2631.06 483.4 0.0999 1.29650 +FS_45 HPT.Fl_O 231.96 94.527 2059.89 532.94 0.0191 71.87 89.136 2031.24 439.1 0.3000 1.31267 +FS_48 Duct3.Fl_O 231.96 94.055 2059.89 532.94 0.0191 72.23 88.690 2031.24 441.4 0.3000 1.31267 +FS_5 LPT.Fl_O 231.96 20.657 1466.64 367.01 0.0191 277.50 19.069 1437.20 1477.4 0.3471 1.33895 +FS_7 Duct4.Fl_O 231.96 20.450 1466.64 367.01 0.0191 280.31 19.628 1451.48 2018.9 0.2481 1.33895 +FS_9 Core_Nozz.Fl_O 231.96 20.450 1466.64 367.01 0.0191 280.31 13.664 1323.14 862.9 0.7938 1.33895 +FS_15 BypBld.Fl_O 1252.23 22.358 628.23 150.26 0.0000 905.87 19.403 603.36 3795.6 0.4547 1.39847 +FS_17 Duct5.Fl_O 1252.23 22.190 628.23 150.26 0.0000 912.72 19.258 603.36 3824.3 0.4547 1.39847 +FS_19 Byp_Nozz.Fl_O 1252.23 22.190 628.23 150.26 0.0000 912.72 13.664 547.05 2706.4 0.8620 1.39847 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1546.58 1.546 0.9080 3546.099 1.1459 0.9134 -40244.9 32.27 17.49 +LPC 165.08 2.201 0.8629 3312.629 1.2903 0.8771 -14212.3 28.74 20.49 +HPC 85.42 5.527 0.8643 6321.181 1.6895 0.8912 -45266.2 21.94 22.00 +HPT 27.39 2.705 0.9146 153.945 1.2327 0.9050 45266.0 +LPT 72.23 4.553 0.9271 80.328 1.4045 0.9128 54457.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2965.32 1.380 0.9380 0.899 1.9991 0.5215 1.4369 0.9679 3943.9586 +LPC 177.07 1.368 0.8988 0.904 1.7259 0.9323 3.2631 0.9600 3662.6571 +HPC 203.06 21.928 0.8526 0.994 2.1021 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.014 0.9329 100.544 5.0135 1.4085 0.4249 0.9803 1.5311 +LPT 150.09 5.957 0.9259 99.034 5.9566 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 9116.93 15698.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1010.46 243.59 81.430 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1010.46 243.59 81.430 +Duct1 0.0025 0.4307 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1010.46 243.59 81.430 +Duct2 0.0025 0.4413 365.99 +Duct3 0.0050 0.3000 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3471 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.9669 1369.46 334.95 270.604 +Duct5 0.0075 0.4547 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.5193 1369.46 334.95 270.604 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 628.23 150.26 22.358 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5013 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7902.3 30085.3 45266.0 +LP_Shaft 3645.8 78451.5 54457.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2634.95 0.9940 0.0550 4.33856 0.02095 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.624 0.9975 1.0000 0.9975 2706.36 0.862 985.8 38367.9 +Core_Nozz 1.497 0.9999 1.0000 0.9999 862.88 0.794 1388.4 10009.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 69 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 2000.0 27.00 1418.57 29048.2 0.4743 13776.38 5.6786 341.30 17.037 2542.4 2479.7 1983.7 + core size:20.21 Q: 123.98 Maximum Thrust: 36310.2 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1418.57 14.545 548.23 131.04 0.0000 1473.62 13.664 538.54 8739.3 0.3000 1.39994 +FS_2 Inlet.Fl_O 1418.57 14.457 548.23 131.04 0.0000 1482.52 12.331 523.87 5943.4 0.4821 1.39994 +FS_21 Fan.Fl_O 1418.57 21.623 621.49 148.64 0.0000 1055.37 18.904 598.12 4515.2 0.4425 1.39864 +FS_13 Splitter.Fl_O2 1206.16 21.623 621.49 148.64 0.0000 897.34 18.829 597.45 3795.6 0.4491 1.39864 +FS_22 Splitter.Fl_O1 212.41 21.623 621.49 148.64 0.0000 158.02 19.272 601.42 719.5 0.4090 1.39864 +FS_23 Duct1.Fl_O 212.41 21.569 621.49 148.64 0.0000 158.42 19.224 601.42 721.3 0.4090 1.39864 +FS_24 LPC.Fl_O 212.41 45.697 792.95 190.10 0.0000 84.46 40.117 764.35 366.0 0.4363 1.39228 +FS_25 Duct2.Fl_O 212.41 45.583 792.95 190.10 0.0000 84.67 40.017 764.35 366.9 0.4363 1.39228 +FS_3 HPC.Fl_O 212.41 247.794 1334.74 325.93 0.0000 20.21 232.774 1312.81 119.9 0.3044 1.35978 +FS_36 Bld3.Fl_O 193.29 247.794 1334.74 325.93 0.0000 18.39 232.774 1312.81 109.1 0.3044 1.35978 +FS_4 Burner.Fl_O 197.12 234.166 2542.37 674.78 0.0198 27.39 232.658 2538.59 483.4 0.0997 1.29931 +FS_45 HPT.Fl_O 216.23 86.245 1983.73 510.51 0.0180 72.06 81.299 1955.76 439.1 0.3005 1.31602 +FS_48 Duct3.Fl_O 216.23 85.814 1983.73 510.51 0.0180 72.42 80.893 1955.76 441.4 0.3005 1.31602 +FS_5 LPT.Fl_O 216.23 19.518 1420.94 354.34 0.0180 269.48 18.112 1394.07 1477.4 0.3351 1.34221 +FS_7 Duct4.Fl_O 216.23 19.323 1420.94 354.34 0.0180 272.20 18.592 1407.04 2018.9 0.2401 1.34221 +FS_9 Core_Nozz.Fl_O 216.23 19.323 1420.94 354.34 0.0180 272.20 13.664 1299.88 862.9 0.7329 1.34221 +FS_15 BypBld.Fl_O 1206.16 21.623 621.49 148.64 0.0000 897.34 18.829 597.45 3795.6 0.4491 1.39864 +FS_17 Duct5.Fl_O 1206.16 21.461 621.49 148.64 0.0000 904.12 18.688 597.45 3824.3 0.4491 1.39864 +FS_19 Byp_Nozz.Fl_O 1206.16 21.461 621.49 148.64 0.0000 904.12 13.664 546.35 2706.4 0.8297 1.39864 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1482.52 1.496 0.9113 3408.541 1.1336 0.9162 -35320.4 35.43 17.61 +LPC 158.42 2.119 0.8600 3201.366 1.2759 0.8739 -12459.6 28.23 19.07 +HPC 84.67 5.436 0.8648 6303.106 1.6833 0.8915 -40820.4 23.19 23.28 +HPT 27.39 2.715 0.9147 154.566 1.2355 0.9048 40820.4 +LPT 72.42 4.397 0.9250 78.680 1.3961 0.9107 47780.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2842.54 1.345 0.9415 0.864 1.9525 0.5215 1.4369 0.9679 3943.9586 +LPC 169.93 1.343 0.8958 0.874 1.6995 0.9323 3.2631 0.9600 3662.6571 +HPC 201.30 21.507 0.8531 0.991 2.1179 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.037 0.9330 100.950 5.0367 1.4085 0.4249 0.9803 1.5311 +LPT 150.48 5.738 0.9238 97.003 5.7383 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 8739.34 15048.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 986.54 237.64 75.207 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 986.54 237.64 75.207 +Duct1 0.0025 0.4090 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 986.54 237.64 75.207 +Duct2 0.0025 0.4363 365.99 +Duct3 0.0050 0.3005 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3351 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.4342 1334.74 325.93 247.794 +Duct5 0.0075 0.4491 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.6823 1334.74 325.93 247.794 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 621.49 148.64 21.623 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.6786 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7793.5 27509.2 40820.4 +LP_Shaft 3504.3 71610.2 47780.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2542.37 0.9940 0.0550 3.82677 0.01980 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.571 0.9975 1.0000 0.9975 2706.36 0.830 948.3 35551.0 +Core_Nozz 1.414 0.9999 1.0000 0.9999 862.88 0.733 1271.5 8545.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 70 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 2000.0 27.00 1279.28 21786.1 0.4740 10327.23 6.0719 341.30 13.905 2344.2 2287.5 1820.5 + core size:20.48 Q: 123.98 Maximum Thrust: 36310.2 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1279.28 14.545 548.23 131.04 0.0000 1328.92 13.664 538.54 7881.2 0.3000 1.39994 +FS_2 Inlet.Fl_O 1279.28 14.457 548.23 131.04 0.0000 1336.95 12.796 529.44 5943.4 0.4212 1.39994 +FS_21 Fan.Fl_O 1279.28 20.085 607.40 145.25 0.0000 1012.95 17.791 586.75 4515.2 0.4199 1.39892 +FS_13 Splitter.Fl_O2 1098.38 20.085 607.40 145.25 0.0000 869.71 17.675 585.66 3795.6 0.4313 1.39892 +FS_22 Splitter.Fl_O1 180.90 20.085 607.40 145.25 0.0000 143.24 18.337 591.83 719.5 0.3631 1.39892 +FS_23 Duct1.Fl_O 180.90 20.035 607.40 145.25 0.0000 143.59 18.291 591.83 721.3 0.3631 1.39892 +FS_24 LPC.Fl_O 180.90 38.621 753.20 180.44 0.0000 82.95 34.102 727.14 366.0 0.4261 1.39413 +FS_25 Duct2.Fl_O 180.90 38.525 753.20 180.44 0.0000 83.16 34.017 727.14 366.9 0.4261 1.39413 +FS_3 HPC.Fl_O 180.90 202.249 1258.65 306.31 0.0000 20.48 189.639 1237.16 119.9 0.3083 1.36446 +FS_36 Bld3.Fl_O 164.61 202.249 1258.65 306.31 0.0000 18.63 189.639 1237.16 109.1 0.3083 1.36446 +FS_4 Burner.Fl_O 167.48 191.125 2344.22 614.42 0.0174 27.38 189.895 2340.68 483.4 0.0995 1.30561 +FS_45 HPT.Fl_O 183.76 69.743 1820.55 463.23 0.0159 72.55 65.687 1794.02 439.1 0.3018 1.32390 +FS_48 Duct3.Fl_O 183.76 69.395 1820.55 463.23 0.0159 72.91 65.359 1794.02 441.4 0.3018 1.32390 +FS_5 LPT.Fl_O 183.76 17.610 1330.94 329.65 0.0159 245.66 16.572 1310.16 1477.4 0.3010 1.34902 +FS_7 Duct4.Fl_O 183.76 17.434 1330.94 329.65 0.0159 248.15 16.890 1320.07 2018.9 0.2170 1.34902 +FS_9 Core_Nozz.Fl_O 183.76 17.434 1330.94 329.65 0.0159 248.15 13.664 1249.19 862.9 0.6095 1.34902 +FS_15 BypBld.Fl_O 1098.38 20.085 607.40 145.25 0.0000 869.71 17.675 585.66 3795.6 0.4313 1.39892 +FS_17 Duct5.Fl_O 1098.38 19.934 607.40 145.25 0.0000 876.28 17.542 585.66 3824.3 0.4313 1.39892 +FS_19 Byp_Nozz.Fl_O 1098.38 19.934 607.40 145.25 0.0000 876.28 13.664 545.32 2706.4 0.7548 1.39892 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1336.95 1.389 0.9118 3088.178 1.1079 0.9158 -25723.5 39.80 17.38 +LPC 143.59 1.928 0.8540 2933.905 1.2400 0.8667 -9006.7 27.89 16.56 +HPC 83.16 5.250 0.8650 6270.326 1.6711 0.8911 -32214.1 25.91 26.05 +HPT 27.38 2.740 0.9150 156.063 1.2425 0.9050 32214.1 +LPT 72.91 3.941 0.9217 74.411 1.3679 0.9079 34729.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2563.42 1.271 0.9420 0.783 1.8999 0.5215 1.4369 0.9679 3943.9586 +LPC 154.03 1.284 0.8895 0.801 1.6663 0.9323 3.2631 0.9600 3662.6571 +HPC 197.70 20.646 0.8533 0.986 2.1504 0.4206 0.2163 1.0137 6357.1603 +HPT 30.12 5.096 0.9333 101.928 5.0962 1.4085 0.4249 0.9803 1.5311 +LPT 151.50 5.102 0.9205 91.740 5.1022 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 7881.22 13570.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 933.42 224.50 62.510 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 933.42 224.50 62.510 +Duct1 0.0025 0.3631 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 933.42 224.50 62.510 +Duct2 0.0025 0.4261 365.99 +Duct3 0.0050 0.3018 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3010 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.3313 1258.65 306.31 202.249 +Duct5 0.0075 0.4313 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.9492 1258.65 306.31 202.249 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 607.40 145.25 20.085 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.0719 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7556.1 22391.3 32214.1 +LP_Shaft 3175.0 57450.4 34729.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2344.22 0.9940 0.0550 2.86868 0.01743 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.459 0.9975 1.0000 0.9975 2706.36 0.755 861.9 29425.5 +Core_Nozz 1.276 0.9999 1.0000 0.9999 862.88 0.610 1038.5 5931.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 71 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 2000.0 27.00 1110.46 14523.9 0.4913 7135.13 6.5267 341.30 10.738 2110.5 2060.9 1629.6 + core size:20.82 Q: 123.98 Maximum Thrust: 36310.2 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1110.46 14.545 548.23 131.04 0.0000 1153.56 13.664 538.54 6841.2 0.3000 1.39994 +FS_2 Inlet.Fl_O 1110.46 14.457 548.23 131.04 0.0000 1160.53 13.252 534.76 5943.4 0.3548 1.39994 +FS_21 Fan.Fl_O 1110.46 18.458 591.71 141.48 0.0000 944.33 16.663 574.68 4515.2 0.3851 1.39917 +FS_13 Splitter.Fl_O2 962.93 18.458 591.71 141.48 0.0000 818.87 16.532 573.39 3795.6 0.4000 1.39917 +FS_22 Splitter.Fl_O1 147.54 18.458 591.71 141.48 0.0000 125.46 17.257 580.45 719.5 0.3116 1.39917 +FS_23 Duct1.Fl_O 147.54 18.412 591.71 141.48 0.0000 125.78 17.214 580.45 721.3 0.3116 1.39917 +FS_24 LPC.Fl_O 147.54 31.328 705.85 168.98 0.0000 80.74 27.886 682.92 366.0 0.4116 1.39581 +FS_25 Duct2.Fl_O 147.54 31.250 705.85 168.98 0.0000 80.94 27.816 682.92 366.9 0.4116 1.39581 +FS_3 HPC.Fl_O 147.54 156.186 1166.65 282.84 0.0000 20.82 146.095 1145.76 119.9 0.3135 1.37024 +FS_36 Bld3.Fl_O 134.26 156.186 1166.65 282.84 0.0000 18.95 146.095 1145.76 109.1 0.3135 1.37024 +FS_4 Burner.Fl_O 136.24 147.596 2110.54 544.87 0.0148 27.36 146.647 2107.29 483.4 0.0991 1.31395 +FS_45 HPT.Fl_O 149.52 53.338 1629.58 409.26 0.0134 73.02 50.194 1604.93 439.1 0.3028 1.33428 +FS_48 Duct3.Fl_O 149.52 53.071 1629.58 409.26 0.0134 73.39 49.943 1604.93 441.4 0.3028 1.33428 +FS_5 LPT.Fl_O 149.52 16.124 1238.16 304.59 0.0134 210.56 15.439 1224.12 1477.4 0.2535 1.35642 +FS_7 Duct4.Fl_O 149.52 15.962 1238.16 304.59 0.0134 212.69 15.600 1230.72 2018.9 0.1841 1.35642 +FS_9 Core_Nozz.Fl_O 149.52 15.962 1238.16 304.59 0.0134 212.69 13.664 1188.52 862.9 0.4827 1.35642 +FS_15 BypBld.Fl_O 962.93 18.458 591.71 141.48 0.0000 818.87 16.532 573.39 3795.6 0.4000 1.39917 +FS_17 Duct5.Fl_O 962.93 18.320 591.71 141.48 0.0000 825.06 16.408 573.39 3824.3 0.4000 1.39917 +FS_19 Byp_Nozz.Fl_O 962.93 18.320 591.71 141.48 0.0000 825.06 13.664 544.18 2706.4 0.6611 1.39917 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1160.53 1.277 0.9113 2687.533 1.0793 0.9143 -16401.3 41.40 16.41 +LPC 125.78 1.702 0.8465 2586.922 1.1929 0.8576 -5740.2 30.08 14.16 +HPC 80.94 4.998 0.8644 6229.218 1.6528 0.8903 -23766.4 29.67 29.86 +HPT 27.36 2.767 0.9154 158.178 1.2514 0.9050 23766.5 +LPT 73.39 3.292 0.9119 68.447 1.3161 0.8983 22141.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2225.16 1.193 0.9415 0.681 1.8790 0.5215 1.4369 0.9679 3943.9586 +LPC 134.92 1.215 0.8818 0.706 1.6679 0.9323 3.2631 0.9600 3662.6571 +HPC 192.42 19.482 0.8528 0.980 2.1806 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.159 0.9338 103.309 5.1593 1.4085 0.4249 0.9803 1.5311 +LPT 152.49 4.197 0.9108 84.386 4.1966 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 6841.22 11779.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 869.67 208.83 49.553 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 869.67 208.83 49.553 +Duct1 0.0025 0.3116 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 869.67 208.83 49.553 +Duct2 0.0025 0.4116 365.99 +Duct3 0.0050 0.3028 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2535 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.1638 1166.65 282.84 156.186 +Duct5 0.0075 0.4000 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.1145 1166.65 282.84 156.186 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 591.71 141.48 18.458 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.5267 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7266.8 17177.3 23766.5 +LP_Shaft 2763.1 42086.2 22141.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2110.54 0.9940 0.0550 1.98198 0.01476 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.341 0.9975 1.0000 0.9975 2706.36 0.661 754.1 22568.1 +Core_Nozz 1.168 0.9999 1.0000 0.9999 862.88 0.483 803.9 3735.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 72 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 2000.0 27.00 891.23 7261.9 0.5617 4078.96 7.0931 341.30 7.368 1792.2 1752.2 1372.7 + core size:21.40 Q: 123.98 Maximum Thrust: 36310.2 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 891.23 14.545 548.23 131.04 0.0000 925.82 13.664 538.54 5490.6 0.3000 1.39994 +FS_2 Inlet.Fl_O 891.23 14.457 548.23 131.04 0.0000 931.41 13.709 539.97 5943.4 0.2766 1.39994 +FS_21 Fan.Fl_O 891.23 16.735 573.91 137.21 0.0000 823.28 15.534 561.84 4515.2 0.3278 1.39946 +FS_13 Splitter.Fl_O2 781.11 16.735 573.91 137.21 0.0000 721.55 15.420 560.65 3795.6 0.3440 1.39946 +FS_22 Splitter.Fl_O1 110.12 16.735 573.91 137.21 0.0000 101.73 16.037 566.98 719.5 0.2473 1.39946 +FS_23 Duct1.Fl_O 110.12 16.693 573.91 137.21 0.0000 101.98 15.997 566.98 721.3 0.2473 1.39946 +FS_24 LPC.Fl_O 110.12 23.553 644.95 154.29 0.0000 76.62 21.257 626.38 366.0 0.3857 1.39798 +FS_25 Duct2.Fl_O 110.12 23.494 644.95 154.29 0.0000 76.81 21.204 626.38 366.9 0.3857 1.39798 +FS_3 HPC.Fl_O 110.12 107.170 1041.75 251.39 0.0000 21.40 99.823 1021.62 119.9 0.3224 1.37810 +FS_36 Bld3.Fl_O 100.21 107.170 1041.75 251.39 0.0000 19.47 99.823 1021.62 109.1 0.3224 1.37810 +FS_4 Burner.Fl_O 101.34 101.276 1792.24 453.12 0.0113 27.34 100.626 1789.39 483.4 0.0985 1.32824 +FS_45 HPT.Fl_O 111.26 36.222 1372.74 339.03 0.0103 73.43 34.062 1351.00 439.1 0.3028 1.35023 +FS_48 Duct3.Fl_O 111.26 36.041 1372.74 339.03 0.0103 73.80 33.892 1351.00 441.4 0.3028 1.35023 +FS_5 LPT.Fl_O 111.26 14.949 1117.81 272.76 0.0103 160.56 14.588 1110.50 1477.4 0.1895 1.36621 +FS_7 Duct4.Fl_O 111.26 14.800 1117.81 272.76 0.0103 162.18 14.607 1113.89 2018.9 0.1387 1.36621 +FS_9 Core_Nozz.Fl_O 111.26 14.800 1117.81 272.76 0.0103 162.18 13.664 1094.09 862.9 0.3436 1.36621 +FS_15 BypBld.Fl_O 781.11 16.735 573.91 137.21 0.0000 721.55 15.420 560.65 3795.6 0.3440 1.39946 +FS_17 Duct5.Fl_O 781.11 16.609 573.91 137.21 0.0000 727.00 15.304 560.65 3824.3 0.3440 1.39946 +FS_19 Byp_Nozz.Fl_O 781.11 16.609 573.91 137.21 0.0000 727.00 13.664 542.78 2706.4 0.5355 1.39946 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 931.41 1.158 0.9113 2108.214 1.0468 0.9132 -7771.2 48.32 13.33 +LPC 101.98 1.411 0.8332 2060.521 1.1238 0.8411 -2661.4 38.78 12.23 +HPC 76.81 4.562 0.8626 6155.158 1.6152 0.8879 -15129.4 36.66 37.09 +HPT 27.34 2.796 0.9163 162.128 1.2648 0.9055 15129.6 +LPT 73.80 2.411 0.8966 58.500 1.2281 0.8852 10432.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1785.85 1.110 0.9415 0.535 1.9275 0.5215 1.4369 0.9679 3943.9586 +LPC 109.39 1.126 0.8679 0.563 1.7677 0.9323 3.2631 0.9600 3662.6571 +HPC 182.61 17.464 0.8510 0.968 2.2349 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.227 0.9347 105.889 5.2271 1.4085 0.4249 0.9803 1.5311 +LPT 153.35 2.968 0.8954 72.123 2.9681 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 5490.58 9454.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 785.44 188.27 35.753 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 785.44 188.27 35.753 +Duct1 0.0025 0.2473 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 785.44 188.27 35.753 +Duct2 0.0025 0.3857 365.99 +Duct3 0.0050 0.3028 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1895 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.8543 1041.75 251.39 107.170 +Duct5 0.0075 0.3440 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.0567 1041.75 251.39 107.170 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 573.91 137.21 16.735 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.0931 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6863.7 11577.3 15129.6 +LP_Shaft 2167.5 25279.3 10432.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1792.24 0.9940 0.0550 1.13305 0.01131 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.216 0.9975 1.0000 0.9975 2706.36 0.536 610.1 14811.9 +Core_Nozz 1.083 0.9999 1.0000 0.9999 862.88 0.344 550.7 1904.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 73 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 2000.0 27.00 1592.51 33830.9 0.5298 17924.58 5.4204 455.07 19.693 2730.0 2661.9 2138.7 + core size:20.01 Q: 220.40 Maximum Thrust: 33830.9 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1592.51 15.257 555.77 132.85 0.0000 1587.91 13.664 538.54 7358.2 0.4000 1.39979 +FS_2 Inlet.Fl_O 1592.51 15.180 555.77 132.85 0.0000 1595.91 12.490 525.64 5943.4 0.5352 1.39979 +FS_21 Fan.Fl_O 1592.51 23.958 641.47 153.45 0.0000 1086.36 20.729 615.55 4515.2 0.4596 1.39809 +FS_13 Splitter.Fl_O2 1344.47 23.958 641.47 153.45 0.0000 917.16 20.696 615.27 3795.6 0.4622 1.39809 +FS_22 Splitter.Fl_O1 248.04 23.958 641.47 153.45 0.0000 169.20 20.901 617.00 719.5 0.4461 1.39809 +FS_23 Duct1.Fl_O 248.04 23.898 641.47 153.45 0.0000 169.63 20.849 617.00 721.3 0.4461 1.39809 +FS_24 LPC.Fl_O 248.04 54.123 834.61 200.25 0.0000 85.43 47.332 803.74 366.0 0.4431 1.39030 +FS_25 Duct2.Fl_O 248.04 53.988 834.61 200.25 0.0000 85.65 47.214 803.74 366.9 0.4431 1.39030 +FS_3 HPC.Fl_O 248.04 300.448 1410.30 345.60 0.0000 20.01 282.621 1387.83 119.9 0.3015 1.35530 +FS_36 Bld3.Fl_O 225.71 300.448 1410.30 345.60 0.0000 18.21 282.621 1387.83 109.1 0.3015 1.35530 +FS_4 Burner.Fl_O 230.69 283.923 2730.00 733.00 0.0221 27.39 282.094 2726.00 483.4 0.1000 1.29391 +FS_45 HPT.Fl_O 253.02 105.328 2138.71 556.34 0.0201 71.69 99.352 2109.36 439.1 0.2996 1.30947 +FS_48 Duct3.Fl_O 253.02 104.801 2138.71 556.34 0.0201 72.05 98.856 2109.36 441.4 0.2996 1.30947 +FS_5 LPT.Fl_O 253.02 22.342 1516.12 380.82 0.0201 284.54 20.526 1484.12 1477.4 0.3579 1.33561 +FS_7 Duct4.Fl_O 253.02 22.118 1516.12 380.82 0.0201 287.42 21.181 1499.70 2018.9 0.2552 1.33561 +FS_9 Core_Nozz.Fl_O 253.02 22.118 1516.12 380.82 0.0201 287.42 13.664 1341.60 862.9 0.8725 1.33561 +FS_15 BypBld.Fl_O 1344.47 23.958 641.47 153.45 0.0000 917.16 20.696 615.27 3795.6 0.4622 1.39809 +FS_17 Duct5.Fl_O 1344.47 23.778 641.47 153.45 0.0000 924.09 20.541 615.27 3824.3 0.4622 1.39809 +FS_19 Byp_Nozz.Fl_O 1344.47 23.778 641.47 153.45 0.0000 924.09 13.664 547.69 2706.4 0.9260 1.39809 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1595.91 1.578 0.9016 3643.358 1.1542 0.9077 -46407.8 30.31 17.80 +LPC 169.63 2.265 0.8644 3391.276 1.3011 0.8790 -16426.1 28.78 21.31 +HPC 85.65 5.565 0.8642 6327.312 1.6898 0.8911 -51006.7 21.31 21.36 +HPT 27.39 2.696 0.9145 153.615 1.2298 0.9051 51006.7 +LPT 72.05 4.691 0.9281 81.551 1.4106 0.9140 62834.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3059.93 1.402 0.9314 0.924 2.0901 0.5215 1.4369 0.9679 3943.9586 +LPC 181.95 1.388 0.9004 0.926 1.7375 0.9323 3.2631 0.9600 3662.6571 +HPC 203.62 22.104 0.8526 0.995 2.0887 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 4.991 0.9329 100.329 4.9908 1.4085 0.4249 0.9803 1.5311 +LPT 149.71 6.149 0.9269 100.542 6.1486 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 7358.22 22524.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1040.69 251.13 90.094 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1040.69 251.13 90.094 +Duct1 0.0025 0.4461 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1040.69 251.13 90.094 +Duct2 0.0025 0.4431 365.99 +Duct3 0.0050 0.2996 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3579 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.6813 1410.30 345.60 300.448 +Duct5 0.0075 0.4622 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 13.6421 1410.30 345.60 300.448 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 641.47 153.45 23.958 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.4204 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 8026.3 33376.9 51006.7 +LP_Shaft 3771.4 87503.3 62834.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.00 0.9940 0.0550 4.97905 0.02206 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.740 0.9975 1.0000 0.9975 2706.36 0.926 1059.7 44280.1 +Core_Nozz 1.619 0.9999 1.0000 0.9999 862.88 0.872 1535.5 12075.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 74 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 4/ 14/ 1/ 2 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 2000.0 27.00 1540.03 30448.0 0.5248 15979.44 5.5877 455.07 18.226 2638.0 2572.8 2062.9 + core size:20.14 Q: 220.40 Maximum Thrust: 33830.9 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1540.03 15.257 555.77 132.85 0.0000 1535.59 13.664 538.54 7115.7 0.4000 1.39979 +FS_2 Inlet.Fl_O 1540.03 15.180 555.77 132.85 0.0000 1543.32 12.712 528.30 5943.4 0.5098 1.39979 +FS_21 Fan.Fl_O 1540.03 23.258 635.00 151.89 0.0000 1076.71 20.190 609.92 4515.2 0.4542 1.39829 +FS_13 Splitter.Fl_O2 1306.26 23.258 635.00 151.89 0.0000 913.27 20.124 609.34 3795.6 0.4596 1.39829 +FS_22 Splitter.Fl_O1 233.77 23.258 635.00 151.89 0.0000 163.44 20.523 612.77 719.5 0.4267 1.39829 +FS_23 Duct1.Fl_O 233.77 23.200 635.00 151.89 0.0000 163.85 20.472 612.77 721.3 0.4267 1.39829 +FS_24 LPC.Fl_O 233.77 51.030 819.30 196.52 0.0000 84.61 44.771 789.67 366.0 0.4375 1.39102 +FS_25 Duct2.Fl_O 233.77 50.902 819.30 196.52 0.0000 84.83 44.659 789.67 366.9 0.4375 1.39102 +FS_3 HPC.Fl_O 233.77 278.067 1378.24 337.23 0.0000 20.14 261.331 1355.87 119.9 0.3035 1.35717 +FS_36 Bld3.Fl_O 212.73 278.067 1378.24 337.23 0.0000 18.33 261.331 1355.87 109.1 0.3035 1.35717 +FS_4 Burner.Fl_O 217.17 262.773 2638.05 704.27 0.0209 27.39 261.080 2634.15 483.4 0.0999 1.29650 +FS_45 HPT.Fl_O 238.21 97.150 2062.86 533.76 0.0190 71.86 91.610 2034.18 439.1 0.3000 1.31262 +FS_48 Duct3.Fl_O 238.21 96.664 2062.86 533.76 0.0190 72.22 91.152 2034.18 441.4 0.3000 1.31262 +FS_5 LPT.Fl_O 238.21 21.047 1466.18 366.86 0.0190 279.66 19.401 1436.22 1477.4 0.3502 1.33902 +FS_7 Duct4.Fl_O 238.21 20.836 1466.18 366.86 0.0190 282.48 19.985 1450.77 2018.9 0.2501 1.33902 +FS_9 Core_Nozz.Fl_O 238.21 20.836 1466.18 366.86 0.0190 282.48 13.664 1316.34 862.9 0.8129 1.33902 +FS_15 BypBld.Fl_O 1306.26 23.258 635.00 151.89 0.0000 913.27 20.124 609.34 3795.6 0.4596 1.39829 +FS_17 Duct5.Fl_O 1306.26 23.083 635.00 151.89 0.0000 920.17 19.973 609.34 3824.3 0.4596 1.39829 +FS_19 Byp_Nozz.Fl_O 1306.26 23.083 635.00 151.89 0.0000 920.17 13.664 546.76 2706.3 0.8989 1.39829 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1543.32 1.532 0.9080 3527.789 1.1426 0.9133 -41488.9 33.65 18.20 +LPC 163.85 2.200 0.8618 3300.370 1.2902 0.8761 -14759.8 28.08 19.84 +HPC 84.83 5.463 0.8649 6306.733 1.6822 0.8915 -46541.9 22.72 22.81 +HPT 27.39 2.705 0.9146 154.326 1.2326 0.9050 46543.1 +LPT 72.22 4.593 0.9268 80.403 1.4070 0.9123 56247.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2958.94 1.370 0.9380 0.894 2.0273 0.5215 1.4369 0.9679 3943.9586 +LPC 175.75 1.368 0.8977 0.901 1.7079 0.9323 3.2631 0.9600 3662.6571 +HPC 201.65 21.631 0.8532 0.992 2.1077 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.012 0.9330 100.793 5.0125 1.4085 0.4249 0.9803 1.5311 +LPT 150.07 6.012 0.9256 99.127 6.0120 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 7115.74 21782.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1019.21 245.77 84.182 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1019.21 245.77 84.182 +Duct1 0.0025 0.4267 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1019.21 245.77 84.182 +Duct2 0.0025 0.4375 365.99 +Duct3 0.0050 0.3000 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3502 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.1821 1378.24 337.23 278.067 +Duct5 0.0075 0.4596 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.8575 1378.24 337.23 278.067 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 635.00 151.89 23.258 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5877 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7926.5 30839.7 46543.1 +LP_Shaft 3651.8 80897.3 56247.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2638.05 0.9940 0.0550 4.43873 0.02087 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.689 0.9975 1.0000 0.9975 2706.36 0.899 1027.8 41728.9 +Core_Nozz 1.525 0.9999 1.0000 0.9999 862.88 0.813 1418.4 10501.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 75 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 2000.0 27.00 1482.60 27064.7 0.5230 14154.82 5.7751 455.07 16.753 2548.1 2485.7 1989.0 + core size:20.26 Q: 220.40 Maximum Thrust: 33830.9 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1482.60 15.257 555.77 132.85 0.0000 1478.32 13.664 538.54 6850.4 0.4000 1.39979 +FS_2 Inlet.Fl_O 1482.60 15.180 555.77 132.85 0.0000 1485.76 12.936 530.94 5943.4 0.4835 1.39979 +FS_21 Fan.Fl_O 1482.60 22.527 628.48 150.32 0.0000 1064.66 19.635 604.34 4515.2 0.4476 1.39846 +FS_13 Splitter.Fl_O2 1263.77 22.527 628.48 150.32 0.0000 907.52 19.537 603.48 3795.6 0.4558 1.39846 +FS_22 Splitter.Fl_O1 218.83 22.527 628.48 150.32 0.0000 157.14 20.110 608.47 719.5 0.4062 1.39846 +FS_23 Duct1.Fl_O 218.83 22.471 628.48 150.32 0.0000 157.54 20.059 608.47 721.3 0.4062 1.39846 +FS_24 LPC.Fl_O 218.83 47.722 802.62 192.45 0.0000 83.83 41.997 774.22 366.0 0.4322 1.39182 +FS_25 Duct2.Fl_O 218.83 47.603 802.62 192.45 0.0000 84.04 41.892 774.22 366.9 0.4322 1.39182 +FS_3 HPC.Fl_O 218.83 255.593 1344.93 328.57 0.0000 20.26 240.012 1322.73 119.9 0.3053 1.35916 +FS_36 Bld3.Fl_O 199.13 255.593 1344.93 328.57 0.0000 18.44 240.012 1322.73 109.1 0.3053 1.35916 +FS_4 Burner.Fl_O 203.07 241.536 2548.14 676.45 0.0197 27.39 239.981 2544.35 483.4 0.0997 1.29922 +FS_45 HPT.Fl_O 222.76 88.997 1988.95 511.98 0.0180 72.03 83.897 1960.94 439.1 0.3004 1.31586 +FS_48 Duct3.Fl_O 222.76 88.552 1988.95 511.98 0.0180 72.39 83.477 1960.94 441.4 0.3004 1.31586 +FS_5 LPT.Fl_O 222.76 19.883 1420.89 354.31 0.0180 272.51 18.416 1393.33 1477.4 0.3395 1.34225 +FS_7 Duct4.Fl_O 222.76 19.685 1420.89 354.31 0.0180 275.26 18.923 1406.65 2018.9 0.2430 1.34225 +FS_9 Core_Nozz.Fl_O 222.76 19.685 1420.89 354.31 0.0180 275.26 13.664 1293.58 862.9 0.7531 1.34225 +FS_15 BypBld.Fl_O 1263.77 22.527 628.48 150.32 0.0000 907.52 19.537 603.48 3795.6 0.4558 1.39846 +FS_17 Duct5.Fl_O 1263.77 22.359 628.48 150.32 0.0000 914.37 19.391 603.48 3824.3 0.4558 1.39846 +FS_19 Byp_Nozz.Fl_O 1263.77 22.359 628.48 150.32 0.0000 914.37 13.664 546.09 2706.4 0.8691 1.39846 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1485.76 1.484 0.9113 3399.202 1.1308 0.9161 -36649.9 36.92 18.48 +LPC 157.54 2.124 0.8588 3196.529 1.2771 0.8729 -13044.0 27.47 18.46 +HPC 84.04 5.369 0.8652 6288.938 1.6757 0.8916 -42144.7 24.00 24.11 +HPT 27.39 2.714 0.9148 154.980 1.2354 0.9048 42144.7 +LPT 72.39 4.454 0.9247 78.898 1.3998 0.9102 49693.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2848.75 1.337 0.9415 0.862 1.9915 0.5215 1.4369 0.9679 3943.9586 +LPC 168.98 1.344 0.8946 0.873 1.6805 0.9323 3.2631 0.9600 3662.6571 +HPC 199.79 21.198 0.8536 0.989 2.1225 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.034 0.9331 101.220 5.0341 1.4085 0.4249 0.9803 1.5311 +LPT 150.43 5.818 0.9235 97.272 5.8176 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6850.37 20969.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 996.42 240.10 78.074 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 996.42 240.10 78.074 +Duct1 0.0025 0.4062 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 996.42 240.10 78.074 +Duct2 0.0025 0.4322 365.99 +Duct3 0.0050 0.3004 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3395 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.6590 1344.93 328.57 255.593 +Duct5 0.0075 0.4558 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.0356 1344.93 328.57 255.593 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 628.48 150.32 22.527 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.7751 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7823.2 28293.7 42144.7 +LP_Shaft 3518.7 74175.0 49693.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2548.14 0.9940 0.0550 3.93190 0.01974 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.636 0.9975 1.0000 0.9975 2706.36 0.869 993.1 39009.3 +Core_Nozz 1.441 0.9999 1.0000 0.9999 862.88 0.753 1303.5 9025.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 76 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 2000.0 27.00 1352.44 20298.5 0.5275 10707.71 6.2082 455.07 13.782 2354.8 2298.2 1829.9 + core size:20.53 Q: 220.40 Maximum Thrust: 33830.9 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1352.44 15.257 555.77 132.85 0.0000 1348.53 13.664 538.54 6249.0 0.4000 1.39979 +FS_2 Inlet.Fl_O 1352.44 15.180 555.77 132.85 0.0000 1355.32 13.379 536.08 5943.4 0.4285 1.39979 +FS_21 Fan.Fl_O 1352.44 20.991 614.74 147.02 0.0000 1030.82 18.494 592.93 4515.2 0.4293 1.39878 +FS_13 Splitter.Fl_O2 1164.81 20.991 614.74 147.02 0.0000 887.81 18.347 591.59 3795.6 0.4429 1.39878 +FS_22 Splitter.Fl_O1 187.62 20.991 614.74 147.02 0.0000 143.01 19.171 599.04 719.5 0.3624 1.39878 +FS_23 Duct1.Fl_O 187.62 20.939 614.74 147.02 0.0000 143.37 19.123 599.04 721.3 0.3624 1.39878 +FS_24 LPC.Fl_O 187.62 40.721 764.62 183.22 0.0000 82.22 36.053 738.75 366.0 0.4214 1.39364 +FS_25 Duct2.Fl_O 187.62 40.619 764.62 183.22 0.0000 82.42 35.963 738.75 366.9 0.4214 1.39364 +FS_3 HPC.Fl_O 187.62 210.271 1271.34 309.57 0.0000 20.53 197.086 1249.54 119.9 0.3093 1.36367 +FS_36 Bld3.Fl_O 170.74 210.271 1271.34 309.57 0.0000 18.68 197.086 1249.54 109.1 0.3093 1.36367 +FS_4 Burner.Fl_O 173.71 198.706 2354.82 617.52 0.0174 27.37 197.428 2351.27 483.4 0.0995 1.30533 +FS_45 HPT.Fl_O 190.60 72.586 1829.95 465.86 0.0159 72.48 68.372 1803.35 439.1 0.3016 1.32351 +FS_48 Duct3.Fl_O 190.60 72.223 1829.95 465.86 0.0159 72.85 68.030 1803.35 441.4 0.3016 1.32351 +FS_5 LPT.Fl_O 190.60 17.908 1331.13 329.70 0.0159 250.58 16.807 1309.43 1477.4 0.3078 1.34901 +FS_7 Duct4.Fl_O 190.60 17.729 1331.13 329.70 0.0159 253.11 17.153 1319.80 2018.9 0.2216 1.34901 +FS_9 Core_Nozz.Fl_O 190.60 17.729 1331.13 329.70 0.0159 253.11 13.664 1243.90 862.9 0.6308 1.34901 +FS_15 BypBld.Fl_O 1164.81 20.991 614.74 147.02 0.0000 887.81 18.347 591.59 3795.6 0.4429 1.39878 +FS_17 Duct5.Fl_O 1164.81 20.834 614.74 147.02 0.0000 894.52 18.209 591.59 3824.3 0.4429 1.39878 +FS_19 Byp_Nozz.Fl_O 1164.81 20.834 614.74 147.02 0.0000 894.52 13.664 545.01 2706.4 0.8003 1.39878 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1355.32 1.383 0.9134 3097.706 1.1061 0.9173 -27109.0 41.92 18.68 +LPC 143.37 1.945 0.8526 2945.381 1.2438 0.8655 -9608.9 26.87 15.97 +HPC 82.42 5.177 0.8652 6256.062 1.6627 0.8911 -33542.0 26.81 26.96 +HPT 27.37 2.738 0.9151 156.531 1.2421 0.9051 33542.0 +LPT 72.85 4.033 0.9216 74.959 1.3747 0.9075 36717.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2598.64 1.266 0.9437 0.785 1.9584 0.5215 1.4369 0.9679 3943.9586 +LPC 153.78 1.290 0.8881 0.804 1.6427 0.9323 3.2631 0.9600 3662.6571 +HPC 195.95 20.308 0.8536 0.984 2.1524 0.4206 0.2163 1.0137 6357.1603 +HPT 30.12 5.089 0.9334 102.233 5.0895 1.4085 0.4249 0.9803 1.5311 +LPT 151.37 5.231 0.9204 92.415 5.2310 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6248.96 19128.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 945.34 227.44 65.473 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 945.34 227.44 65.473 +Duct1 0.0025 0.3624 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 945.34 227.44 65.473 +Duct2 0.0025 0.4214 365.99 +Duct3 0.0050 0.3016 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3078 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.5669 1271.34 309.57 210.271 +Duct5 0.0075 0.4429 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.3194 1271.34 309.57 210.271 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 614.74 147.02 20.991 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.2082 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7595.9 23192.3 33542.0 +LP_Shaft 3206.6 60140.0 36717.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2354.82 0.9940 0.0550 2.97436 0.01742 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.525 0.9975 1.0000 0.9975 2706.36 0.800 913.6 33073.8 +Core_Nozz 1.297 0.9999 1.0000 0.9999 862.88 0.631 1072.5 6353.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 77 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 2000.0 27.00 1195.39 13532.3 0.5534 7489.29 6.7436 455.07 10.756 2127.1 2077.4 1643.8 + core size:20.88 Q: 220.40 Maximum Thrust: 33830.9 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1195.39 15.257 555.77 132.85 0.0000 1191.94 13.664 538.54 5523.3 0.4000 1.39979 +FS_2 Inlet.Fl_O 1195.39 15.180 555.77 132.85 0.0000 1197.94 13.822 541.09 5943.4 0.3684 1.39979 +FS_21 Fan.Fl_O 1195.39 19.346 599.40 143.33 0.0000 976.16 17.318 580.75 4515.2 0.4011 1.39905 +FS_13 Splitter.Fl_O2 1041.02 19.346 599.40 143.33 0.0000 850.10 17.145 579.10 3795.6 0.4190 1.39905 +FS_22 Splitter.Fl_O1 154.37 19.346 599.40 143.33 0.0000 126.06 18.074 587.88 719.5 0.3133 1.39905 +FS_23 Duct1.Fl_O 154.37 19.298 599.40 143.33 0.0000 126.38 18.029 587.88 721.3 0.3133 1.39905 +FS_24 LPC.Fl_O 154.37 33.389 719.08 172.18 0.0000 80.00 29.797 696.24 366.0 0.4071 1.39538 +FS_25 Duct2.Fl_O 154.37 33.306 719.08 172.18 0.0000 80.20 29.722 696.24 366.9 0.4071 1.39538 +FS_3 HPC.Fl_O 154.37 164.094 1182.53 286.87 0.0000 20.88 153.430 1161.26 119.9 0.3145 1.36924 +FS_36 Bld3.Fl_O 140.48 164.094 1182.53 286.87 0.0000 19.00 153.430 1161.26 109.1 0.3145 1.36924 +FS_4 Burner.Fl_O 142.56 155.069 2127.12 549.66 0.0148 27.36 154.072 2123.85 483.4 0.0991 1.31341 +FS_45 HPT.Fl_O 156.45 56.108 1643.79 413.16 0.0135 72.95 52.807 1619.01 439.1 0.3025 1.33356 +FS_48 Duct3.Fl_O 156.45 55.828 1643.79 413.16 0.0135 73.32 52.543 1619.01 441.4 0.3025 1.33356 +FS_5 LPT.Fl_O 156.45 16.348 1238.30 304.64 0.0135 217.30 15.607 1223.27 1477.4 0.2623 1.35639 +FS_7 Duct4.Fl_O 156.45 16.185 1238.30 304.64 0.0135 219.50 15.794 1230.35 2018.9 0.1902 1.35639 +FS_9 Core_Nozz.Fl_O 156.45 16.185 1238.30 304.64 0.0135 219.50 13.664 1184.31 862.9 0.5042 1.35639 +FS_15 BypBld.Fl_O 1041.02 19.346 599.40 143.33 0.0000 850.10 17.145 579.10 3795.6 0.4190 1.39905 +FS_17 Duct5.Fl_O 1041.02 19.201 599.40 143.33 0.0000 856.53 17.017 579.10 3824.3 0.4190 1.39905 +FS_19 Byp_Nozz.Fl_O 1041.02 19.201 599.40 143.33 0.0000 856.53 13.664 543.91 2706.4 0.7145 1.39905 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1197.94 1.274 0.9133 2720.812 1.0785 0.9163 -17721.5 44.91 18.39 +LPC 126.38 1.730 0.8452 2619.930 1.1997 0.8567 -6301.2 28.41 13.63 +HPC 80.20 4.927 0.8643 6216.889 1.6445 0.8899 -25049.2 30.62 30.83 +HPT 27.36 2.764 0.9155 158.715 1.2507 0.9051 25049.3 +LPT 73.32 3.415 0.9132 69.467 1.3275 0.8993 24022.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2296.89 1.191 0.9436 0.690 1.9686 0.5215 1.4369 0.9679 3943.9586 +LPC 135.56 1.224 0.8804 0.715 1.6361 0.9323 3.2631 0.9600 3662.6571 +HPC 190.67 19.153 0.8527 0.978 2.1813 0.4206 0.2163 1.0137 6357.1603 +HPT 30.10 5.151 0.9339 103.660 5.1512 1.4085 0.4249 0.9803 1.5311 +LPT 152.35 4.369 0.9121 85.644 4.3686 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5523.33 16907.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 883.91 212.32 52.466 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 883.91 212.32 52.466 +Duct1 0.0025 0.3133 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 883.91 212.32 52.466 +Duct2 0.0025 0.4071 365.99 +Duct3 0.0050 0.3025 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2623 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.4030 1182.53 286.87 164.094 +Duct5 0.0075 0.4190 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.4904 1182.53 286.87 164.094 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 599.40 143.33 19.346 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.7436 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7320.1 17972.7 25049.3 +LP_Shaft 2816.4 44796.7 24022.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2127.12 0.9940 0.0550 2.08036 0.01481 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.405 0.9975 1.0000 0.9975 2706.36 0.714 814.8 26364.1 +Core_Nozz 1.184 0.9999 1.0000 0.9999 862.88 0.504 838.2 4075.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 78 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 2000.0 27.00 994.20 6766.2 0.6480 4384.71 7.5080 455.07 7.512 1819.4 1779.1 1395.1 + core size:21.44 Q: 220.40 Maximum Thrust: 33830.9 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 994.20 15.257 555.77 132.85 0.0000 991.32 13.664 538.54 4593.7 0.4000 1.39979 +FS_2 Inlet.Fl_O 994.20 15.180 555.77 132.85 0.0000 996.31 14.273 546.07 5943.4 0.2981 1.39979 +FS_21 Fan.Fl_O 994.20 17.580 581.95 139.14 0.0000 880.35 16.119 567.72 4515.2 0.3543 1.39933 +FS_13 Splitter.Fl_O2 877.34 17.580 581.95 139.14 0.0000 776.87 15.952 566.03 3795.6 0.3752 1.39933 +FS_22 Splitter.Fl_O1 116.85 17.580 581.95 139.14 0.0000 103.47 16.821 574.67 719.5 0.2519 1.39933 +FS_23 Duct1.Fl_O 116.85 17.536 581.95 139.14 0.0000 103.73 16.779 574.67 721.3 0.2519 1.39933 +FS_24 LPC.Fl_O 116.85 25.438 659.98 157.91 0.0000 76.15 22.993 641.27 366.0 0.3830 1.39745 +FS_25 Duct2.Fl_O 116.85 25.374 659.98 157.91 0.0000 76.34 22.935 641.27 366.9 0.3830 1.39745 +FS_3 HPC.Fl_O 116.85 114.612 1062.05 256.47 0.0000 21.44 106.722 1041.50 119.9 0.3233 1.37683 +FS_36 Bld3.Fl_O 106.34 114.612 1062.05 256.47 0.0000 19.51 106.722 1041.50 109.1 0.3233 1.37683 +FS_4 Burner.Fl_O 107.55 108.308 1819.42 460.74 0.0115 27.33 107.614 1816.54 483.4 0.0985 1.32697 +FS_45 HPT.Fl_O 118.07 38.779 1395.13 345.00 0.0104 73.39 36.470 1373.13 439.1 0.3027 1.34881 +FS_48 Duct3.Fl_O 118.07 38.585 1395.13 345.00 0.0104 73.75 36.288 1373.13 441.4 0.3027 1.34881 +FS_5 LPT.Fl_O 118.07 15.099 1120.58 273.50 0.0104 168.92 14.694 1112.44 1477.4 0.1998 1.36594 +FS_7 Duct4.Fl_O 118.07 14.948 1120.58 273.50 0.0104 170.63 14.732 1116.22 2018.9 0.1461 1.36594 +FS_9 Core_Nozz.Fl_O 118.07 14.948 1120.58 273.50 0.0104 170.63 13.664 1093.88 862.9 0.3647 1.36594 +FS_15 BypBld.Fl_O 877.34 17.580 581.95 139.14 0.0000 776.87 15.952 566.03 3795.6 0.3752 1.39933 +FS_17 Duct5.Fl_O 877.34 17.448 581.95 139.14 0.0000 782.74 15.832 566.03 3824.3 0.3752 1.39933 +FS_19 Byp_Nozz.Fl_O 877.34 17.448 581.95 139.14 0.0000 782.74 13.664 542.70 2706.4 0.6015 1.39933 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 996.31 1.158 0.9087 2176.304 1.0471 0.9107 -8842.1 53.96 16.53 +LPC 103.73 1.451 0.8340 2126.791 1.1341 0.8426 -3103.2 35.68 11.73 +HPC 76.34 4.517 0.8625 6146.223 1.6092 0.8877 -16295.4 37.35 37.83 +HPT 27.33 2.793 0.9164 162.540 1.2637 0.9056 16295.5 +LPT 73.75 2.556 0.8991 60.314 1.2450 0.8872 11945.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1910.30 1.110 0.9388 0.552 2.0676 0.5215 1.4369 0.9679 3943.9586 +LPC 111.27 1.138 0.8688 0.581 1.7159 0.9323 3.2631 0.9600 3662.6571 +HPC 181.49 17.257 0.8509 0.967 2.2412 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.220 0.9348 106.158 5.2199 1.4085 0.4249 0.9803 1.5311 +LPT 153.25 3.170 0.8979 74.359 3.1699 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4593.69 14061.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 802.42 192.40 38.448 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 802.42 192.40 38.448 +Duct1 0.0025 0.2519 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 802.42 192.40 38.448 +Duct2 0.0025 0.3830 365.99 +Duct3 0.0050 0.3027 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1998 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.0899 1062.05 256.47 114.612 +Duct5 0.0075 0.3752 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.4270 1062.05 256.47 114.612 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 581.95 139.14 17.580 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.5080 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6933.1 12344.5 16295.5 +LP_Shaft 2252.8 27849.0 11945.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1819.42 0.9940 0.0550 1.21797 0.01145 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.277 0.9975 1.0000 0.9975 2706.36 0.601 685.2 18683.8 +Core_Nozz 1.094 0.9999 1.0000 0.9999 862.88 0.365 584.3 2144.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 79 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 2000.0 27.00 1662.16 31771.5 0.5767 18322.50 5.5125 568.83 19.073 2730.0 2662.3 2138.9 + core size:20.07 Q: 344.38 Maximum Thrust: 31771.5 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1662.16 16.208 565.46 135.18 0.0000 1573.59 13.664 538.54 6144.0 0.5000 1.39961 +FS_2 Inlet.Fl_O 1662.16 16.127 565.46 135.18 0.0000 1581.51 13.336 535.58 5943.4 0.5281 1.39961 +FS_21 Fan.Fl_O 1662.16 25.138 649.95 155.49 0.0000 1087.77 21.740 623.62 4515.2 0.4604 1.39782 +FS_13 Splitter.Fl_O2 1406.93 25.138 649.95 155.49 0.0000 920.74 21.683 623.15 3795.6 0.4647 1.39782 +FS_22 Splitter.Fl_O1 255.23 25.138 649.95 155.49 0.0000 167.03 22.028 625.96 719.5 0.4387 1.39782 +FS_23 Duct1.Fl_O 255.23 25.075 649.95 155.49 0.0000 167.45 21.973 625.96 721.3 0.4387 1.39782 +FS_24 LPC.Fl_O 255.23 56.436 844.15 202.59 0.0000 84.79 49.480 813.53 366.0 0.4389 1.38986 +FS_25 Duct2.Fl_O 255.23 56.295 844.15 202.59 0.0000 85.00 49.356 813.53 366.9 0.4389 1.38986 +FS_3 HPC.Fl_O 255.23 309.146 1419.53 348.01 0.0000 20.07 290.673 1396.78 119.9 0.3027 1.35477 +FS_36 Bld3.Fl_O 232.26 309.146 1419.53 348.01 0.0000 18.27 290.673 1396.78 109.1 0.3027 1.35477 +FS_4 Burner.Fl_O 237.35 292.143 2730.00 732.87 0.0219 27.39 290.261 2725.99 483.4 0.1000 1.29401 +FS_45 HPT.Fl_O 260.32 108.320 2138.95 556.32 0.0199 71.72 102.169 2109.56 439.1 0.2997 1.30955 +FS_48 Duct3.Fl_O 260.32 107.779 2138.95 556.32 0.0199 72.08 101.658 2109.56 441.4 0.2997 1.30955 +FS_5 LPT.Fl_O 260.32 22.865 1514.93 380.44 0.0199 285.94 20.987 1482.58 1477.4 0.3599 1.33576 +FS_7 Duct4.Fl_O 260.32 22.636 1514.93 380.44 0.0199 288.83 21.667 1498.34 2018.9 0.2565 1.33576 +FS_9 Core_Nozz.Fl_O 260.32 22.636 1514.93 380.44 0.0199 288.83 13.664 1332.53 862.9 0.8944 1.33576 +FS_15 BypBld.Fl_O 1406.93 25.138 649.95 155.49 0.0000 920.74 21.683 623.15 3795.6 0.4647 1.39782 +FS_17 Duct5.Fl_O 1406.93 24.949 649.95 155.49 0.0000 927.70 21.520 623.15 3824.3 0.4647 1.39782 +FS_19 Byp_Nozz.Fl_O 1406.93 24.949 649.95 155.49 0.0000 927.70 13.664 547.39 2706.4 0.9687 1.39782 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1581.51 1.559 0.9030 3605.145 1.1494 0.9089 -47771.2 31.87 18.32 +LPC 167.45 2.251 0.8631 3362.672 1.2988 0.8776 -17006.2 28.09 20.46 +HPC 85.00 5.492 0.8649 6311.038 1.6816 0.8914 -52515.2 22.23 22.32 +HPT 27.39 2.697 0.9146 154.094 1.2300 0.9052 52515.4 +LPT 72.08 4.714 0.9276 81.392 1.4119 0.9132 64778.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3032.33 1.389 0.9329 0.914 2.0889 0.5215 1.4369 0.9679 3943.9586 +LPC 179.61 1.383 0.8990 0.918 1.7162 0.9323 3.2631 0.9600 3662.6571 +HPC 202.07 21.764 0.8532 0.993 2.0976 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 4.994 0.9329 100.641 4.9941 1.4085 0.4249 0.9803 1.5311 +LPT 149.78 6.181 0.9264 100.346 6.1805 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6144.02 29386.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1050.13 253.49 93.337 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1050.13 253.49 93.337 +Duct1 0.0025 0.4387 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1050.13 253.49 93.337 +Duct2 0.0025 0.4389 365.99 +Duct3 0.0050 0.2997 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3599 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.9329 1419.53 348.01 309.146 +Duct5 0.0075 0.4647 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 14.0374 1419.53 348.01 309.146 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 649.95 155.49 25.138 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5125 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 8051.3 34257.4 52515.4 +LP_Shaft 3764.3 90382.1 64778.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.00 0.9940 0.0550 5.08958 0.02191 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.826 0.9975 1.0000 0.9975 2706.36 0.969 1108.3 48462.9 +Core_Nozz 1.657 0.9999 1.0000 0.9999 862.88 0.894 1569.1 12695.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 80 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 2000.0 27.00 1612.86 28594.4 0.5739 16410.55 5.6860 568.83 17.718 2642.0 2577.1 2066.5 + core size:20.20 Q: 344.38 Maximum Thrust: 31771.5 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1612.86 16.208 565.46 135.18 0.0000 1526.92 13.664 538.54 5961.8 0.5000 1.39961 +FS_2 Inlet.Fl_O 1612.86 16.127 565.46 135.18 0.0000 1534.61 13.542 537.94 5943.4 0.5058 1.39961 +FS_21 Fan.Fl_O 1612.86 24.437 643.81 154.01 0.0000 1080.65 21.185 618.15 4515.2 0.4564 1.39802 +FS_13 Splitter.Fl_O2 1371.63 24.437 643.81 154.01 0.0000 919.02 21.093 617.38 3795.6 0.4635 1.39802 +FS_22 Splitter.Fl_O1 241.23 24.437 643.81 154.01 0.0000 161.63 21.637 621.88 719.5 0.4207 1.39802 +FS_23 Duct1.Fl_O 241.23 24.376 643.81 154.01 0.0000 162.03 21.583 621.88 721.3 0.4207 1.39802 +FS_24 LPC.Fl_O 241.23 53.447 830.02 199.13 0.0000 83.91 47.020 800.65 366.0 0.4329 1.39052 +FS_25 Duct2.Fl_O 241.23 53.313 830.02 199.13 0.0000 84.12 46.902 800.65 366.9 0.4329 1.39052 +FS_3 HPC.Fl_O 241.23 287.176 1389.21 340.09 0.0000 20.20 269.775 1366.54 119.9 0.3047 1.35653 +FS_36 Bld3.Fl_O 219.52 287.176 1389.21 340.09 0.0000 18.38 269.775 1366.54 109.1 0.3047 1.35653 +FS_4 Burner.Fl_O 224.08 271.381 2641.97 705.36 0.0208 27.39 269.634 2638.07 483.4 0.0999 1.29648 +FS_45 HPT.Fl_O 245.79 100.329 2066.50 534.75 0.0189 71.86 94.608 2037.77 439.1 0.3000 1.31256 +FS_48 Duct3.Fl_O 245.79 99.827 2066.50 534.75 0.0189 72.22 94.135 2037.77 441.4 0.3000 1.31256 +FS_5 LPT.Fl_O 245.79 21.542 1466.32 366.87 0.0189 281.93 19.828 1435.79 1477.4 0.3536 1.33907 +FS_7 Duct4.Fl_O 245.79 21.327 1466.32 366.87 0.0189 284.78 20.441 1450.63 2018.9 0.2523 1.33907 +FS_9 Core_Nozz.Fl_O 245.79 21.327 1466.32 366.87 0.0189 284.78 13.664 1308.55 862.9 0.8362 1.33907 +FS_15 BypBld.Fl_O 1371.63 24.437 643.81 154.01 0.0000 919.02 21.093 617.38 3795.6 0.4635 1.39802 +FS_17 Duct5.Fl_O 1371.63 24.253 643.81 154.01 0.0000 925.97 20.935 617.38 3824.3 0.4635 1.39802 +FS_19 Byp_Nozz.Fl_O 1371.63 24.253 643.81 154.01 0.0000 925.97 13.664 546.60 2706.4 0.9437 1.39802 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1534.61 1.515 0.9081 3499.405 1.1386 0.9134 -42980.8 35.15 18.83 +LPC 162.03 2.193 0.8603 3279.568 1.2892 0.8747 -15399.8 27.29 19.03 +HPC 84.12 5.387 0.8654 6290.777 1.6737 0.8917 -48109.5 23.66 23.77 +HPT 27.39 2.705 0.9147 154.824 1.2326 0.9051 48109.5 +LPT 72.22 4.634 0.9261 80.377 1.4093 0.9115 58380.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2942.40 1.359 0.9382 0.887 2.0457 0.5215 1.4369 0.9679 3943.9586 +LPC 173.80 1.365 0.8961 0.895 1.6858 0.9323 3.2631 0.9600 3662.6571 +HPC 199.98 21.278 0.8537 0.990 2.1145 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.013 0.9331 101.118 5.0127 1.4085 0.4249 0.9803 1.5311 +LPT 150.08 6.069 0.9249 99.095 6.0694 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5961.79 28515.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1030.05 248.47 87.574 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1030.05 248.47 87.574 +Duct1 0.0025 0.4207 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1030.05 248.47 87.574 +Duct2 0.0025 0.4329 365.99 +Duct3 0.0050 0.3000 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3536 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.4430 1389.21 340.09 287.176 +Duct5 0.0075 0.4635 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 13.2676 1389.21 340.09 287.176 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 643.81 154.01 24.437 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.6860 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7958.0 31751.4 48109.5 +LP_Shaft 3653.9 83917.2 58380.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2641.97 0.9940 0.0550 4.55849 0.02077 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.775 0.9975 1.0000 0.9975 2706.36 0.944 1078.9 45995.1 +Core_Nozz 1.561 0.9999 1.0000 0.9999 862.88 0.836 1454.9 11114.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 81 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 2000.0 27.00 1559.15 25417.2 0.5743 14597.54 5.8821 568.83 16.348 2554.6 2492.4 1994.8 + core size:20.33 Q: 344.38 Maximum Thrust: 31771.5 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1559.15 16.208 565.46 135.18 0.0000 1476.07 13.664 538.54 5763.3 0.5000 1.39961 +FS_2 Inlet.Fl_O 1559.15 16.127 565.46 135.18 0.0000 1483.50 13.751 540.30 5943.4 0.4826 1.39961 +FS_21 Fan.Fl_O 1559.15 23.705 637.55 152.50 0.0000 1071.66 20.613 612.66 4515.2 0.4514 1.39821 +FS_13 Splitter.Fl_O2 1332.60 23.705 637.55 152.50 0.0000 915.94 20.488 611.59 3795.6 0.4614 1.39821 +FS_22 Splitter.Fl_O1 226.55 23.705 637.55 152.50 0.0000 155.72 21.213 617.69 719.5 0.4016 1.39821 +FS_23 Duct1.Fl_O 226.55 23.646 637.55 152.50 0.0000 156.11 21.160 617.69 721.3 0.4016 1.39821 +FS_24 LPC.Fl_O 226.55 50.230 814.48 195.34 0.0000 83.06 44.332 786.33 366.0 0.4273 1.39125 +FS_25 Duct2.Fl_O 226.55 50.104 814.48 195.34 0.0000 83.27 44.221 786.33 366.9 0.4273 1.39125 +FS_3 HPC.Fl_O 226.55 264.964 1357.40 331.81 0.0000 20.33 248.696 1334.87 119.9 0.3065 1.35841 +FS_36 Bld3.Fl_O 206.16 264.964 1357.40 331.81 0.0000 18.50 248.696 1334.87 109.1 0.3065 1.35841 +FS_4 Burner.Fl_O 210.22 250.391 2554.58 678.31 0.0197 27.38 248.779 2550.79 483.4 0.0997 1.29913 +FS_45 HPT.Fl_O 230.61 92.286 1994.78 513.60 0.0179 72.02 87.000 1966.71 439.1 0.3004 1.31570 +FS_48 Duct3.Fl_O 230.61 91.824 1994.78 513.60 0.0179 72.38 86.565 1966.71 441.4 0.3004 1.31570 +FS_5 LPT.Fl_O 230.61 20.341 1421.20 354.37 0.0179 275.79 18.800 1392.87 1477.4 0.3442 1.34228 +FS_7 Duct4.Fl_O 230.61 20.138 1421.20 354.37 0.0179 278.57 19.339 1406.60 2018.9 0.2461 1.34228 +FS_9 Core_Nozz.Fl_O 230.61 20.138 1421.20 354.37 0.0179 278.57 13.664 1286.24 862.9 0.7772 1.34228 +FS_15 BypBld.Fl_O 1332.60 23.705 637.55 152.50 0.0000 915.94 20.488 611.59 3795.6 0.4614 1.39821 +FS_17 Duct5.Fl_O 1332.60 23.527 637.55 152.50 0.0000 922.86 20.334 611.59 3824.3 0.4614 1.39821 +FS_19 Byp_Nozz.Fl_O 1332.60 23.527 637.55 152.50 0.0000 922.86 13.664 545.98 2706.4 0.9164 1.39821 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1483.50 1.470 0.9109 3381.050 1.1275 0.9157 -38222.5 38.46 19.25 +LPC 156.11 2.124 0.8571 3184.178 1.2775 0.8713 -13730.7 26.57 17.69 +HPC 83.27 5.288 0.8656 6272.832 1.6666 0.8917 -43743.3 25.02 25.15 +HPT 27.38 2.713 0.9148 155.524 1.2353 0.9049 43743.3 +LPT 72.38 4.514 0.9242 79.043 1.4036 0.9095 51953.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2844.41 1.327 0.9411 0.857 2.0225 0.5215 1.4369 0.9679 3943.9586 +LPC 167.44 1.345 0.8928 0.869 1.6571 0.9323 3.2631 0.9600 3662.6571 +HPC 197.96 20.824 0.8539 0.987 2.1282 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.032 0.9332 101.575 5.0322 1.4085 0.4249 0.9803 1.5311 +LPT 150.40 5.902 0.9230 97.450 5.9022 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5763.25 27565.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1008.53 243.11 81.581 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1008.53 243.11 81.581 +Duct1 0.0025 0.4016 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1008.53 243.11 81.581 +Duct2 0.0025 0.4273 365.99 +Duct3 0.0050 0.3004 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3442 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.9293 1357.40 331.81 264.964 +Duct5 0.0075 0.4614 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.4603 1357.40 331.81 264.964 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 637.55 152.50 23.705 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.8821 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7860.6 29227.3 43743.3 +LP_Shaft 3530.3 77292.8 51953.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2554.58 0.9940 0.0550 4.05487 0.01967 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.722 0.9975 1.0000 0.9975 2706.36 0.916 1047.0 43365.8 +Core_Nozz 1.474 0.9999 1.0000 0.9999 862.88 0.777 1341.8 9617.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 82 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 2000.0 27.00 1437.82 19062.9 0.5848 11147.35 6.3509 568.83 13.560 2366.6 2310.1 1840.4 + core size:20.60 Q: 344.38 Maximum Thrust: 31771.5 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1437.82 16.208 565.46 135.18 0.0000 1361.21 13.664 538.54 5314.8 0.5000 1.39961 +FS_2 Inlet.Fl_O 1437.82 16.127 565.46 135.18 0.0000 1368.06 14.171 544.97 5943.4 0.4337 1.39961 +FS_21 Fan.Fl_O 1437.82 22.159 624.23 149.30 0.0000 1046.14 19.429 601.28 4515.2 0.4375 1.39857 +FS_13 Splitter.Fl_O2 1242.22 22.159 624.23 149.30 0.0000 903.82 19.246 599.65 3795.6 0.4533 1.39857 +FS_22 Splitter.Fl_O1 195.60 22.159 624.23 149.30 0.0000 142.31 20.258 608.47 719.5 0.3604 1.39857 +FS_23 Duct1.Fl_O 195.60 22.103 624.23 149.30 0.0000 142.67 20.207 608.47 721.3 0.3604 1.39857 +FS_24 LPC.Fl_O 195.60 43.290 778.44 186.57 0.0000 81.35 38.449 752.79 366.0 0.4159 1.39299 +FS_25 Duct2.Fl_O 195.60 43.182 778.44 186.57 0.0000 81.55 38.353 752.79 366.9 0.4159 1.39299 +FS_3 HPC.Fl_O 195.60 219.786 1286.59 313.49 0.0000 20.60 205.904 1264.40 119.9 0.3106 1.36272 +FS_36 Bld3.Fl_O 178.00 219.786 1286.59 313.49 0.0000 18.74 205.904 1264.40 109.1 0.3106 1.36272 +FS_4 Burner.Fl_O 181.09 207.698 2366.61 620.96 0.0174 27.37 206.362 2363.04 483.4 0.0995 1.30504 +FS_45 HPT.Fl_O 198.70 75.943 1840.38 468.77 0.0158 72.43 71.541 1813.71 439.1 0.3014 1.32309 +FS_48 Duct3.Fl_O 198.70 75.563 1840.38 468.77 0.0158 72.79 71.183 1813.71 441.4 0.3014 1.32309 +FS_5 LPT.Fl_O 198.70 18.279 1331.85 329.89 0.0158 255.99 17.102 1309.09 1477.4 0.3153 1.34898 +FS_7 Duct4.Fl_O 198.70 18.096 1331.85 329.89 0.0158 258.58 17.482 1320.00 2018.9 0.2267 1.34898 +FS_9 Core_Nozz.Fl_O 198.70 18.096 1331.85 329.89 0.0158 258.58 13.664 1237.93 862.9 0.6559 1.34898 +FS_15 BypBld.Fl_O 1242.22 22.159 624.23 149.30 0.0000 903.82 19.246 599.65 3795.6 0.4533 1.39857 +FS_17 Duct5.Fl_O 1242.22 21.992 624.23 149.30 0.0000 910.65 19.102 599.65 3824.3 0.4533 1.39857 +FS_19 Byp_Nozz.Fl_O 1242.22 21.992 624.23 149.30 0.0000 910.65 13.664 544.95 2706.4 0.8534 1.39857 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1368.06 1.374 0.9129 3099.985 1.1039 0.9168 -28731.3 43.87 19.87 +LPC 142.67 1.959 0.8506 2950.447 1.2470 0.8639 -10313.9 25.71 15.24 +HPC 81.55 5.090 0.8653 6240.097 1.6528 0.8910 -35125.1 27.93 28.10 +HPT 27.37 2.735 0.9152 157.143 1.2416 0.9053 35125.2 +LPT 72.79 4.134 0.9210 75.451 1.3818 0.9066 39045.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2623.07 1.260 0.9432 0.786 2.0109 0.5215 1.4369 0.9679 3943.9586 +LPC 153.03 1.294 0.8860 0.806 1.6155 0.9323 3.2631 0.9600 3662.6571 +HPC 193.88 19.906 0.8536 0.982 2.1554 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.083 0.9335 102.633 5.0834 1.4085 0.4249 0.9803 1.5311 +LPT 151.26 5.372 0.9198 93.021 5.3718 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5314.79 25420.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 959.71 230.99 69.055 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 959.71 230.99 69.055 +Duct1 0.0025 0.3604 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 959.71 230.99 69.055 +Duct2 0.0025 0.4159 365.99 +Duct3 0.0050 0.3014 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3153 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.8460 1286.59 313.49 219.786 +Duct5 0.0075 0.4533 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.7580 1286.59 313.49 219.786 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 624.23 149.30 22.159 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.3509 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7644.6 24132.1 35125.2 +LP_Shaft 3236.8 63355.3 39045.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2366.61 0.9940 0.0550 3.09649 0.01740 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.609 0.9975 1.0000 0.9975 2706.36 0.853 974.2 37611.9 +Core_Nozz 1.324 0.9999 1.0000 0.9999 862.88 0.656 1112.7 6871.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 83 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 2000.0 27.00 1292.48 12708.6 0.6207 7888.82 6.9561 568.83 10.699 2144.3 2094.6 1658.6 + core size:20.95 Q: 344.38 Maximum Thrust: 31771.5 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1292.48 16.208 565.46 135.18 0.0000 1223.61 13.664 538.54 4777.5 0.5000 1.39961 +FS_2 Inlet.Fl_O 1292.48 16.127 565.46 135.18 0.0000 1229.77 14.596 549.59 5943.4 0.3801 1.39961 +FS_21 Fan.Fl_O 1292.48 20.489 609.33 145.72 0.0000 1004.81 18.192 589.02 4515.2 0.4157 1.39889 +FS_13 Splitter.Fl_O2 1130.03 20.489 609.33 145.72 0.0000 878.51 17.972 586.97 3795.6 0.4369 1.39889 +FS_22 Splitter.Fl_O1 162.45 20.489 609.33 145.72 0.0000 126.29 19.136 597.58 719.5 0.3140 1.39889 +FS_23 Duct1.Fl_O 162.45 20.438 609.33 145.72 0.0000 126.61 19.088 597.58 721.3 0.3140 1.39889 +FS_24 LPC.Fl_O 162.45 35.946 735.17 176.07 0.0000 79.07 32.181 712.48 366.0 0.4013 1.39483 +FS_25 Duct2.Fl_O 162.45 35.856 735.17 176.07 0.0000 79.27 32.100 712.48 366.9 0.4013 1.39483 +FS_3 HPC.Fl_O 162.45 173.416 1201.26 291.64 0.0000 20.95 162.057 1179.54 119.9 0.3160 1.36806 +FS_36 Bld3.Fl_O 147.83 173.416 1201.26 291.64 0.0000 19.07 162.057 1179.54 109.1 0.3160 1.36806 +FS_4 Burner.Fl_O 150.02 163.878 2144.30 554.61 0.0148 27.35 162.826 2141.01 483.4 0.0991 1.31288 +FS_45 HPT.Fl_O 164.64 59.369 1658.61 417.23 0.0135 72.88 55.883 1633.70 439.1 0.3023 1.33284 +FS_48 Duct3.Fl_O 164.64 59.072 1658.61 417.23 0.0135 73.25 55.604 1633.70 441.4 0.3023 1.33284 +FS_5 LPT.Fl_O 164.64 16.627 1237.92 304.55 0.0135 224.82 15.817 1221.76 1477.4 0.2722 1.35640 +FS_7 Duct4.Fl_O 164.64 16.461 1237.92 304.55 0.0135 227.09 16.034 1229.40 2018.9 0.1971 1.35640 +FS_9 Core_Nozz.Fl_O 164.64 16.461 1237.92 304.55 0.0135 227.09 13.664 1178.68 862.9 0.5293 1.35640 +FS_15 BypBld.Fl_O 1130.03 20.489 609.33 145.72 0.0000 878.51 17.972 586.97 3795.6 0.4369 1.39889 +FS_17 Duct5.Fl_O 1130.03 20.335 609.33 145.72 0.0000 885.15 17.837 586.97 3824.3 0.4369 1.39889 +FS_19 Byp_Nozz.Fl_O 1130.03 20.335 609.33 145.72 0.0000 885.15 13.664 543.95 2706.4 0.7756 1.39889 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1229.77 1.270 0.9115 2750.369 1.0776 0.9144 -19273.0 47.99 20.22 +LPC 126.61 1.759 0.8430 2649.516 1.2065 0.8549 -6977.4 26.58 12.93 +HPC 79.27 4.836 0.8641 6201.974 1.6340 0.8894 -26561.4 31.88 32.11 +HPT 27.35 2.760 0.9156 159.454 1.2500 0.9053 26561.4 +LPT 73.25 3.553 0.9147 70.514 1.3398 0.9005 26249.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2357.91 1.188 0.9416 0.697 2.0501 0.5215 1.4369 0.9679 3943.9586 +LPC 135.81 1.233 0.8781 0.723 1.5994 0.9323 3.2631 0.9600 3662.6571 +HPC 188.46 18.735 0.8524 0.976 2.1829 0.4206 0.2163 1.0137 6357.1603 +HPT 30.10 5.143 0.9340 104.142 5.1432 1.4085 0.4249 0.9803 1.5311 +LPT 152.20 4.561 0.9135 86.935 4.5611 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4777.53 22850.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 901.01 216.52 56.008 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 901.01 216.52 56.008 +Duct1 0.0025 0.3140 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 901.01 216.52 56.008 +Duct2 0.0025 0.4013 365.99 +Duct3 0.0050 0.3023 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2722 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.6858 1201.26 291.64 173.416 +Duct5 0.0075 0.4369 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.9348 1201.26 291.64 173.416 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 609.33 145.72 20.489 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.9561 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7383.8 18893.3 26561.4 +LP_Shaft 2871.8 48008.0 26249.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2144.30 0.9940 0.0550 2.19134 0.01482 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.488 0.9975 1.0000 0.9975 2706.36 0.776 884.5 31067.1 +Core_Nozz 1.205 0.9999 1.0000 0.9999 862.88 0.529 877.9 4492.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 84 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 2000.0 27.00 1108.88 6354.3 0.7454 4736.41 7.8732 568.83 7.623 1847.8 1807.2 1418.6 + core size:21.51 Q: 344.38 Maximum Thrust: 31771.5 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1108.88 16.208 565.46 135.18 0.0000 1049.79 13.664 538.54 4098.9 0.5000 1.39961 +FS_2 Inlet.Fl_O 1108.88 16.127 565.46 135.18 0.0000 1055.08 15.036 554.26 5943.4 0.3180 1.39961 +FS_21 Fan.Fl_O 1108.88 18.676 592.39 141.65 0.0000 932.53 16.911 575.84 4515.2 0.3794 1.39916 +FS_13 Splitter.Fl_O2 983.91 18.676 592.39 141.65 0.0000 827.43 16.680 573.59 3795.6 0.4051 1.39916 +FS_22 Splitter.Fl_O1 124.97 18.676 592.39 141.65 0.0000 105.10 17.843 584.73 719.5 0.2562 1.39916 +FS_23 Duct1.Fl_O 124.97 18.629 592.39 141.65 0.0000 105.36 17.798 584.73 721.3 0.2562 1.39916 +FS_24 LPC.Fl_O 124.97 27.828 678.43 162.36 0.0000 75.48 25.206 659.61 366.0 0.3790 1.39677 +FS_25 Duct2.Fl_O 124.97 27.758 678.43 162.36 0.0000 75.67 25.143 659.61 366.9 0.3790 1.39677 +FS_3 HPC.Fl_O 124.97 123.561 1086.00 262.48 0.0000 21.51 114.996 1064.89 119.9 0.3246 1.37533 +FS_36 Bld3.Fl_O 113.72 123.561 1086.00 262.48 0.0000 19.57 114.996 1064.89 109.1 0.3246 1.37533 +FS_4 Burner.Fl_O 115.04 116.765 1847.82 468.71 0.0116 27.33 116.016 1844.90 483.4 0.0985 1.32570 +FS_45 HPT.Fl_O 126.29 41.844 1418.61 351.27 0.0105 73.35 39.355 1396.33 439.1 0.3027 1.34737 +FS_48 Duct3.Fl_O 126.29 41.635 1418.61 351.27 0.0105 73.72 39.158 1396.33 441.4 0.3027 1.34737 +FS_5 LPT.Fl_O 126.29 15.290 1122.38 273.98 0.0105 178.56 14.830 1113.24 1477.4 0.2119 1.36576 +FS_7 Duct4.Fl_O 126.29 15.137 1122.38 273.98 0.0105 180.36 14.892 1117.49 2018.9 0.1547 1.36576 +FS_9 Core_Nozz.Fl_O 126.29 15.137 1122.38 273.98 0.0105 180.36 13.664 1091.95 862.9 0.3897 1.36576 +FS_15 BypBld.Fl_O 983.91 18.676 592.39 141.65 0.0000 827.43 16.680 573.59 3795.6 0.4051 1.39916 +FS_17 Duct5.Fl_O 983.91 18.536 592.39 141.65 0.0000 833.68 16.555 573.59 3824.3 0.4051 1.39916 +FS_19 Byp_Nozz.Fl_O 983.91 18.536 592.39 141.65 0.0000 833.68 13.664 542.98 2706.4 0.6747 1.39916 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1055.08 1.158 0.8984 2246.087 1.0476 0.9005 -10147.1 58.49 19.56 +LPC 105.36 1.494 0.8335 2194.446 1.1452 0.8428 -3662.2 32.44 11.09 +HPC 75.67 4.451 0.8622 6133.500 1.6007 0.8872 -17702.2 38.43 38.95 +HPT 27.33 2.790 0.9165 163.187 1.2626 0.9057 17702.2 +LPT 73.72 2.723 0.9021 62.266 1.2639 0.8897 13809.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2022.97 1.110 0.9281 0.570 2.1909 0.5215 1.4369 0.9679 3943.9586 +LPC 113.01 1.151 0.8682 0.599 1.6601 0.9323 3.2631 0.9600 3662.6571 +HPC 179.89 16.955 0.8506 0.965 2.2521 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.214 0.9349 106.580 5.2141 1.4085 0.4249 0.9803 1.5311 +LPT 153.18 3.404 0.9009 76.766 3.4036 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4098.87 19604.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 822.91 197.40 41.793 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 822.91 197.40 41.793 +Duct1 0.0025 0.2562 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 822.91 197.40 41.793 +Duct2 0.0025 0.3790 365.99 +Duct3 0.0050 0.3027 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2119 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.3739 1086.00 262.48 123.561 +Duct5 0.0075 0.4051 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.8733 1086.00 262.48 123.561 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 592.39 141.65 18.676 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8732 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7014.8 13254.0 17702.2 +LP_Shaft 2345.2 30925.9 13809.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1847.82 0.9940 0.0550 1.31567 0.01157 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.356 0.9975 1.0000 0.9975 2706.36 0.675 768.8 23510.7 +Core_Nozz 1.108 0.9999 1.0000 0.9999 862.88 0.390 623.8 2448.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 85 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 5000.0 27.00 1345.36 44734.9 0.3611 16153.91 5.1136 0.00 21.798 2730.0 2660.9 2140.0 + core size:19.85 Q: 0.00 Maximum Thrust: 44734.9 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1345.36 12.228 527.84 126.15 0.0000 1631.17 12.228 527.84 -----.- 0.0000 1.40035 +FS_2 Inlet.Fl_O 1345.36 12.130 527.84 126.15 0.0000 1644.32 9.803 496.65 5943.4 0.5599 1.40035 +FS_21 Fan.Fl_O 1345.36 19.944 618.16 147.84 0.0000 1082.26 17.281 593.40 4515.2 0.4573 1.39871 +FS_13 Splitter.Fl_O2 1125.30 19.944 618.16 147.84 0.0000 905.24 17.313 593.72 3795.6 0.4543 1.39871 +FS_22 Splitter.Fl_O1 220.06 19.944 618.16 147.84 0.0000 177.03 17.107 591.70 719.5 0.4734 1.39871 +FS_23 Duct1.Fl_O 220.06 19.894 618.16 147.84 0.0000 177.47 17.065 591.70 721.3 0.4734 1.39871 +FS_24 LPC.Fl_O 220.06 46.851 813.92 195.21 0.0000 86.47 40.802 782.84 366.0 0.4499 1.39128 +FS_25 Duct2.Fl_O 220.06 46.733 813.92 195.21 0.0000 86.69 40.700 782.84 366.9 0.4499 1.39128 +FS_3 HPC.Fl_O 220.06 266.535 1388.14 339.81 0.0000 19.85 250.986 1366.35 119.9 0.2987 1.35659 +FS_36 Bld3.Fl_O 200.26 266.535 1388.14 339.81 0.0000 18.06 250.986 1366.35 109.1 0.2987 1.35659 +FS_4 Burner.Fl_O 204.74 251.875 2730.00 733.33 0.0224 27.41 250.251 2725.99 483.4 0.1000 1.29367 +FS_45 HPT.Fl_O 224.55 93.889 2139.95 556.90 0.0204 71.39 88.609 2110.87 439.1 0.2982 1.30922 +FS_48 Duct3.Fl_O 224.55 93.420 2139.95 556.90 0.0204 71.75 88.166 2110.87 441.4 0.2982 1.30922 +FS_5 LPT.Fl_O 224.55 19.852 1514.64 380.53 0.0204 284.06 18.245 1482.80 1477.4 0.3572 1.33549 +FS_7 Duct4.Fl_O 224.55 19.654 1514.64 380.53 0.0204 286.93 18.824 1498.30 2018.9 0.2547 1.33549 +FS_9 Core_Nozz.Fl_O 224.55 19.654 1514.64 380.53 0.0204 286.93 12.228 1342.76 862.9 0.8657 1.33549 +FS_15 BypBld.Fl_O 1125.30 19.944 618.16 147.84 0.0000 905.24 17.313 593.72 3795.6 0.4543 1.39871 +FS_17 Duct5.Fl_O 1125.30 19.794 618.16 147.84 0.0000 912.08 17.183 593.72 3824.3 0.4543 1.39871 +FS_19 Byp_Nozz.Fl_O 1125.30 19.794 618.16 147.84 0.0000 912.08 12.228 538.73 2706.4 0.8589 1.39871 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1644.32 1.644 0.8917 3804.398 1.1711 0.8990 -41285.8 25.32 16.14 +LPC 177.47 2.355 0.8676 3515.497 1.3167 0.8824 -14747.6 29.76 23.37 +HPC 86.69 5.703 0.8629 6357.086 1.7055 0.8904 -45023.8 19.38 19.36 +HPT 27.41 2.683 0.9139 152.413 1.2282 0.9045 45024.3 +LPT 71.75 4.706 0.9304 82.964 1.4128 0.9166 56034.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3152.74 1.448 0.9212 0.965 2.1146 0.5215 1.4369 0.9679 3943.9586 +LPC 190.36 1.415 0.9037 0.960 1.7816 0.9323 3.2631 0.9600 3662.6571 +HPC 206.08 22.742 0.8512 1.000 2.0562 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.960 0.9322 99.544 4.9604 1.4085 0.4249 0.9803 1.5311 +LPT 149.09 6.169 0.9292 102.284 6.1694 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1019.42 245.82 78.934 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1019.42 245.82 78.934 +Duct1 0.0025 0.4734 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1019.42 245.82 78.934 +Duct2 0.0025 0.4499 365.99 +Duct3 0.0050 0.2982 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3572 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.7021 1388.14 339.81 266.535 +Duct5 0.0075 0.4543 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.1033 1388.14 339.81 266.535 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 618.16 147.84 19.944 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.1136 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7963.5 29694.7 45024.3 +LP_Shaft 3837.9 76682.2 56034.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.00 0.9940 0.0550 4.48720 0.02241 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.619 0.9975 1.0000 0.9975 2706.36 0.859 974.9 34097.7 +Core_Nozz 1.607 0.9999 1.0000 0.9999 862.88 0.866 1524.1 10637.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 86 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 5000.0 27.00 1284.83 40262.3 0.3475 13991.21 5.3230 0.00 19.692 2618.7 2553.0 2046.0 + core size:19.98 Q: 0.00 Maximum Thrust: 44734.9 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1284.83 12.228 527.84 126.15 0.0000 1557.79 12.228 527.84 -----.- 0.0000 1.40035 +FS_2 Inlet.Fl_O 1284.83 12.130 527.84 126.15 0.0000 1570.35 10.069 500.46 5943.4 0.5226 1.40035 +FS_21 Fan.Fl_O 1284.83 19.243 609.92 145.86 0.0000 1064.06 16.776 586.51 4515.2 0.4472 1.39888 +FS_13 Splitter.Fl_O2 1081.64 19.243 609.92 145.86 0.0000 895.77 16.767 586.43 3795.6 0.4480 1.39888 +FS_22 Splitter.Fl_O1 203.20 19.243 609.92 145.86 0.0000 168.28 16.820 586.95 719.5 0.4428 1.39888 +FS_23 Duct1.Fl_O 203.20 19.195 609.92 145.86 0.0000 168.70 16.778 586.95 721.3 0.4428 1.39888 +FS_24 LPC.Fl_O 203.20 42.652 789.19 189.18 0.0000 86.36 37.162 759.09 366.0 0.4490 1.39247 +FS_25 Duct2.Fl_O 203.20 42.545 789.19 189.18 0.0000 86.58 37.069 759.09 366.9 0.4490 1.39247 +FS_3 HPC.Fl_O 203.20 240.792 1345.71 328.78 0.0000 19.98 226.554 1324.18 119.9 0.3005 1.35912 +FS_36 Bld3.Fl_O 184.91 240.792 1345.71 328.78 0.0000 18.18 226.554 1324.18 109.1 0.3005 1.35912 +FS_4 Burner.Fl_O 188.80 227.548 2618.74 698.62 0.0210 27.40 226.082 2614.87 483.4 0.0999 1.29679 +FS_45 HPT.Fl_O 207.08 84.135 2045.99 528.99 0.0191 71.84 79.341 2017.53 439.1 0.2999 1.31309 +FS_48 Duct3.Fl_O 207.08 83.715 2045.99 528.99 0.0191 72.20 78.944 2017.53 441.4 0.2999 1.31309 +FS_5 LPT.Fl_O 207.08 18.407 1456.13 364.19 0.0191 277.02 16.998 1426.98 1477.4 0.3464 1.33949 +FS_7 Duct4.Fl_O 207.08 18.223 1456.13 364.19 0.0191 279.82 17.493 1441.11 2018.9 0.2476 1.33949 +FS_9 Core_Nozz.Fl_O 207.08 18.223 1456.13 364.19 0.0191 279.82 12.228 1314.91 862.8 0.7894 1.33949 +FS_15 BypBld.Fl_O 1081.64 19.243 609.92 145.86 0.0000 895.77 16.767 586.43 3795.6 0.4480 1.39888 +FS_17 Duct5.Fl_O 1081.64 19.099 609.92 145.86 0.0000 902.54 16.642 586.43 3824.3 0.4480 1.39888 +FS_19 Byp_Nozz.Fl_O 1081.64 19.099 609.92 145.86 0.0000 902.54 12.228 537.00 2706.3 0.8243 1.39888 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1570.35 1.586 0.9060 3611.531 1.1555 0.9119 -35827.8 28.91 16.21 +LPC 168.70 2.222 0.8650 3359.736 1.2939 0.8792 -12455.7 29.94 21.94 +HPC 86.58 5.660 0.8626 6353.320 1.7052 0.8903 -40132.3 20.30 20.28 +HPT 27.40 2.705 0.9145 153.144 1.2328 0.9048 40132.0 +LPT 72.20 4.548 0.9278 80.546 1.4051 0.9136 48283.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3011.07 1.408 0.9360 0.916 1.9708 0.5215 1.4369 0.9679 3943.9586 +LPC 180.96 1.375 0.9011 0.917 1.7621 0.9323 3.2631 0.9600 3662.6571 +HPC 205.83 22.541 0.8510 0.999 2.0870 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.012 0.9328 100.021 5.0119 1.4085 0.4249 0.9803 1.5311 +LPT 150.03 5.949 0.9266 99.303 5.9493 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 988.15 238.04 71.588 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 988.15 238.04 71.588 +Duct1 0.0025 0.4428 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 988.15 238.04 71.588 +Duct2 0.0025 0.4490 365.99 +Duct3 0.0050 0.2999 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3464 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.1119 1345.71 328.78 240.792 +Duct5 0.0075 0.4480 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.1759 1345.71 328.78 240.792 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 609.92 145.86 19.243 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3230 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7836.9 26895.5 40132.0 +LP_Shaft 3643.3 69604.4 48283.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2618.74 0.9940 0.0550 3.88645 0.02102 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.562 0.9975 1.0000 0.9975 2706.36 0.824 934.1 31402.3 +Core_Nozz 1.490 0.9999 1.0000 0.9999 862.88 0.789 1376.6 8860.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 87 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 5000.0 27.00 1217.25 35788.7 0.3377 12085.80 5.4948 0.00 17.765 2511.1 2448.6 1957.6 + core size:20.12 Q: 0.00 Maximum Thrust: 44734.9 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1217.25 12.228 527.84 126.15 0.0000 1475.84 12.228 527.84 -----.- 0.0000 1.40035 +FS_2 Inlet.Fl_O 1217.25 12.130 527.84 126.15 0.0000 1487.75 10.330 504.15 5943.4 0.4843 1.40035 +FS_21 Fan.Fl_O 1217.25 18.489 602.14 143.99 0.0000 1042.46 16.231 580.17 4515.2 0.4355 1.39901 +FS_13 Splitter.Fl_O2 1029.83 18.489 602.14 143.99 0.0000 881.95 16.197 579.82 3795.6 0.4391 1.39901 +FS_22 Splitter.Fl_O1 187.42 18.489 602.14 143.99 0.0000 160.51 16.405 581.94 719.5 0.4169 1.39901 +FS_23 Duct1.Fl_O 187.42 18.443 602.14 143.99 0.0000 160.91 16.364 581.94 721.3 0.4169 1.39901 +FS_24 LPC.Fl_O 187.42 39.223 769.08 184.30 0.0000 85.51 34.293 740.43 366.0 0.4431 1.39344 +FS_25 Duct2.Fl_O 187.42 39.125 769.08 184.30 0.0000 85.72 34.207 740.43 366.9 0.4431 1.39344 +FS_3 HPC.Fl_O 187.42 217.229 1305.48 318.37 0.0000 20.12 204.192 1284.18 119.9 0.3026 1.36156 +FS_36 Bld3.Fl_O 170.55 217.229 1305.48 318.37 0.0000 18.31 204.192 1284.18 109.1 0.3026 1.36156 +FS_4 Burner.Fl_O 173.91 205.281 2511.10 665.39 0.0197 27.39 203.959 2507.36 483.4 0.0997 1.30009 +FS_45 HPT.Fl_O 190.78 75.586 1957.58 503.00 0.0179 72.06 71.252 1929.92 439.1 0.3004 1.31705 +FS_48 Duct3.Fl_O 190.78 75.208 1957.58 503.00 0.0179 72.42 70.895 1929.92 441.4 0.3004 1.31705 +FS_5 LPT.Fl_O 190.78 17.251 1403.40 349.59 0.0179 267.33 16.030 1377.28 1477.4 0.3319 1.34330 +FS_7 Duct4.Fl_O 190.78 17.079 1403.40 349.59 0.0179 270.03 16.444 1389.88 2018.9 0.2379 1.34330 +FS_9 Core_Nozz.Fl_O 190.78 17.079 1403.40 349.59 0.0179 270.03 12.228 1287.66 862.8 0.7190 1.34330 +FS_15 BypBld.Fl_O 1029.83 18.489 602.14 143.99 0.0000 881.95 16.197 579.82 3795.6 0.4391 1.39901 +FS_17 Duct5.Fl_O 1029.83 18.351 602.14 143.99 0.0000 888.62 16.075 579.82 3824.3 0.4391 1.39901 +FS_19 Byp_Nozz.Fl_O 1029.83 18.351 602.14 143.99 0.0000 888.62 12.228 536.22 2706.3 0.7842 1.39901 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1487.75 1.524 0.9090 3449.480 1.1408 0.9143 -30721.1 32.32 16.13 +LPC 160.91 2.127 0.8620 3229.656 1.2772 0.8757 -10688.7 29.37 20.20 +HPC 85.72 5.552 0.8638 6328.986 1.6975 0.8909 -35550.8 21.75 21.80 +HPT 27.39 2.716 0.9146 153.795 1.2361 0.9046 35550.7 +LPT 72.42 4.360 0.9255 78.650 1.3949 0.9113 41407.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2852.43 1.365 0.9391 0.875 1.8902 0.5215 1.4369 0.9679 3943.9586 +LPC 172.60 1.345 0.8979 0.882 1.7310 0.9323 3.2631 0.9600 3662.6571 +HPC 203.79 22.044 0.8521 0.996 2.1067 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.038 0.9329 100.446 5.0385 1.4085 0.4249 0.9803 1.5311 +LPT 150.49 5.686 0.9243 96.966 5.6865 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 960.64 231.22 65.217 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 960.64 231.22 65.217 +Duct1 0.0025 0.4169 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 960.64 231.22 65.217 +Duct2 0.0025 0.4431 365.99 +Duct3 0.0050 0.3004 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3319 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.5596 1305.48 318.37 217.229 +Duct5 0.0075 0.4391 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.3080 1305.48 318.37 217.229 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 602.14 143.99 18.489 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.4948 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7706.8 24227.5 35550.7 +LP_Shaft 3479.8 62496.6 41407.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2511.10 0.9940 0.0550 3.35717 0.01968 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.501 0.9975 1.0000 0.9975 2706.36 0.784 888.1 28424.7 +Core_Nozz 1.397 0.9999 1.0000 0.9999 862.88 0.719 1242.0 7364.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 88 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 5000.0 27.00 1062.58 26840.5 0.3230 8668.97 5.8436 0.00 14.019 2288.3 2232.4 1773.7 + core size:20.41 Q: 0.00 Maximum Thrust: 44734.9 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1062.58 12.228 527.84 126.15 0.0000 1288.32 12.228 527.84 -----.- 0.0000 1.40035 +FS_2 Inlet.Fl_O 1062.58 12.130 527.84 126.15 0.0000 1298.71 10.827 510.96 5943.4 0.4061 1.40035 +FS_21 Fan.Fl_O 1062.58 16.943 586.41 140.21 0.0000 980.01 15.150 567.99 4515.2 0.4030 1.39925 +FS_13 Splitter.Fl_O2 907.31 16.943 586.41 140.21 0.0000 836.81 15.084 567.29 3795.6 0.4108 1.39925 +FS_22 Splitter.Fl_O1 155.27 16.943 586.41 140.21 0.0000 143.20 15.469 571.38 719.5 0.3630 1.39925 +FS_23 Duct1.Fl_O 155.27 16.900 586.41 140.21 0.0000 143.56 15.430 571.38 721.3 0.3630 1.39925 +FS_24 LPC.Fl_O 155.27 32.055 723.32 173.21 0.0000 84.06 28.186 697.42 366.0 0.4332 1.39524 +FS_25 Duct2.Fl_O 155.27 31.975 723.32 173.21 0.0000 84.27 28.115 697.42 366.9 0.4332 1.39524 +FS_3 HPC.Fl_O 155.27 171.413 1219.09 296.18 0.0000 20.41 160.804 1198.33 119.9 0.3069 1.36694 +FS_36 Bld3.Fl_O 141.29 171.413 1219.09 296.18 0.0000 18.57 160.804 1198.33 109.1 0.3069 1.36694 +FS_4 Burner.Fl_O 143.70 161.986 2288.27 597.80 0.0170 27.38 160.943 2284.80 483.4 0.0994 1.30738 +FS_45 HPT.Fl_O 157.67 58.979 1773.70 449.97 0.0155 72.65 55.538 1747.64 439.1 0.3021 1.32617 +FS_48 Duct3.Fl_O 157.67 58.684 1773.70 449.97 0.0155 73.02 55.260 1747.64 441.4 0.3021 1.32617 +FS_5 LPT.Fl_O 157.67 15.414 1305.17 322.74 0.0155 238.46 14.562 1286.02 1477.4 0.2910 1.35083 +FS_7 Duct4.Fl_O 157.67 15.260 1305.17 322.74 0.0155 240.87 14.813 1295.13 2018.9 0.2102 1.35083 +FS_9 Core_Nozz.Fl_O 157.67 15.260 1305.17 322.74 0.0155 240.87 12.227 1231.86 863.0 0.5800 1.35083 +FS_15 BypBld.Fl_O 907.31 16.943 586.41 140.21 0.0000 836.81 15.084 567.29 3795.6 0.4108 1.39925 +FS_17 Duct5.Fl_O 907.31 16.816 586.41 140.21 0.0000 843.13 14.971 567.29 3824.3 0.4108 1.39925 +FS_19 Byp_Nozz.Fl_O 907.31 16.816 586.41 140.21 0.0000 843.13 12.228 535.39 2706.4 0.6904 1.39925 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1298.71 1.397 0.9029 3066.802 1.1110 0.9074 -21136.2 35.91 15.11 +LPC 143.56 1.897 0.8556 2909.612 1.2335 0.8680 -7248.6 29.52 17.41 +HPC 84.27 5.361 0.8644 6293.721 1.6854 0.8910 -27015.5 24.59 24.70 +HPT 27.38 2.747 0.9149 155.372 1.2444 0.9048 27015.5 +LPT 73.02 3.807 0.9213 73.460 1.3590 0.9077 28383.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2490.09 1.276 0.9328 0.778 1.7943 0.5215 1.4369 0.9679 3943.9586 +LPC 153.99 1.275 0.8913 0.794 1.7021 0.9323 3.2631 0.9600 3662.6571 +HPC 200.35 21.159 0.8527 0.990 2.1483 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.111 0.9332 101.476 5.1106 1.4085 0.4249 0.9803 1.5311 +LPT 151.73 4.916 0.9201 90.567 4.9159 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 899.90 216.25 52.403 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 899.90 216.25 52.403 +Duct1 0.0025 0.3630 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 899.90 216.25 52.403 +Duct2 0.0025 0.4332 365.99 +Duct3 0.0050 0.3021 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2910 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.4343 1219.09 296.18 171.413 +Duct5 0.0075 0.4108 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.5396 1219.09 296.18 171.413 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 586.41 140.21 16.943 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.8436 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7432.4 19090.6 27015.5 +LP_Shaft 3093.8 48184.6 28383.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2288.27 0.9940 0.0550 2.40805 0.01704 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.375 0.9975 1.0000 0.9975 2706.36 0.690 781.2 22029.2 +Core_Nozz 1.248 0.9999 1.0000 0.9999 862.88 0.580 981.8 4811.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:45 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 89 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 8/ 18/ 1/ 6 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 5000.0 27.00 874.14 17894.0 0.3141 5621.35 6.1562 0.00 10.344 2022.4 1974.5 1556.8 + core size:20.80 Q: 0.00 Maximum Thrust: 44734.9 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 874.14 12.228 527.84 126.15 0.0000 1059.85 12.228 527.84 -----.- 0.0000 1.40035 +FS_2 Inlet.Fl_O 874.14 12.130 527.84 126.15 0.0000 1068.39 11.286 517.07 5943.4 0.3224 1.40035 +FS_21 Fan.Fl_O 874.14 15.374 569.12 136.06 0.0000 875.27 14.113 555.38 4515.2 0.3519 1.39955 +FS_13 Splitter.Fl_O2 751.99 15.374 569.12 136.06 0.0000 752.96 14.047 554.63 3795.6 0.3615 1.39955 +FS_22 Splitter.Fl_O1 122.15 15.374 569.12 136.06 0.0000 122.31 14.427 558.88 719.5 0.3028 1.39955 +FS_23 Duct1.Fl_O 122.15 15.336 569.12 136.06 0.0000 122.62 14.391 558.88 721.3 0.3028 1.39955 +FS_24 LPC.Fl_O 122.15 25.033 669.86 160.29 0.0000 81.49 22.223 647.55 366.0 0.4162 1.39708 +FS_25 Duct2.Fl_O 122.15 24.971 669.86 160.29 0.0000 81.70 22.168 647.55 366.9 0.4162 1.39708 +FS_3 HPC.Fl_O 122.15 126.480 1114.16 269.56 0.0000 20.80 118.325 1094.12 119.9 0.3128 1.37355 +FS_36 Bld3.Fl_O 111.16 126.480 1114.16 269.56 0.0000 18.93 118.325 1094.12 109.1 0.3128 1.37355 +FS_4 Burner.Fl_O 112.72 119.524 2022.42 519.27 0.0140 27.37 118.755 2019.28 483.4 0.0990 1.31736 +FS_45 HPT.Fl_O 123.71 43.037 1556.84 389.18 0.0128 73.19 40.487 1532.96 439.1 0.3031 1.33835 +FS_48 Duct3.Fl_O 123.71 42.821 1556.84 389.18 0.0128 73.56 40.285 1532.96 441.4 0.3031 1.33835 +FS_5 LPT.Fl_O 123.71 14.071 1202.94 295.27 0.0128 196.77 13.553 1191.07 1477.4 0.2355 1.35910 +FS_7 Duct4.Fl_O 123.71 13.930 1202.94 295.27 0.0128 198.76 13.656 1196.63 2018.9 0.1714 1.35910 +FS_9 Core_Nozz.Fl_O 123.71 13.930 1202.94 295.27 0.0128 198.76 12.228 1162.16 862.9 0.4411 1.35910 +FS_15 BypBld.Fl_O 751.99 15.374 569.12 136.06 0.0000 752.96 14.047 554.63 3795.6 0.3615 1.39955 +FS_17 Duct5.Fl_O 751.99 15.259 569.12 136.06 0.0000 758.65 13.941 554.63 3824.3 0.3615 1.39955 +FS_19 Byp_Nozz.Fl_O 751.99 15.259 569.12 136.06 0.0000 758.65 12.228 534.21 2706.4 0.5716 1.39955 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1068.39 1.267 0.8962 2587.052 1.0782 0.8997 -12250.8 34.48 12.53 +LPC 122.62 1.632 0.8466 2491.463 1.1770 0.8569 -4188.3 33.11 14.65 +HPC 81.70 5.065 0.8642 6242.450 1.6633 0.8906 -18885.0 28.91 29.08 +HPT 27.37 2.777 0.9154 157.749 1.2550 0.9051 18885.0 +LPT 73.56 3.043 0.9095 66.144 1.2942 0.8965 16438.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2048.50 1.186 0.9259 0.656 1.7070 0.5215 1.4369 0.9679 3943.9586 +LPC 131.52 1.194 0.8819 0.680 1.7193 0.9323 3.2631 0.9600 3662.6571 +HPC 194.23 19.792 0.8526 0.982 2.1847 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.183 0.9338 103.028 5.1830 1.4085 0.4249 0.9803 1.5311 +LPT 152.85 3.850 0.9083 81.547 3.8502 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 827.57 198.53 39.842 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 827.57 198.53 39.842 +Duct1 0.0025 0.3028 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 827.57 198.53 39.842 +Duct2 0.0025 0.4162 365.99 +Duct3 0.0050 0.3031 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2355 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.2753 1114.16 269.56 126.480 +Duct5 0.0075 0.3615 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.7183 1114.16 269.56 126.480 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 569.12 136.06 15.374 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.1562 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7094.2 13981.4 18885.0 +LP_Shaft 2609.8 33082.3 16438.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2022.42 0.9940 0.0550 1.56149 0.01405 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.248 0.9975 1.0000 0.9975 2706.36 0.572 646.0 15099.2 +Core_Nozz 1.139 0.9999 1.0000 0.9999 862.88 0.441 726.8 2794.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 90 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 5000.0 27.00 623.93 8946.7 0.3235 2894.46 6.1842 0.00 6.647 1660.9 1624.1 1266.9 + core size:21.52 Q: 0.00 Maximum Thrust: 44734.9 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 623.93 12.228 527.84 126.15 0.0000 756.48 12.228 527.84 -----.- 0.0000 1.40035 +FS_2 Inlet.Fl_O 623.93 12.130 527.84 126.15 0.0000 762.58 11.717 522.64 5943.4 0.2229 1.40035 +FS_21 Fan.Fl_O 623.93 13.813 550.27 131.53 0.0000 683.75 13.148 542.56 4515.2 0.2664 1.39990 +FS_13 Splitter.Fl_O2 537.08 13.813 550.27 131.53 0.0000 588.57 13.113 542.16 3795.6 0.2734 1.39990 +FS_22 Splitter.Fl_O1 86.85 13.813 550.27 131.53 0.0000 95.17 13.312 544.49 719.5 0.2303 1.39990 +FS_23 Duct1.Fl_O 86.85 13.778 550.27 131.53 0.0000 95.41 13.279 544.49 721.3 0.2303 1.39990 +FS_24 LPC.Fl_O 86.85 18.110 604.18 144.48 0.0000 76.06 16.374 587.06 366.0 0.3823 1.39898 +FS_25 Duct2.Fl_O 86.85 18.065 604.18 144.48 0.0000 76.25 16.333 587.06 366.9 0.3823 1.39898 +FS_3 HPC.Fl_O 86.85 81.283 974.11 234.56 0.0000 21.52 75.645 954.91 119.9 0.3239 1.38232 +FS_36 Bld3.Fl_O 79.03 81.283 974.11 234.56 0.0000 19.58 75.645 954.91 109.1 0.3239 1.38232 +FS_4 Burner.Fl_O 79.84 76.812 1660.88 416.45 0.0102 27.33 76.320 1658.20 483.4 0.0982 1.33501 +FS_45 HPT.Fl_O 87.65 27.368 1266.89 310.97 0.0093 73.56 25.731 1246.45 439.1 0.3025 1.35743 +FS_48 Duct3.Fl_O 87.65 27.231 1266.89 310.97 0.0093 73.93 25.602 1246.45 441.4 0.3025 1.35743 +FS_5 LPT.Fl_O 87.65 13.109 1067.96 259.84 0.0093 141.00 12.866 1062.58 1477.4 0.1653 1.37009 +FS_7 Duct4.Fl_O 87.65 12.978 1067.96 259.84 0.0093 142.43 12.848 1065.06 2018.9 0.1213 1.37009 +FS_9 Core_Nozz.Fl_O 87.65 12.978 1067.96 259.84 0.0093 142.43 12.228 1050.88 863.0 0.2961 1.37009 +FS_15 BypBld.Fl_O 537.08 13.813 550.27 131.53 0.0000 588.57 13.113 542.16 3795.6 0.2734 1.39990 +FS_17 Duct5.Fl_O 537.08 13.709 550.27 131.53 0.0000 593.02 13.015 542.16 3824.3 0.2734 1.39990 +FS_19 Byp_Nozz.Fl_O 537.08 13.709 550.27 131.53 0.0000 593.02 12.228 532.57 2706.4 0.4076 1.39990 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 762.58 1.139 0.8906 1906.220 1.0425 0.8927 -4749.6 35.69 7.25 +LPC 95.41 1.314 0.8285 1866.966 1.0980 0.8350 -1591.2 46.18 12.65 +HPC 76.25 4.500 0.8621 6144.520 1.6123 0.8873 -11068.6 37.81 38.30 +HPT 27.33 2.807 0.9165 162.726 1.2706 0.9056 11069.0 +LPT 73.93 2.077 0.8862 54.027 1.1863 0.8760 6340.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1462.15 1.097 0.9201 0.483 1.6287 0.5215 1.4369 0.9679 3943.9586 +LPC 102.34 1.096 0.8630 0.510 1.8821 0.9323 3.2631 0.9600 3662.6571 +HPC 181.28 17.178 0.8505 0.967 2.2484 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.252 0.9349 106.280 5.2521 1.4085 0.4249 0.9803 1.5311 +LPT 153.61 2.503 0.8851 66.608 2.5028 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 734.89 176.01 27.326 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 734.89 176.01 27.326 +Duct1 0.0025 0.2303 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 734.89 176.01 27.326 +Duct2 0.0025 0.3823 365.99 +Duct3 0.0050 0.3025 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1653 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.0397 974.11 234.56 81.283 +Duct5 0.0075 0.2734 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.7766 974.11 234.56 81.283 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 550.27 131.53 13.813 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.1842 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6631.7 8766.3 11069.0 +LP_Shaft 1923.0 17317.0 6340.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1660.88 0.9940 0.0550 0.80402 0.01017 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.121 0.9975 1.0000 0.9975 2706.36 0.408 460.0 7678.2 +Core_Nozz 1.061 0.9999 1.0000 0.9999 862.88 0.296 465.6 1268.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 91 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 5000.0 27.00 1354.11 40535.7 0.3999 16209.03 5.1284 112.64 21.734 2730.0 2661.0 2139.9 + core size:19.86 Q: 12.33 Maximum Thrust: 40535.7 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1354.11 12.313 528.90 126.40 0.0000 1631.96 12.228 527.84 27686.0 0.1000 1.40033 +FS_2 Inlet.Fl_O 1354.11 12.227 528.90 126.40 0.0000 1643.47 9.885 497.69 5943.4 0.5594 1.40033 +FS_21 Fan.Fl_O 1354.11 20.067 619.02 148.05 0.0000 1083.38 17.381 594.17 4515.2 0.4579 1.39869 +FS_13 Splitter.Fl_O2 1133.15 20.067 619.02 148.05 0.0000 906.60 17.410 594.45 3795.6 0.4552 1.39869 +FS_22 Splitter.Fl_O1 220.96 20.067 619.02 148.05 0.0000 176.78 17.222 592.62 719.5 0.4725 1.39869 +FS_23 Duct1.Fl_O 220.96 20.016 619.02 148.05 0.0000 177.22 17.179 592.62 721.3 0.4725 1.39869 +FS_24 LPC.Fl_O 220.96 47.098 814.84 195.43 0.0000 86.42 41.026 783.78 366.0 0.4495 1.39123 +FS_25 Duct2.Fl_O 220.96 46.980 814.84 195.43 0.0000 86.63 40.924 783.78 366.9 0.4495 1.39123 +FS_3 HPC.Fl_O 220.96 267.626 1389.07 340.06 0.0000 19.86 252.002 1367.26 119.9 0.2988 1.35654 +FS_36 Bld3.Fl_O 201.07 267.626 1389.07 340.06 0.0000 18.07 252.002 1367.26 109.1 0.2988 1.35654 +FS_4 Burner.Fl_O 205.57 252.906 2730.00 733.31 0.0224 27.41 251.276 2725.99 483.4 0.1000 1.29368 +FS_45 HPT.Fl_O 225.46 94.265 2139.94 556.89 0.0204 71.40 88.963 2110.85 439.1 0.2983 1.30923 +FS_48 Duct3.Fl_O 225.46 93.793 2139.94 556.89 0.0204 71.75 88.518 2110.85 441.4 0.2983 1.30923 +FS_5 LPT.Fl_O 225.46 19.916 1514.41 380.46 0.0204 284.28 18.301 1482.52 1477.4 0.3575 1.33551 +FS_7 Duct4.Fl_O 225.46 19.716 1514.41 380.46 0.0204 287.15 18.883 1498.05 2018.9 0.2550 1.33551 +FS_9 Core_Nozz.Fl_O 225.46 19.716 1514.41 380.46 0.0204 287.15 12.228 1341.45 862.9 0.8688 1.33551 +FS_15 BypBld.Fl_O 1133.15 20.067 619.02 148.05 0.0000 906.60 17.410 594.45 3795.6 0.4552 1.39869 +FS_17 Duct5.Fl_O 1133.15 19.916 619.02 148.05 0.0000 913.45 17.279 594.45 3824.3 0.4552 1.39869 +FS_19 Byp_Nozz.Fl_O 1133.15 19.916 619.02 148.05 0.0000 913.45 12.228 538.54 2706.4 0.8648 1.39869 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1643.47 1.641 0.8917 3799.441 1.1704 0.8990 -41466.4 25.56 16.28 +LPC 177.22 2.353 0.8675 3511.978 1.3163 0.8823 -14813.0 29.70 23.29 +HPC 86.63 5.697 0.8630 6355.402 1.7047 0.8905 -45212.9 19.47 19.45 +HPT 27.41 2.683 0.9139 152.459 1.2282 0.9045 45213.2 +LPT 71.75 4.710 0.9303 82.939 1.4131 0.9165 56279.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3151.13 1.446 0.9213 0.963 2.1203 0.5215 1.4369 0.9679 3943.9586 +LPC 190.10 1.415 0.9036 0.959 1.7795 0.9323 3.2631 0.9600 3662.6571 +HPC 205.95 22.711 0.8513 1.000 2.0575 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.961 0.9323 99.574 4.9610 1.4085 0.4249 0.9803 1.5311 +LPT 149.10 6.175 0.9291 102.253 6.1747 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 27685.98 4740.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1020.35 246.05 79.305 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1020.35 246.05 79.305 +Duct1 0.0025 0.4725 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1020.35 246.05 79.305 +Duct2 0.0025 0.4495 365.99 +Duct3 0.0050 0.2983 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3575 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.7335 1389.07 340.06 267.626 +Duct5 0.0075 0.4552 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.1526 1389.07 340.06 267.626 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 619.02 148.05 20.067 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.1284 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7965.9 29810.3 45213.2 +LP_Shaft 3836.7 77041.3 56279.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.00 0.9940 0.0550 4.50251 0.02239 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.629 0.9975 1.0000 0.9975 2706.36 0.865 981.4 34563.0 +Core_Nozz 1.612 0.9999 1.0000 0.9999 862.88 0.869 1528.8 10713.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 92 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 5000.0 27.00 1297.17 36482.4 0.3876 14142.23 5.3302 112.64 19.741 2624.0 2558.1 2050.4 + core size:19.98 Q: 12.33 Maximum Thrust: 40535.7 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1297.17 12.313 528.90 126.40 0.0000 1563.34 12.228 527.84 26521.8 0.1000 1.40033 +FS_2 Inlet.Fl_O 1297.17 12.227 528.90 126.40 0.0000 1574.37 10.136 501.27 5943.4 0.5245 1.40033 +FS_21 Fan.Fl_O 1297.17 19.400 611.19 146.17 0.0000 1066.67 16.898 587.59 4515.2 0.4486 1.39885 +FS_13 Splitter.Fl_O2 1092.25 19.400 611.19 146.17 0.0000 898.16 16.888 587.49 3795.6 0.4496 1.39885 +FS_22 Splitter.Fl_O1 204.92 19.400 611.19 146.17 0.0000 168.50 16.950 588.10 719.5 0.4436 1.39885 +FS_23 Duct1.Fl_O 204.92 19.352 611.19 146.17 0.0000 168.93 16.907 588.10 721.3 0.4436 1.39885 +FS_24 LPC.Fl_O 204.92 43.099 791.38 189.72 0.0000 86.31 37.559 761.25 366.0 0.4486 1.39236 +FS_25 Duct2.Fl_O 204.92 42.991 791.38 189.72 0.0000 86.53 37.466 761.25 366.9 0.4486 1.39236 +FS_3 HPC.Fl_O 204.92 243.079 1348.77 329.57 0.0000 19.98 228.703 1327.20 119.9 0.3006 1.35893 +FS_36 Bld3.Fl_O 186.47 243.079 1348.77 329.57 0.0000 18.18 228.703 1327.20 109.1 0.3006 1.35893 +FS_4 Burner.Fl_O 190.40 229.710 2624.00 700.24 0.0211 27.40 228.229 2620.12 483.4 0.0999 1.29665 +FS_45 HPT.Fl_O 208.85 84.955 2050.39 530.28 0.0192 71.83 80.116 2021.90 439.1 0.2998 1.31291 +FS_48 Duct3.Fl_O 208.85 84.530 2050.39 530.28 0.0192 72.19 79.715 2021.90 441.4 0.2998 1.31291 +FS_5 LPT.Fl_O 208.85 18.525 1458.34 364.81 0.0192 277.81 17.098 1428.97 1477.4 0.3475 1.33934 +FS_7 Duct4.Fl_O 208.85 18.340 1458.34 364.81 0.0192 280.61 17.601 1443.22 2018.9 0.2483 1.33934 +FS_9 Core_Nozz.Fl_O 208.85 18.340 1458.34 364.81 0.0192 280.61 12.228 1314.78 862.9 0.7960 1.33934 +FS_15 BypBld.Fl_O 1092.25 19.400 611.19 146.17 0.0000 898.16 16.888 587.49 3795.6 0.4496 1.39885 +FS_17 Duct5.Fl_O 1092.25 19.255 611.19 146.17 0.0000 904.95 16.762 587.49 3824.3 0.4496 1.39885 +FS_19 Byp_Nozz.Fl_O 1092.25 19.255 611.19 146.17 0.0000 904.95 12.228 536.87 2706.3 0.8323 1.39885 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1574.37 1.587 0.9057 3616.948 1.1556 0.9116 -36268.4 29.01 16.38 +LPC 168.93 2.227 0.8651 3364.632 1.2948 0.8792 -12626.9 29.86 21.93 +HPC 86.53 5.654 0.8627 6351.680 1.7043 0.8903 -40547.4 20.36 20.34 +HPT 27.40 2.704 0.9145 153.163 1.2326 0.9048 40547.7 +LPT 72.19 4.563 0.9279 80.661 1.4060 0.9137 48895.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3018.73 1.408 0.9356 0.917 1.9841 0.5215 1.4369 0.9679 3943.9586 +LPC 181.20 1.376 0.9011 0.919 1.7609 0.9323 3.2631 0.9600 3662.6571 +HPC 205.70 22.515 0.8511 0.999 2.0870 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.010 0.9328 100.033 5.0103 1.4085 0.4249 0.9803 1.5311 +LPT 150.01 5.970 0.9267 99.445 5.9702 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 26521.80 4541.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 990.67 238.67 72.304 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 990.67 238.67 72.304 +Duct1 0.0025 0.4436 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 990.67 238.67 72.304 +Duct2 0.0025 0.4486 365.99 +Duct3 0.0050 0.2998 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3475 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.1721 1348.77 329.57 243.079 +Duct5 0.0075 0.4496 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.2705 1348.77 329.57 243.079 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 611.19 146.17 19.400 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3302 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7845.8 27143.4 40547.7 +LP_Shaft 3652.4 70310.3 48895.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2624.00 0.9940 0.0550 3.92840 0.02107 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.575 0.9975 1.0000 0.9975 2706.36 0.832 943.0 32013.7 +Core_Nozz 1.500 0.9999 1.0000 0.9999 862.88 0.796 1388.1 9010.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 93 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 5000.0 27.00 1233.53 32428.8 0.3794 12303.37 5.4978 112.64 17.906 2520.8 2458.0 1965.7 + core size:20.11 Q: 12.33 Maximum Thrust: 40535.7 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1233.53 12.313 528.90 126.40 0.0000 1486.64 12.228 527.84 25220.6 0.1000 1.40033 +FS_2 Inlet.Fl_O 1233.53 12.227 528.90 126.40 0.0000 1497.13 10.385 504.76 5943.4 0.4885 1.40033 +FS_21 Fan.Fl_O 1233.53 18.680 603.73 144.37 0.0000 1047.00 16.375 581.47 4515.2 0.4379 1.39899 +FS_13 Splitter.Fl_O2 1043.69 18.680 603.73 144.37 0.0000 885.87 16.339 581.11 3795.6 0.4416 1.39899 +FS_22 Splitter.Fl_O1 189.84 18.680 603.73 144.37 0.0000 161.13 16.556 583.30 719.5 0.4190 1.39899 +FS_23 Duct1.Fl_O 189.84 18.633 603.73 144.37 0.0000 161.54 16.514 583.30 721.3 0.4190 1.39899 +FS_24 LPC.Fl_O 189.84 39.831 772.32 185.08 0.0000 85.47 34.830 743.59 366.0 0.4428 1.39328 +FS_25 Duct2.Fl_O 189.84 39.731 772.32 185.08 0.0000 85.68 34.743 743.59 366.9 0.4428 1.39328 +FS_3 HPC.Fl_O 189.84 220.478 1310.42 319.64 0.0000 20.11 207.250 1289.05 119.9 0.3026 1.36126 +FS_36 Bld3.Fl_O 172.75 220.478 1310.42 319.64 0.0000 18.30 207.250 1289.05 109.1 0.3026 1.36126 +FS_4 Burner.Fl_O 176.17 208.352 2520.80 668.36 0.0198 27.39 207.010 2517.05 483.4 0.0998 1.29980 +FS_45 HPT.Fl_O 193.25 76.756 1965.65 505.35 0.0180 72.03 72.358 1937.92 439.1 0.3003 1.31669 +FS_48 Duct3.Fl_O 193.25 76.372 1965.65 505.35 0.0180 72.39 71.996 1937.92 441.4 0.3003 1.31669 +FS_5 LPT.Fl_O 193.25 17.399 1407.30 350.67 0.0180 268.87 16.152 1380.78 1477.4 0.3342 1.34301 +FS_7 Duct4.Fl_O 193.25 17.225 1407.30 350.67 0.0180 271.58 16.578 1393.58 2018.9 0.2394 1.34301 +FS_9 Core_Nozz.Fl_O 193.25 17.225 1407.30 350.67 0.0180 271.58 12.228 1288.45 862.8 0.7286 1.34301 +FS_15 BypBld.Fl_O 1043.69 18.680 603.73 144.37 0.0000 885.87 16.339 581.11 3795.6 0.4416 1.39899 +FS_17 Duct5.Fl_O 1043.69 18.540 603.73 144.37 0.0000 892.56 16.217 581.11 3824.3 0.4416 1.39899 +FS_19 Byp_Nozz.Fl_O 1043.69 18.540 603.73 144.37 0.0000 892.56 12.228 536.07 2706.3 0.7947 1.39899 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1497.13 1.528 0.9094 3463.992 1.1415 0.9146 -31359.5 32.37 16.36 +LPC 161.54 2.138 0.8621 3242.192 1.2792 0.8759 -10935.1 29.28 20.25 +HPC 85.68 5.549 0.8638 6327.995 1.6967 0.8910 -36140.5 21.77 21.82 +HPT 27.39 2.714 0.9146 153.798 1.2357 0.9046 36140.5 +LPT 72.39 4.389 0.9257 78.897 1.3968 0.9115 42294.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2870.54 1.367 0.9395 0.878 1.9061 0.5215 1.4369 0.9679 3943.9586 +LPC 173.27 1.349 0.8980 0.885 1.7303 0.9323 3.2631 0.9600 3662.6571 +HPC 203.70 22.030 0.8522 0.995 2.1059 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.035 0.9329 100.448 5.0352 1.4085 0.4249 0.9803 1.5311 +LPT 150.43 5.728 0.9245 97.271 5.7280 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 25220.62 4318.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 964.51 232.18 66.211 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 964.51 232.18 66.211 +Duct1 0.0025 0.4190 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 964.51 232.18 66.211 +Duct2 0.0025 0.4428 365.99 +Duct3 0.0050 0.3003 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3342 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.6443 1310.42 319.64 220.478 +Duct5 0.0075 0.4416 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.4410 1310.42 319.64 220.478 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 603.73 144.37 18.680 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.4978 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7721.8 24581.5 36140.5 +LP_Shaft 3498.0 63503.8 42294.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2520.80 0.9940 0.0550 3.41760 0.01978 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.516 0.9975 1.0000 0.9975 2706.36 0.795 899.7 29186.4 +Core_Nozz 1.409 0.9999 1.0000 0.9999 862.88 0.729 1258.8 7560.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 94 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 5000.0 27.00 1087.67 24321.2 0.3690 8975.70 5.8480 112.64 14.304 2307.8 2251.4 1789.9 + core size:20.39 Q: 12.33 Maximum Thrust: 40535.7 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1087.67 12.313 528.90 126.40 0.0000 1310.86 12.228 527.84 22238.5 0.1000 1.40033 +FS_2 Inlet.Fl_O 1087.67 12.227 528.90 126.40 0.0000 1320.11 10.863 511.30 5943.4 0.4145 1.40033 +FS_21 Fan.Fl_O 1087.67 17.190 588.62 140.74 0.0000 990.60 15.326 569.65 4515.2 0.4084 1.39922 +FS_13 Splitter.Fl_O2 928.84 17.190 588.62 140.74 0.0000 845.94 15.257 568.92 3795.6 0.4164 1.39922 +FS_22 Splitter.Fl_O1 158.83 17.190 588.62 140.74 0.0000 144.65 15.661 573.18 719.5 0.3673 1.39922 +FS_23 Duct1.Fl_O 158.83 17.147 588.62 140.74 0.0000 145.02 15.621 573.18 721.3 0.3673 1.39922 +FS_24 LPC.Fl_O 158.83 32.920 728.81 174.54 0.0000 84.05 28.947 702.73 366.0 0.4332 1.39506 +FS_25 Duct2.Fl_O 158.83 32.837 728.81 174.54 0.0000 84.26 28.875 702.73 366.9 0.4332 1.39506 +FS_3 HPC.Fl_O 158.83 176.128 1228.00 298.46 0.0000 20.39 165.246 1207.15 119.9 0.3067 1.36638 +FS_36 Bld3.Fl_O 144.54 176.128 1228.00 298.46 0.0000 18.56 165.246 1207.15 109.1 0.3067 1.36638 +FS_4 Burner.Fl_O 147.03 166.441 2307.78 603.64 0.0173 27.38 165.370 2304.28 483.4 0.0994 1.30671 +FS_45 HPT.Fl_O 161.32 60.675 1789.94 454.59 0.0157 72.59 57.142 1763.74 439.1 0.3018 1.32533 +FS_48 Duct3.Fl_O 161.32 60.372 1789.94 454.59 0.0157 72.95 56.857 1763.74 441.4 0.3018 1.32533 +FS_5 LPT.Fl_O 161.32 15.580 1312.23 324.66 0.0157 242.05 14.691 1292.36 1477.4 0.2960 1.35027 +FS_7 Duct4.Fl_O 161.32 15.424 1312.23 324.66 0.0157 244.49 14.958 1301.83 2018.9 0.2135 1.35027 +FS_9 Core_Nozz.Fl_O 161.32 15.424 1312.23 324.66 0.0157 244.49 12.227 1235.14 862.9 0.5944 1.35027 +FS_15 BypBld.Fl_O 928.84 17.190 588.62 140.74 0.0000 845.94 15.257 568.92 3795.6 0.4164 1.39922 +FS_17 Duct5.Fl_O 928.84 17.061 588.62 140.74 0.0000 852.33 15.142 568.92 3824.3 0.4164 1.39922 +FS_19 Byp_Nozz.Fl_O 928.84 17.061 588.62 140.74 0.0000 852.33 12.228 535.19 2706.4 0.7066 1.39922 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1320.11 1.406 0.9052 3102.145 1.1129 0.9097 -22063.6 36.36 15.53 +LPC 145.02 1.920 0.8560 2940.545 1.2382 0.8685 -7594.4 29.23 17.50 +HPC 84.26 5.364 0.8645 6293.524 1.6849 0.8911 -27848.8 24.50 24.61 +HPT 27.38 2.743 0.9149 155.296 1.2436 0.9048 27848.8 +LPT 72.95 3.875 0.9219 74.043 1.3640 0.9082 29656.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2531.13 1.282 0.9351 0.787 1.8158 0.5215 1.4369 0.9679 3943.9586 +LPC 155.56 1.282 0.8916 0.803 1.6984 0.9323 3.2631 0.9600 3662.6571 +HPC 200.32 21.172 0.8528 0.990 2.1451 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.103 0.9332 101.426 5.1027 1.4085 0.4249 0.9803 1.5311 +LPT 151.59 5.011 0.9207 91.285 5.0106 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 22238.55 3807.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 906.66 217.91 53.829 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 906.66 217.91 53.829 +Duct1 0.0025 0.3673 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 906.66 217.91 53.829 +Duct2 0.0025 0.4332 365.99 +Duct3 0.0050 0.3018 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2960 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.5591 1228.00 298.46 176.128 +Duct5 0.0075 0.4164 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.7357 1228.00 298.46 176.128 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 588.62 140.74 17.190 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.8480 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7460.3 19605.8 27848.8 +LP_Shaft 3132.6 49722.8 29656.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2307.78 0.9940 0.0550 2.49325 0.01725 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.395 0.9975 1.0000 0.9975 2706.36 0.707 799.4 23078.7 +Core_Nozz 1.261 0.9999 1.0000 0.9999 862.88 0.594 1007.3 5050.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 95 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 8/ 18/ 1/ 6 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 5000.0 27.00 909.82 16214.2 0.3683 5972.37 6.1851 112.64 10.738 2055.5 2006.7 1584.0 + core size:20.76 Q: 12.33 Maximum Thrust: 40535.7 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 909.82 12.313 528.90 126.40 0.0000 1096.51 12.228 527.84 18602.1 0.1000 1.40033 +FS_2 Inlet.Fl_O 909.82 12.227 528.90 126.40 0.0000 1104.24 11.314 517.28 5943.4 0.3349 1.40033 +FS_21 Fan.Fl_O 909.82 15.655 571.91 136.73 0.0000 896.87 14.299 557.31 4515.2 0.3621 1.39950 +FS_13 Splitter.Fl_O2 783.19 15.655 571.91 136.73 0.0000 772.04 14.225 556.49 3795.6 0.3724 1.39950 +FS_22 Splitter.Fl_O1 126.63 15.655 571.91 136.73 0.0000 124.82 14.647 561.15 719.5 0.3098 1.39950 +FS_23 Duct1.Fl_O 126.63 15.616 571.91 136.73 0.0000 125.14 14.610 561.15 721.3 0.3098 1.39950 +FS_24 LPC.Fl_O 126.63 26.038 677.71 162.18 0.0000 81.69 23.098 655.01 366.0 0.4176 1.39679 +FS_25 Duct2.Fl_O 126.63 25.972 677.71 162.18 0.0000 81.90 23.040 655.01 366.9 0.4176 1.39679 +FS_3 HPC.Fl_O 126.63 132.218 1128.28 273.12 0.0000 20.76 123.731 1108.12 119.9 0.3121 1.37266 +FS_36 Bld3.Fl_O 115.23 132.218 1128.28 273.12 0.0000 18.89 123.731 1108.12 109.1 0.3121 1.37266 +FS_4 Burner.Fl_O 116.89 124.946 2055.53 528.91 0.0144 27.37 124.143 2052.35 483.4 0.0990 1.31599 +FS_45 HPT.Fl_O 128.28 45.064 1583.98 396.68 0.0131 73.11 42.401 1559.83 439.1 0.3029 1.33676 +FS_48 Duct3.Fl_O 128.28 44.839 1583.98 396.68 0.0131 73.48 42.189 1559.83 441.4 0.3029 1.33676 +FS_5 LPT.Fl_O 128.28 14.221 1214.47 298.34 0.0131 202.86 13.663 1201.70 1477.4 0.2434 1.35815 +FS_7 Duct4.Fl_O 128.28 14.079 1214.47 298.34 0.0131 204.91 13.783 1207.69 2018.9 0.1770 1.35815 +FS_9 Core_Nozz.Fl_O 128.28 14.079 1214.47 298.34 0.0131 204.91 12.228 1170.09 862.9 0.4590 1.35815 +FS_15 BypBld.Fl_O 783.19 15.655 571.91 136.73 0.0000 772.04 14.225 556.49 3795.6 0.3724 1.39950 +FS_17 Duct5.Fl_O 783.19 15.537 571.91 136.73 0.0000 777.88 14.118 556.49 3824.3 0.3724 1.39950 +FS_19 Byp_Nozz.Fl_O 783.19 15.537 571.91 136.73 0.0000 777.88 12.228 534.07 2706.4 0.5952 1.39950 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1104.24 1.280 0.8996 2649.483 1.0813 0.9031 -13288.8 35.62 13.42 +LPC 125.14 1.667 0.8477 2547.889 1.1850 0.8583 -4560.7 32.19 14.84 +HPC 81.90 5.091 0.8644 6246.118 1.6649 0.8907 -19875.9 28.48 28.64 +HPT 27.37 2.773 0.9153 157.479 1.2535 0.9050 19875.9 +LPT 73.48 3.153 0.9106 67.224 1.3043 0.8972 17849.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2117.23 1.195 0.9294 0.672 1.7395 0.5215 1.4369 0.9679 3943.9586 +LPC 134.23 1.205 0.8830 0.696 1.7079 0.9323 3.2631 0.9600 3662.6571 +HPC 194.71 19.910 0.8527 0.983 2.1800 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.172 0.9337 102.852 5.1721 1.4085 0.4249 0.9803 1.5311 +LPT 152.68 4.003 0.9094 82.879 4.0034 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 18602.09 3185.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 837.71 201.01 41.538 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 837.71 201.01 41.538 +Duct1 0.0025 0.3098 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 837.71 201.01 41.538 +Duct2 0.0025 0.4176 365.99 +Duct3 0.0050 0.3029 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2434 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.4319 1128.28 273.12 132.218 +Duct5 0.0075 0.3724 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.9644 1128.28 273.12 132.218 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 571.91 136.73 15.655 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.1851 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7139.8 14621.0 19875.9 +LP_Shaft 2675.5 35039.3 17849.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2055.53 0.9940 0.0550 1.65899 0.01440 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.271 0.9975 1.0000 0.9975 2706.36 0.595 672.7 16373.9 +Core_Nozz 1.151 0.9999 1.0000 0.9999 862.88 0.459 758.8 3025.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 96 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 5000.0 27.00 674.26 8106.8 0.3946 3199.08 6.3734 112.64 7.054 1709.9 1671.6 1306.0 + core size:21.41 Q: 12.33 Maximum Thrust: 40535.7 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 674.26 12.313 528.90 126.40 0.0000 812.62 12.228 527.84 13785.9 0.1000 1.40033 +FS_2 Inlet.Fl_O 674.26 12.227 528.90 126.40 0.0000 818.35 11.745 522.85 5943.4 0.2403 1.40033 +FS_21 Fan.Fl_O 674.26 14.090 553.28 132.25 0.0000 726.33 13.319 544.45 4515.2 0.2847 1.39984 +FS_13 Splitter.Fl_O2 582.82 14.090 553.28 132.25 0.0000 627.82 13.272 543.90 3795.6 0.2936 1.39984 +FS_22 Splitter.Fl_O1 91.44 14.090 553.28 132.25 0.0000 98.51 13.542 547.04 719.5 0.2389 1.39984 +FS_23 Duct1.Fl_O 91.44 14.055 553.28 132.25 0.0000 98.75 13.508 547.04 721.3 0.2389 1.39984 +FS_24 LPC.Fl_O 91.44 19.011 613.17 146.64 0.0000 76.86 17.145 595.37 366.0 0.3871 1.39881 +FS_25 Duct2.Fl_O 91.44 18.963 613.17 146.64 0.0000 77.05 17.102 595.37 366.9 0.3871 1.39881 +FS_3 HPC.Fl_O 91.44 86.864 993.35 239.33 0.0000 21.41 80.905 974.04 119.9 0.3222 1.38113 +FS_36 Bld3.Fl_O 83.21 86.864 993.35 239.33 0.0000 19.48 80.905 974.04 109.1 0.3222 1.38113 +FS_4 Burner.Fl_O 84.10 82.087 1709.94 430.11 0.0107 27.34 81.560 1707.20 483.4 0.0983 1.33236 +FS_45 HPT.Fl_O 92.33 29.283 1305.96 321.30 0.0097 73.53 27.532 1285.02 439.1 0.3027 1.35468 +FS_48 Duct3.Fl_O 92.33 29.136 1305.96 321.30 0.0097 73.90 27.395 1285.02 441.4 0.3027 1.35468 +FS_5 LPT.Fl_O 92.33 13.206 1085.26 264.33 0.0097 148.62 12.934 1079.19 1477.4 0.1747 1.36868 +FS_7 Duct4.Fl_O 92.33 13.074 1085.26 264.33 0.0097 150.13 12.929 1081.99 2018.9 0.1281 1.36868 +FS_9 Core_Nozz.Fl_O 92.33 13.074 1085.26 264.33 0.0097 150.13 12.228 1065.81 862.9 0.3143 1.36868 +FS_15 BypBld.Fl_O 582.82 14.090 553.28 132.25 0.0000 627.82 13.272 543.90 3795.6 0.2936 1.39984 +FS_17 Duct5.Fl_O 582.82 13.985 553.28 132.25 0.0000 632.56 13.172 543.90 3824.3 0.2936 1.39984 +FS_19 Byp_Nozz.Fl_O 582.82 13.985 553.28 132.25 0.0000 632.56 12.228 532.45 2706.4 0.4422 1.39984 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 818.35 1.152 0.8974 1996.590 1.0461 0.8995 -5580.9 37.94 8.55 +LPC 98.75 1.353 0.8318 1952.094 1.1082 0.8388 -1861.4 43.56 12.78 +HPC 77.05 4.581 0.8625 6159.718 1.6200 0.8879 -11992.6 36.44 36.86 +HPT 27.34 2.803 0.9163 161.963 1.2684 0.9055 11993.6 +LPT 73.90 2.206 0.8915 55.791 1.2034 0.8809 7441.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1569.07 1.106 0.9271 0.506 1.6906 0.5215 1.4369 0.9679 3943.9586 +LPC 105.93 1.108 0.8665 0.533 1.8449 0.9323 3.2631 0.9600 3662.6571 +HPC 183.18 17.553 0.8509 0.969 2.2344 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.244 0.9347 105.781 5.2441 1.4085 0.4249 0.9803 1.5311 +LPT 153.55 2.683 0.8903 68.783 2.6826 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 13785.92 2360.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 747.58 179.08 28.911 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 747.58 179.08 28.911 +Duct1 0.0025 0.2389 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 747.58 179.08 28.911 +Duct2 0.0025 0.3871 365.99 +Duct3 0.0050 0.3027 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1747 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.2006 993.35 239.33 86.864 +Duct5 0.0075 0.2936 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.0295 993.35 239.33 86.864 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 553.28 132.25 14.090 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.3734 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6697.4 9405.4 11993.6 +LP_Shaft 2016.2 19385.1 7441.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1709.94 0.9940 0.0550 0.88863 0.01068 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.144 0.9975 1.0000 0.9975 2706.36 0.442 499.0 9039.6 +Core_Nozz 1.069 0.9999 1.0000 0.9999 862.88 0.314 497.5 1427.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 97 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 2/ 12/ 1/ 0 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 5000.0 27.00 1377.13 37082.8 0.4406 16338.78 5.1717 225.28 21.496 2730.0 2661.1 2139.8 + core size:19.87 Q: 49.31 Maximum Thrust: 37082.8 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1377.13 12.573 532.07 127.16 0.0000 1630.26 12.228 527.84 14078.4 0.2000 1.40027 +FS_2 Inlet.Fl_O 1377.13 12.498 532.07 127.16 0.0000 1640.11 10.117 500.86 5943.4 0.5577 1.40027 +FS_21 Fan.Fl_O 1377.13 20.402 621.61 148.67 0.0000 1085.95 17.656 596.50 4515.2 0.4593 1.39863 +FS_13 Splitter.Fl_O2 1154.00 20.402 621.61 148.67 0.0000 909.99 17.677 596.70 3795.6 0.4574 1.39863 +FS_22 Splitter.Fl_O1 223.14 20.402 621.61 148.67 0.0000 175.96 17.543 595.42 719.5 0.4696 1.39863 +FS_23 Duct1.Fl_O 223.14 20.351 621.61 148.67 0.0000 176.40 17.499 595.42 721.3 0.4696 1.39863 +FS_24 LPC.Fl_O 223.14 47.708 817.32 196.04 0.0000 86.28 41.580 786.29 366.0 0.4487 1.39112 +FS_25 Duct2.Fl_O 223.14 47.589 817.32 196.04 0.0000 86.50 41.476 786.29 366.9 0.4487 1.39112 +FS_3 HPC.Fl_O 223.14 270.283 1391.69 340.74 0.0000 19.87 254.474 1369.79 119.9 0.2991 1.35638 +FS_36 Bld3.Fl_O 203.05 270.283 1391.69 340.74 0.0000 18.08 254.474 1369.79 109.1 0.2991 1.35638 +FS_4 Burner.Fl_O 207.59 255.417 2729.99 733.27 0.0224 27.40 253.771 2725.98 483.4 0.1000 1.29371 +FS_45 HPT.Fl_O 227.68 95.158 2139.83 556.83 0.0203 71.42 89.802 2110.72 439.1 0.2984 1.30926 +FS_48 Duct3.Fl_O 227.68 94.682 2139.83 556.83 0.0203 71.78 89.353 2110.72 441.4 0.2984 1.30926 +FS_5 LPT.Fl_O 227.68 20.072 1513.96 380.32 0.0203 284.80 18.438 1481.94 1477.4 0.3583 1.33556 +FS_7 Duct4.Fl_O 227.68 19.871 1513.96 380.32 0.0203 287.67 19.028 1497.54 2018.9 0.2555 1.33556 +FS_9 Core_Nozz.Fl_O 227.68 19.871 1513.96 380.32 0.0203 287.67 12.228 1338.35 862.9 0.8762 1.33556 +FS_15 BypBld.Fl_O 1154.00 20.402 621.61 148.67 0.0000 909.99 17.677 596.70 3795.6 0.4574 1.39863 +FS_17 Duct5.Fl_O 1154.00 20.249 621.61 148.67 0.0000 916.87 17.544 596.70 3824.3 0.4574 1.39863 +FS_19 Byp_Nozz.Fl_O 1154.00 20.249 621.61 148.67 0.0000 916.87 12.228 538.24 2706.4 0.8804 1.39863 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1640.11 1.632 0.8924 3782.291 1.1683 0.8996 -41903.2 26.23 16.62 +LPC 176.40 2.344 0.8672 3499.279 1.3148 0.8820 -14953.7 29.57 23.04 +HPC 86.50 5.680 0.8632 6351.352 1.7027 0.8906 -45683.4 19.70 19.68 +HPT 27.40 2.684 0.9140 152.594 1.2284 0.9046 45683.1 +LPT 71.78 4.717 0.9300 82.814 1.4134 0.9161 56857.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3144.68 1.440 0.9220 0.959 2.1306 0.5215 1.4369 0.9679 3943.9586 +LPC 189.22 1.412 0.9033 0.955 1.7740 0.9323 3.2631 0.9600 3662.6571 +HPC 205.64 22.632 0.8516 0.999 2.0610 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.964 0.9324 99.662 4.9638 1.4085 0.4249 0.9803 1.5311 +LPT 149.15 6.185 0.9288 102.099 6.1853 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 14078.40 9642.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1022.88 246.68 80.214 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1022.88 246.68 80.214 +Duct1 0.0025 0.4696 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1022.88 246.68 80.214 +Duct2 0.0025 0.4487 365.99 +Duct3 0.0050 0.2984 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3583 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.8098 1391.69 340.74 270.283 +Duct5 0.0075 0.4574 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.2725 1391.69 340.74 270.283 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 621.61 148.67 20.402 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.1717 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7972.9 30093.5 45683.1 +LP_Shaft 3830.8 77952.9 56857.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2729.99 0.9940 0.0550 4.53855 0.02235 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.656 0.9975 1.0000 0.9975 2706.36 0.880 998.8 35825.5 +Core_Nozz 1.625 0.9999 1.0000 0.9999 862.88 0.876 1540.3 10899.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 98 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 5000.0 27.00 1323.53 33374.3 0.4298 14345.69 5.3666 225.28 19.628 2627.9 2562.0 2053.8 + core size:20.00 Q: 49.31 Maximum Thrust: 37082.8 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1323.53 12.573 532.07 127.16 0.0000 1566.80 12.228 527.84 13530.4 0.2000 1.40027 +FS_2 Inlet.Fl_O 1323.53 12.498 532.07 127.16 0.0000 1576.27 10.353 504.18 5943.4 0.5255 1.40027 +FS_21 Fan.Fl_O 1323.53 19.757 614.16 146.88 0.0000 1071.28 17.183 590.19 4515.2 0.4512 1.39879 +FS_13 Splitter.Fl_O2 1115.64 19.757 614.16 146.88 0.0000 903.02 17.166 590.02 3795.6 0.4528 1.39879 +FS_22 Splitter.Fl_O1 207.89 19.757 614.16 146.88 0.0000 168.27 17.270 591.04 719.5 0.4428 1.39879 +FS_23 Duct1.Fl_O 207.89 19.708 614.16 146.88 0.0000 168.69 17.227 591.04 721.3 0.4428 1.39879 +FS_24 LPC.Fl_O 207.89 43.960 795.62 190.75 0.0000 86.08 38.346 765.55 366.0 0.4471 1.39216 +FS_25 Duct2.Fl_O 207.89 43.850 795.62 190.75 0.0000 86.29 38.250 765.55 366.9 0.4471 1.39216 +FS_3 HPC.Fl_O 207.89 246.795 1353.49 330.80 0.0000 20.00 232.168 1331.81 119.9 0.3009 1.35865 +FS_36 Bld3.Fl_O 189.18 246.795 1353.49 330.80 0.0000 18.20 232.168 1331.81 109.1 0.3009 1.35865 +FS_4 Burner.Fl_O 193.16 233.222 2627.88 701.40 0.0211 27.40 231.719 2624.00 483.4 0.0999 1.29657 +FS_45 HPT.Fl_O 211.87 86.274 2053.80 531.26 0.0192 71.82 81.361 2025.28 439.1 0.2998 1.31280 +FS_48 Duct3.Fl_O 211.87 85.842 2053.80 531.26 0.0192 72.18 80.954 2025.28 441.4 0.2998 1.31280 +FS_5 LPT.Fl_O 211.87 18.720 1459.27 365.06 0.0192 279.00 17.264 1429.60 1477.4 0.3492 1.33929 +FS_7 Duct4.Fl_O 211.87 18.532 1459.27 365.06 0.0192 281.81 17.779 1444.00 2018.9 0.2495 1.33929 +FS_9 Core_Nozz.Fl_O 211.87 18.532 1459.27 365.06 0.0192 281.81 12.228 1312.10 862.9 0.8067 1.33929 +FS_15 BypBld.Fl_O 1115.64 19.757 614.16 146.88 0.0000 903.02 17.166 590.02 3795.6 0.4528 1.39879 +FS_17 Duct5.Fl_O 1115.64 19.609 614.16 146.88 0.0000 909.84 17.037 590.02 3824.3 0.4528 1.39879 +FS_19 Byp_Nozz.Fl_O 1115.64 19.609 614.16 146.88 0.0000 909.84 12.228 536.68 2706.4 0.8499 1.39879 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1576.27 1.581 0.9055 3614.267 1.1543 0.9113 -36917.8 29.64 16.79 +LPC 168.69 2.231 0.8648 3364.044 1.2955 0.8790 -12903.9 29.59 21.70 +HPC 86.29 5.628 0.8632 6344.800 1.7012 0.8906 -41191.9 20.66 20.67 +HPT 27.40 2.703 0.9145 153.293 1.2325 0.9048 41191.9 +LPT 72.18 4.586 0.9279 80.775 1.4074 0.9136 49821.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3022.22 1.404 0.9354 0.916 2.0069 0.5215 1.4369 0.9679 3943.9586 +LPC 180.94 1.377 0.9008 0.918 1.7540 0.9323 3.2631 0.9600 3662.6571 +HPC 205.15 22.395 0.8515 0.998 2.0892 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.009 0.9328 100.119 5.0088 1.4085 0.4249 0.9803 1.5311 +LPT 149.98 6.002 0.9267 99.586 6.0019 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 13530.40 9267.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 995.10 239.77 73.581 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 995.10 239.77 73.581 +Duct1 0.0025 0.4428 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 995.10 239.77 73.581 +Duct2 0.0025 0.4471 365.99 +Duct3 0.0050 0.2998 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3492 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.2761 1353.49 330.80 246.795 +Duct5 0.0075 0.4528 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.4338 1353.49 330.80 246.795 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 614.16 146.88 19.757 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3666 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7858.3 27530.9 41191.9 +LP_Shaft 3660.6 71482.1 49821.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2627.88 0.9940 0.0550 3.98491 0.02106 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.604 0.9975 1.0000 0.9975 2706.36 0.850 962.9 33387.1 +Core_Nozz 1.516 0.9999 1.0000 0.9999 862.88 0.807 1405.3 9254.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 99 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 5000.0 27.00 1263.71 29666.3 0.4231 12551.09 5.5372 225.28 17.883 2528.1 2465.3 1971.9 + core size:20.13 Q: 49.31 Maximum Thrust: 37082.8 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1263.71 12.573 532.07 127.16 0.0000 1495.99 12.228 527.84 12918.9 0.2000 1.40027 +FS_2 Inlet.Fl_O 1263.71 12.498 532.07 127.16 0.0000 1505.03 10.590 507.45 5943.4 0.4921 1.40027 +FS_21 Fan.Fl_O 1263.71 19.060 606.96 145.15 0.0000 1054.06 16.670 584.20 4515.2 0.4418 1.39893 +FS_13 Splitter.Fl_O2 1070.40 19.060 606.96 145.15 0.0000 892.82 16.627 583.77 3795.6 0.4461 1.39893 +FS_22 Splitter.Fl_O1 193.31 19.060 606.96 145.15 0.0000 161.24 16.889 586.38 719.5 0.4193 1.39893 +FS_23 Duct1.Fl_O 193.31 19.012 606.96 145.15 0.0000 161.64 16.846 586.38 721.3 0.4193 1.39893 +FS_24 LPC.Fl_O 193.31 40.814 777.50 186.34 0.0000 85.22 35.724 748.79 366.0 0.4412 1.39304 +FS_25 Duct2.Fl_O 193.31 40.712 777.50 186.34 0.0000 85.43 35.635 748.79 366.9 0.4412 1.39304 +FS_3 HPC.Fl_O 193.31 224.853 1316.68 321.26 0.0000 20.13 211.337 1295.19 119.9 0.3029 1.36087 +FS_36 Bld3.Fl_O 175.91 224.853 1316.68 321.26 0.0000 18.32 211.337 1295.19 109.1 0.3029 1.36087 +FS_4 Burner.Fl_O 179.40 212.486 2528.12 670.56 0.0198 27.39 211.117 2524.36 483.4 0.0998 1.29962 +FS_45 HPT.Fl_O 196.80 78.317 1971.92 507.15 0.0180 72.00 73.833 1944.14 439.1 0.3002 1.31644 +FS_48 Duct3.Fl_O 196.80 77.925 1971.92 507.15 0.0180 72.37 73.463 1944.14 441.4 0.3002 1.31644 +FS_5 LPT.Fl_O 196.80 17.602 1409.28 351.21 0.0180 270.84 16.320 1382.29 1477.4 0.3370 1.34288 +FS_7 Duct4.Fl_O 196.80 17.426 1409.28 351.21 0.0180 273.57 16.760 1395.33 2018.9 0.2413 1.34288 +FS_9 Core_Nozz.Fl_O 196.80 17.426 1409.28 351.21 0.0180 273.57 12.228 1286.43 862.9 0.7413 1.34288 +FS_15 BypBld.Fl_O 1070.40 19.060 606.96 145.15 0.0000 892.82 16.627 583.77 3795.6 0.4461 1.39893 +FS_17 Duct5.Fl_O 1070.40 18.917 606.96 145.15 0.0000 899.56 16.502 583.77 3824.3 0.4461 1.39893 +FS_19 Byp_Nozz.Fl_O 1070.40 18.917 606.96 145.15 0.0000 899.56 12.228 535.85 2706.4 0.8148 1.39893 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1505.03 1.525 0.9100 3469.770 1.1408 0.9152 -32153.6 33.03 16.89 +LPC 161.64 2.147 0.8619 3248.653 1.2810 0.8757 -11267.1 28.96 20.06 +HPC 85.43 5.523 0.8642 6321.598 1.6935 0.8912 -36900.3 22.07 22.14 +HPT 27.39 2.713 0.9146 153.933 1.2355 0.9047 36900.2 +LPT 72.37 4.427 0.9258 79.139 1.3992 0.9115 43420.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2885.71 1.365 0.9401 0.880 1.9347 0.5215 1.4369 0.9679 3943.9586 +LPC 173.38 1.351 0.8978 0.887 1.7233 0.9323 3.2631 0.9600 3662.6571 +HPC 203.11 21.909 0.8525 0.994 2.1074 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.032 0.9329 100.536 5.0321 1.4085 0.4249 0.9803 1.5311 +LPT 150.37 5.781 0.9246 97.569 5.7807 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 12918.85 8848.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 970.09 233.56 67.688 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 970.09 233.56 67.688 +Duct1 0.0025 0.4193 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 970.09 233.56 67.688 +Duct2 0.0025 0.4412 365.99 +Duct3 0.0050 0.3002 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3370 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.7658 1316.68 321.26 224.853 +Duct5 0.0075 0.4461 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.6320 1316.68 321.26 224.853 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 606.96 145.15 19.060 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5372 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7739.8 25039.9 36900.2 +LP_Shaft 3514.3 64892.3 43420.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2528.12 0.9940 0.0550 3.48641 0.01982 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.547 0.9975 1.0000 0.9975 2706.36 0.815 922.4 30686.7 +Core_Nozz 1.425 0.9999 1.0000 0.9999 862.88 0.741 1279.8 7828.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 100 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 5000.0 27.00 1126.53 22249.7 0.4168 9272.82 5.9090 225.28 14.427 2322.0 2265.3 1802.0 + core size:20.40 Q: 49.31 Maximum Thrust: 37082.8 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1126.53 12.573 532.07 127.16 0.0000 1333.59 12.228 527.84 11516.5 0.2000 1.40027 +FS_2 Inlet.Fl_O 1126.53 12.498 532.07 127.16 0.0000 1341.65 11.050 513.66 5943.4 0.4230 1.40027 +FS_21 Fan.Fl_O 1126.53 17.605 592.26 141.61 0.0000 1004.90 15.631 572.50 4515.2 0.4157 1.39916 +FS_13 Splitter.Fl_O2 963.47 17.605 592.26 141.61 0.0000 859.45 15.550 571.65 3795.6 0.4248 1.39916 +FS_22 Splitter.Fl_O1 163.05 17.605 592.26 141.61 0.0000 145.45 16.019 576.52 719.5 0.3697 1.39916 +FS_23 Duct1.Fl_O 163.05 17.561 592.26 141.61 0.0000 145.81 15.979 576.52 721.3 0.3697 1.39916 +FS_24 LPC.Fl_O 163.05 34.072 735.81 176.23 0.0000 83.77 29.993 709.71 366.0 0.4313 1.39481 +FS_25 Duct2.Fl_O 163.05 33.987 735.81 176.23 0.0000 83.98 29.918 709.71 366.9 0.4313 1.39481 +FS_3 HPC.Fl_O 163.05 181.391 1237.24 300.82 0.0000 20.40 170.170 1216.23 119.9 0.3069 1.36580 +FS_36 Bld3.Fl_O 148.38 181.391 1237.24 300.82 0.0000 18.57 170.170 1216.23 109.1 0.3069 1.36580 +FS_4 Burner.Fl_O 150.95 171.415 2321.98 607.87 0.0174 27.38 170.311 2318.46 483.4 0.0995 1.30625 +FS_45 HPT.Fl_O 165.63 62.559 1802.00 458.01 0.0158 72.52 58.923 1775.71 439.1 0.3016 1.32474 +FS_48 Duct3.Fl_O 165.63 62.246 1802.00 458.01 0.0158 72.89 58.628 1775.71 441.4 0.3016 1.32474 +FS_5 LPT.Fl_O 165.63 15.769 1315.88 325.65 0.0158 245.86 14.839 1295.27 1477.4 0.3012 1.34998 +FS_7 Duct4.Fl_O 165.63 15.612 1315.88 325.65 0.0158 248.34 15.124 1305.10 2018.9 0.2171 1.34998 +FS_9 Core_Nozz.Fl_O 165.63 15.612 1315.88 325.65 0.0158 248.34 12.227 1234.70 862.9 0.6102 1.34998 +FS_15 BypBld.Fl_O 963.47 17.605 592.26 141.61 0.0000 859.45 15.550 571.65 3795.6 0.4248 1.39916 +FS_17 Duct5.Fl_O 963.47 17.473 592.26 141.61 0.0000 865.95 15.434 571.65 3824.3 0.4248 1.39916 +FS_19 Byp_Nozz.Fl_O 963.47 17.473 592.26 141.61 0.0000 865.95 12.228 534.85 2706.4 0.7327 1.39916 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1341.65 1.409 0.9089 3126.613 1.1131 0.9132 -23032.0 37.60 16.37 +LPC 145.81 1.940 0.8558 2963.471 1.2424 0.8685 -7985.8 28.69 17.34 +HPC 83.98 5.337 0.8647 6287.353 1.6815 0.8912 -28743.2 24.78 24.90 +HPT 27.38 2.740 0.9149 155.409 1.2429 0.9049 28743.2 +LPT 72.89 3.947 0.9221 74.599 1.3694 0.9082 31016.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2572.45 1.284 0.9390 0.793 1.8559 0.5215 1.4369 0.9679 3943.9586 +LPC 156.41 1.288 0.8914 0.809 1.6875 0.9323 3.2631 0.9600 3662.6571 +HPC 199.65 21.050 0.8531 0.989 2.1441 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.095 0.9332 101.500 5.0954 1.4085 0.4249 0.9803 1.5311 +LPT 151.46 5.111 0.9209 91.971 5.1114 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 11516.46 7887.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 914.51 219.84 55.581 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 914.51 219.84 55.581 +Duct1 0.0025 0.3697 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 914.51 219.84 55.581 +Duct2 0.0025 0.4313 365.99 +Duct3 0.0050 0.3016 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3012 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.7069 1237.24 300.82 181.391 +Duct5 0.0075 0.4248 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.9679 1237.24 300.82 181.391 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 592.26 141.61 17.605 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9090 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7488.7 20158.8 28743.2 +LP_Shaft 3166.7 51442.1 31016.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2321.98 0.9940 0.0550 2.57578 0.01736 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.429 0.9975 1.0000 0.9975 2706.36 0.733 828.7 24815.6 +Core_Nozz 1.277 0.9999 1.0000 0.9999 862.88 0.610 1033.8 5321.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 101 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 5000.0 27.00 959.30 14832.8 0.4237 6283.96 6.3042 225.28 10.972 2079.2 2029.9 1603.6 + core size:20.75 Q: 49.31 Maximum Thrust: 37082.8 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 959.30 12.573 532.07 127.16 0.0000 1135.63 12.228 527.84 9806.9 0.2000 1.40027 +FS_2 Inlet.Fl_O 959.30 12.498 532.07 127.16 0.0000 1142.49 11.491 519.45 5943.4 0.3483 1.40027 +FS_21 Fan.Fl_O 959.30 16.082 575.96 137.70 0.0000 923.74 14.594 560.21 4515.2 0.3750 1.39943 +FS_13 Splitter.Fl_O2 827.96 16.082 575.96 137.70 0.0000 797.28 14.503 559.21 3795.6 0.3871 1.39943 +FS_22 Splitter.Fl_O1 131.34 16.082 575.96 137.70 0.0000 126.47 15.017 564.80 719.5 0.3144 1.39943 +FS_23 Duct1.Fl_O 131.34 16.042 575.96 137.70 0.0000 126.78 14.980 564.80 721.3 0.3144 1.39943 +FS_24 LPC.Fl_O 131.34 27.234 686.46 164.30 0.0000 81.53 24.173 663.60 366.0 0.4166 1.39648 +FS_25 Duct2.Fl_O 131.34 27.165 686.46 164.30 0.0000 81.74 24.112 663.60 366.9 0.4166 1.39648 +FS_3 HPC.Fl_O 131.34 137.954 1141.35 276.43 0.0000 20.75 129.102 1120.99 119.9 0.3122 1.37184 +FS_36 Bld3.Fl_O 119.52 137.954 1141.35 276.43 0.0000 18.89 129.102 1120.99 109.1 0.3122 1.37184 +FS_4 Burner.Fl_O 121.26 130.367 2079.22 535.81 0.0146 27.37 129.528 2076.01 483.4 0.0991 1.31506 +FS_45 HPT.Fl_O 133.08 47.083 1603.63 402.11 0.0133 73.04 44.307 1579.28 439.1 0.3027 1.33565 +FS_48 Duct3.Fl_O 133.08 46.848 1603.63 402.11 0.0133 73.41 44.085 1579.28 441.4 0.3027 1.33565 +FS_5 LPT.Fl_O 133.08 14.375 1220.39 299.93 0.0133 208.69 13.777 1206.78 1477.4 0.2509 1.35765 +FS_7 Duct4.Fl_O 133.08 14.231 1220.39 299.93 0.0133 210.80 13.915 1213.17 2018.9 0.1823 1.35765 +FS_9 Core_Nozz.Fl_O 133.08 14.231 1220.39 299.93 0.0133 210.80 12.228 1172.48 863.0 0.4767 1.35765 +FS_15 BypBld.Fl_O 827.96 16.082 575.96 137.70 0.0000 797.28 14.503 559.21 3795.6 0.3871 1.39943 +FS_17 Duct5.Fl_O 827.96 15.962 575.96 137.70 0.0000 803.30 14.394 559.21 3824.3 0.3871 1.39943 +FS_19 Byp_Nozz.Fl_O 827.96 15.962 575.96 137.70 0.0000 803.30 12.228 533.73 2706.4 0.6290 1.39943 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1142.49 1.287 0.9057 2696.385 1.0825 0.9090 -14297.7 38.07 14.85 +LPC 126.78 1.698 0.8480 2591.608 1.1919 0.8589 -4942.5 31.05 14.76 +HPC 81.74 5.078 0.8645 6243.237 1.6627 0.8907 -20836.2 28.58 28.75 +HPT 27.37 2.769 0.9153 157.515 1.2524 0.9049 20836.2 +LPT 73.41 3.259 0.9117 68.197 1.3140 0.8981 19239.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2190.57 1.200 0.9357 0.684 1.8020 0.5215 1.4369 0.9679 3943.9586 +LPC 136.00 1.214 0.8833 0.708 1.6902 0.9323 3.2631 0.9600 3662.6571 +HPC 194.32 19.853 0.8528 0.982 2.1777 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.163 0.9337 102.876 5.1632 1.4085 0.4249 0.9803 1.5311 +LPT 152.53 4.151 0.9105 84.079 4.1512 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 9806.89 6716.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 848.07 203.54 43.396 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 848.07 203.54 43.396 +Duct1 0.0025 0.3144 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 848.07 203.54 43.396 +Duct2 0.0025 0.4166 365.99 +Duct3 0.0050 0.3027 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2509 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.5967 1141.35 276.43 137.954 +Duct5 0.0075 0.3871 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.2234 1141.35 276.43 137.954 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 575.96 137.70 16.082 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.3042 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7182.4 15236.4 20836.2 +LP_Shaft 2731.0 37000.7 19239.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2079.22 0.9940 0.0550 1.74554 0.01461 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.305 0.9975 1.0000 0.9975 2706.36 0.629 710.6 18287.5 +Core_Nozz 1.164 0.9999 1.0000 0.9999 862.88 0.477 788.7 3262.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 102 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 5000.0 27.00 739.28 7416.5 0.4678 3469.13 6.6891 225.28 7.344 1746.7 1707.5 1335.6 + core size:21.37 Q: 49.31 Maximum Thrust: 37082.8 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 739.28 12.573 532.07 127.16 0.0000 875.17 12.228 527.84 7557.6 0.2000 1.40027 +FS_2 Inlet.Fl_O 739.28 12.498 532.07 127.16 0.0000 880.45 11.923 524.96 5943.4 0.2601 1.40027 +FS_21 Fan.Fl_O 739.28 14.497 557.51 133.27 0.0000 776.96 13.580 547.20 4515.2 0.3069 1.39976 +FS_13 Splitter.Fl_O2 643.13 14.497 557.51 133.27 0.0000 675.91 13.510 546.39 3795.6 0.3191 1.39976 +FS_22 Splitter.Fl_O1 96.15 14.497 557.51 133.27 0.0000 101.05 13.902 550.87 719.5 0.2455 1.39976 +FS_23 Duct1.Fl_O 96.15 14.461 557.51 133.27 0.0000 101.30 13.867 550.87 721.3 0.2455 1.39976 +FS_24 LPC.Fl_O 96.15 20.094 623.42 149.11 0.0000 77.09 18.109 605.20 366.0 0.3885 1.39859 +FS_25 Duct2.Fl_O 96.15 20.044 623.42 149.11 0.0000 77.28 18.063 605.20 366.9 0.3885 1.39859 +FS_3 HPC.Fl_O 96.15 92.335 1011.08 243.74 0.0000 21.37 86.029 991.55 119.9 0.3216 1.38002 +FS_36 Bld3.Fl_O 87.49 92.335 1011.08 243.74 0.0000 19.44 86.029 991.55 109.1 0.3216 1.38002 +FS_4 Burner.Fl_O 88.46 87.257 1746.73 440.39 0.0110 27.34 86.697 1743.94 483.4 0.0984 1.33045 +FS_45 HPT.Fl_O 97.11 31.168 1335.63 329.17 0.0100 73.48 29.308 1314.34 439.1 0.3027 1.35266 +FS_48 Duct3.Fl_O 97.11 31.013 1335.63 329.17 0.0100 73.85 29.162 1314.34 441.4 0.3027 1.35266 +FS_5 LPT.Fl_O 97.11 13.307 1095.54 267.02 0.0100 155.86 13.005 1088.78 1477.4 0.1836 1.36781 +FS_7 Duct4.Fl_O 97.11 13.174 1095.54 267.02 0.0100 157.44 13.012 1091.90 2018.9 0.1345 1.36781 +FS_9 Core_Nozz.Fl_O 97.11 13.174 1095.54 267.02 0.0100 157.44 12.228 1073.73 862.9 0.3319 1.36781 +FS_15 BypBld.Fl_O 643.13 14.497 557.51 133.27 0.0000 675.91 13.510 546.39 3795.6 0.3191 1.39976 +FS_17 Duct5.Fl_O 643.13 14.389 557.51 133.27 0.0000 681.02 13.408 546.39 3824.3 0.3191 1.39976 +FS_19 Byp_Nozz.Fl_O 643.13 14.389 557.51 133.27 0.0000 681.02 12.228 532.17 2706.4 0.4879 1.39976 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 880.45 1.160 0.9060 2073.898 1.0478 0.9081 -6385.9 42.22 10.74 +LPC 101.30 1.390 0.8326 2026.016 1.1182 0.8401 -2154.4 40.83 12.62 +HPC 77.28 4.607 0.8627 6164.170 1.6218 0.8881 -12873.5 35.97 36.36 +HPT 27.34 2.800 0.9163 161.699 1.2666 0.9055 12873.9 +LPT 73.85 2.331 0.8954 57.475 1.2192 0.8844 8540.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1688.15 1.111 0.9360 0.526 1.7938 0.5215 1.4369 0.9679 3943.9586 +LPC 108.66 1.119 0.8672 0.553 1.8028 0.9323 3.2631 0.9600 3662.6571 +HPC 183.73 17.672 0.8511 0.970 2.2290 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.235 0.9347 105.608 5.2354 1.4085 0.4249 0.9803 1.5311 +LPT 153.44 2.856 0.8942 70.860 2.8560 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 7557.63 5176.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 760.56 182.23 30.635 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 760.56 182.23 30.635 +Duct1 0.0025 0.2455 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 760.56 182.23 30.635 +Duct2 0.0025 0.3885 365.99 +Duct3 0.0050 0.3027 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1836 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.3651 1011.08 243.74 92.335 +Duct5 0.0075 0.3191 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.2881 1011.08 243.74 92.335 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 557.51 133.27 14.497 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6891 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6758.0 10005.1 12873.9 +LP_Shaft 2100.5 21353.4 8540.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1746.73 0.9940 0.0550 0.96365 0.01101 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.177 0.9975 1.0000 0.9975 2706.36 0.488 550.4 11001.8 +Core_Nozz 1.077 0.9999 1.0000 0.9999 862.88 0.332 527.2 1591.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 103 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 2/ 12/ 1/ 0 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 5000.0 27.00 1393.19 35562.4 0.4619 16424.50 5.2028 281.60 21.303 2730.0 2661.2 2139.7 + core size:19.89 Q: 77.05 Maximum Thrust: 35562.4 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1393.19 12.771 534.44 127.73 0.0000 1627.39 12.228 527.84 11394.1 0.2500 1.40022 +FS_2 Inlet.Fl_O 1393.19 12.694 534.44 127.73 0.0000 1637.22 10.288 503.26 5943.4 0.5562 1.40022 +FS_21 Fan.Fl_O 1393.19 20.645 623.57 149.14 0.0000 1087.38 17.857 598.30 4515.2 0.4601 1.39859 +FS_13 Splitter.Fl_O2 1168.59 20.645 623.57 149.14 0.0000 912.08 17.872 598.44 3795.6 0.4588 1.39859 +FS_22 Splitter.Fl_O1 224.61 20.645 623.57 149.14 0.0000 175.31 17.778 597.54 719.5 0.4673 1.39859 +FS_23 Duct1.Fl_O 224.61 20.594 623.57 149.14 0.0000 175.75 17.734 597.54 721.3 0.4673 1.39859 +FS_24 LPC.Fl_O 224.61 48.125 819.11 196.47 0.0000 86.19 41.958 788.10 366.0 0.4481 1.39103 +FS_25 Duct2.Fl_O 224.61 48.004 819.11 196.47 0.0000 86.41 41.853 788.10 366.9 0.4481 1.39103 +FS_3 HPC.Fl_O 224.61 272.065 1393.61 341.24 0.0000 19.89 256.128 1371.65 119.9 0.2994 1.35627 +FS_36 Bld3.Fl_O 204.39 272.065 1393.61 341.24 0.0000 18.10 256.128 1371.65 109.1 0.2994 1.35627 +FS_4 Burner.Fl_O 208.96 257.101 2729.99 733.24 0.0223 27.40 255.444 2725.99 483.4 0.1000 1.29373 +FS_45 HPT.Fl_O 229.17 95.748 2139.72 556.78 0.0203 71.44 90.355 2110.59 439.1 0.2985 1.30928 +FS_48 Duct3.Fl_O 229.17 95.269 2139.72 556.78 0.0203 71.80 89.904 2110.59 441.4 0.2985 1.30928 +FS_5 LPT.Fl_O 229.17 20.179 1513.73 380.25 0.0203 285.13 18.531 1481.63 1477.4 0.3588 1.33559 +FS_7 Duct4.Fl_O 229.17 19.977 1513.73 380.25 0.0203 288.01 19.127 1497.27 2018.9 0.2558 1.33559 +FS_9 Core_Nozz.Fl_O 229.17 19.977 1513.73 380.25 0.0203 288.01 12.228 1336.31 862.9 0.8813 1.33559 +FS_15 BypBld.Fl_O 1168.59 20.645 623.57 149.14 0.0000 912.08 17.872 598.44 3795.6 0.4588 1.39859 +FS_17 Duct5.Fl_O 1168.59 20.491 623.57 149.14 0.0000 918.97 17.738 598.44 3824.3 0.4588 1.39859 +FS_19 Byp_Nozz.Fl_O 1168.59 20.491 623.57 149.14 0.0000 918.97 12.228 538.12 2706.4 0.8915 1.39859 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1637.22 1.626 0.8932 3768.703 1.1668 0.9002 -42197.8 26.70 16.84 +LPC 175.75 2.337 0.8669 3488.990 1.3136 0.8817 -15041.2 29.48 22.86 +HPC 86.41 5.667 0.8633 6348.692 1.7014 0.8907 -46005.1 19.87 19.86 +HPT 27.40 2.685 0.9141 152.697 1.2285 0.9047 46005.0 +LPT 71.80 4.721 0.9298 82.702 1.4135 0.9158 57239.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3139.15 1.436 0.9227 0.956 2.1348 0.5215 1.4369 0.9679 3943.9586 +LPC 188.51 1.410 0.9030 0.953 1.7700 0.9323 3.2631 0.9600 3662.6571 +HPC 205.43 22.577 0.8517 0.999 2.0641 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.966 0.9325 99.729 4.9663 1.4085 0.4249 0.9803 1.5311 +LPT 149.20 6.191 0.9286 101.962 6.1911 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 11394.08 12193.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1024.72 247.14 80.829 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1024.72 247.14 80.829 +Duct1 0.0025 0.4673 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1024.72 247.14 80.829 +Duct2 0.0025 0.4481 365.99 +Duct3 0.0050 0.2985 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3588 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.8613 1393.61 341.24 272.065 +Duct5 0.0075 0.4588 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.3535 1393.61 341.24 272.065 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 623.57 149.14 20.645 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.2028 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7978.3 30285.1 46005.0 +LP_Shaft 3825.6 78583.8 57239.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2729.99 0.9940 0.0550 4.56236 0.02232 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.676 0.9975 1.0000 0.9975 2706.36 0.891 1011.3 36729.4 +Core_Nozz 1.634 0.9999 1.0000 0.9999 862.88 0.881 1548.1 11026.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 104 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 5000.0 27.00 1341.20 32006.0 0.4520 14465.34 5.3934 281.60 19.507 2629.6 2563.8 2055.4 + core size:20.01 Q: 77.05 Maximum Thrust: 35562.4 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1341.20 12.771 534.44 127.73 0.0000 1566.65 12.228 527.84 10968.8 0.2500 1.40022 +FS_2 Inlet.Fl_O 1341.20 12.694 534.44 127.73 0.0000 1576.12 10.517 506.44 5943.4 0.5254 1.40022 +FS_21 Fan.Fl_O 1341.20 20.006 616.32 147.40 0.0000 1073.94 17.384 592.11 4515.2 0.4526 1.39875 +FS_13 Splitter.Fl_O2 1131.42 20.006 616.32 147.40 0.0000 905.96 17.362 591.90 3795.6 0.4547 1.39875 +FS_22 Splitter.Fl_O1 209.78 20.006 616.32 147.40 0.0000 167.98 17.498 593.22 719.5 0.4418 1.39875 +FS_23 Duct1.Fl_O 209.78 19.956 616.32 147.40 0.0000 168.40 17.454 593.22 721.3 0.4418 1.39875 +FS_24 LPC.Fl_O 209.78 44.535 798.55 191.46 0.0000 85.89 38.877 768.53 366.0 0.4459 1.39201 +FS_25 Duct2.Fl_O 209.78 44.424 798.55 191.46 0.0000 86.11 38.779 768.53 366.9 0.4459 1.39201 +FS_3 HPC.Fl_O 209.78 249.126 1356.57 331.60 0.0000 20.01 234.336 1334.81 119.9 0.3012 1.35846 +FS_36 Bld3.Fl_O 190.90 249.126 1356.57 331.60 0.0000 18.21 234.336 1334.81 109.1 0.3012 1.35846 +FS_4 Burner.Fl_O 194.92 235.424 2629.64 701.91 0.0210 27.40 233.907 2625.75 483.4 0.0999 1.29654 +FS_45 HPT.Fl_O 213.80 87.098 2055.40 531.71 0.0192 71.81 82.139 2026.86 439.1 0.2998 1.31275 +FS_48 Duct3.Fl_O 213.80 86.663 2055.40 531.71 0.0192 72.17 81.729 2026.86 441.4 0.2998 1.31275 +FS_5 LPT.Fl_O 213.80 18.843 1459.51 365.12 0.0192 279.71 17.369 1429.66 1477.4 0.3503 1.33928 +FS_7 Duct4.Fl_O 213.80 18.654 1459.51 365.12 0.0192 282.54 17.892 1444.15 2018.9 0.2502 1.33928 +FS_9 Core_Nozz.Fl_O 213.80 18.654 1459.51 365.12 0.0192 282.54 12.228 1310.09 862.9 0.8134 1.33928 +FS_15 BypBld.Fl_O 1131.42 20.006 616.32 147.40 0.0000 905.96 17.362 591.90 3795.6 0.4547 1.39875 +FS_17 Duct5.Fl_O 1131.42 19.856 616.32 147.40 0.0000 912.81 17.232 591.90 3824.3 0.4547 1.39875 +FS_19 Byp_Nozz.Fl_O 1131.42 19.856 616.32 147.40 0.0000 912.81 12.228 536.65 2706.4 0.8619 1.39875 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1576.12 1.576 0.9054 3610.029 1.1532 0.9112 -37313.4 30.10 17.06 +LPC 168.40 2.232 0.8645 3361.696 1.2957 0.8788 -13079.0 29.38 21.50 +HPC 86.11 5.608 0.8634 6339.636 1.6988 0.8908 -41592.4 20.91 20.92 +HPT 27.40 2.703 0.9145 153.399 1.2325 0.9049 41592.4 +LPT 72.17 4.599 0.9278 80.829 1.4083 0.9136 50392.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3021.94 1.401 0.9354 0.915 2.0198 0.5215 1.4369 0.9679 3943.9586 +LPC 180.63 1.377 0.9005 0.918 1.7485 0.9323 3.2631 0.9600 3662.6571 +HPC 204.71 22.301 0.8518 0.997 2.0911 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.008 0.9328 100.188 5.0081 1.4085 0.4249 0.9803 1.5311 +LPT 149.97 6.021 0.9266 99.652 6.0208 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 10968.81 11738.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 998.09 240.51 74.413 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 998.09 240.51 74.413 +Duct1 0.0025 0.4418 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 998.09 240.51 74.413 +Duct2 0.0025 0.4459 365.99 +Duct3 0.0050 0.2998 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3503 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.3422 1356.57 331.60 249.126 +Duct5 0.0075 0.4547 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.5378 1356.57 331.60 249.126 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 616.32 147.40 20.006 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3934 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7866.3 27770.1 41592.4 +LP_Shaft 3664.5 72224.5 50392.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2629.64 0.9940 0.0550 4.01815 0.02105 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.624 0.9975 1.0000 0.9975 2706.36 0.862 976.4 34335.9 +Core_Nozz 1.526 0.9999 1.0000 0.9999 862.88 0.813 1415.9 9408.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 105 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 5000.0 27.00 1283.26 28450.0 0.4460 12688.95 5.5673 281.60 17.810 2531.6 2468.7 1974.9 + core size:20.15 Q: 77.05 Maximum Thrust: 35562.4 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1283.26 12.771 534.44 127.73 0.0000 1498.97 12.228 527.84 10495.0 0.2500 1.40022 +FS_2 Inlet.Fl_O 1283.26 12.694 534.44 127.73 0.0000 1508.03 10.747 509.59 5943.4 0.4935 1.40022 +FS_21 Fan.Fl_O 1283.26 19.317 609.24 145.70 0.0000 1058.06 16.874 586.18 4515.2 0.4439 1.39889 +FS_13 Splitter.Fl_O2 1087.85 19.317 609.24 145.70 0.0000 896.95 16.824 585.69 3795.6 0.4488 1.39889 +FS_22 Splitter.Fl_O1 195.40 19.317 609.24 145.70 0.0000 161.11 17.121 588.62 719.5 0.4189 1.39889 +FS_23 Duct1.Fl_O 195.40 19.269 609.24 145.70 0.0000 161.51 17.078 588.62 721.3 0.4189 1.39889 +FS_24 LPC.Fl_O 195.40 41.437 780.87 187.16 0.0000 85.03 36.297 752.20 366.0 0.4400 1.39287 +FS_25 Duct2.Fl_O 195.40 41.334 780.87 187.16 0.0000 85.24 36.206 752.20 366.9 0.4400 1.39287 +FS_3 HPC.Fl_O 195.40 227.449 1320.51 322.25 0.0000 20.15 213.755 1298.93 119.9 0.3032 1.36064 +FS_36 Bld3.Fl_O 177.82 227.449 1320.51 322.25 0.0000 18.33 213.755 1298.93 109.1 0.3032 1.36064 +FS_4 Burner.Fl_O 181.34 214.939 2531.56 671.59 0.0198 27.39 213.555 2527.79 483.4 0.0998 1.29954 +FS_45 HPT.Fl_O 198.93 79.239 1974.91 508.01 0.0180 71.99 74.704 1947.10 439.1 0.3002 1.31633 +FS_48 Duct3.Fl_O 198.93 78.842 1974.91 508.01 0.0180 72.35 74.330 1947.10 441.4 0.3002 1.31633 +FS_5 LPT.Fl_O 198.93 17.724 1410.02 351.41 0.0180 271.95 16.422 1382.76 1477.4 0.3386 1.34283 +FS_7 Duct4.Fl_O 198.93 17.547 1410.02 351.41 0.0180 274.70 16.871 1395.94 2018.9 0.2424 1.34283 +FS_9 Core_Nozz.Fl_O 198.93 17.547 1410.02 351.41 0.0180 274.70 12.228 1284.81 862.9 0.7488 1.34283 +FS_15 BypBld.Fl_O 1087.85 19.317 609.24 145.70 0.0000 896.95 16.824 585.69 3795.6 0.4488 1.39889 +FS_17 Duct5.Fl_O 1087.85 19.173 609.24 145.70 0.0000 903.73 16.698 585.69 3824.3 0.4488 1.39889 +FS_19 Byp_Nozz.Fl_O 1087.85 19.173 609.24 145.70 0.0000 903.73 12.228 535.80 2706.4 0.8281 1.39889 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1508.03 1.522 0.9102 3469.600 1.1400 0.9154 -32611.1 33.52 17.22 +LPC 161.51 2.150 0.8616 3249.645 1.2817 0.8755 -11463.9 28.73 19.89 +HPC 85.24 5.503 0.8644 6316.847 1.6911 0.8913 -37347.0 22.31 22.42 +HPT 27.39 2.713 0.9146 154.046 1.2354 0.9047 37347.0 +LPT 72.35 4.448 0.9258 79.252 1.4006 0.9114 44075.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2891.46 1.363 0.9403 0.880 1.9516 0.5215 1.4369 0.9679 3943.9586 +LPC 173.25 1.353 0.8975 0.887 1.7177 0.9323 3.2631 0.9600 3662.6571 +HPC 202.66 21.815 0.8527 0.994 2.1088 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.031 0.9330 100.610 5.0307 1.4085 0.4249 0.9803 1.5311 +LPT 150.34 5.810 0.9246 97.708 5.8102 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 10494.97 11231.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 973.64 234.44 68.599 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 973.64 234.44 68.599 +Duct1 0.0025 0.4189 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 973.64 234.44 68.599 +Duct2 0.0025 0.4400 365.99 +Duct3 0.0050 0.3002 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3386 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.8391 1320.51 322.25 227.449 +Duct5 0.0075 0.4488 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.7471 1320.51 322.25 227.449 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 609.24 145.70 19.317 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5673 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7750.8 25307.3 37347.0 +LP_Shaft 3522.0 65726.8 44075.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2531.56 0.9940 0.0550 3.52471 0.01982 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.568 0.9975 1.0000 0.9975 2706.36 0.828 937.4 31693.2 +Core_Nozz 1.435 0.9999 1.0000 0.9999 862.88 0.749 1292.0 7988.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 106 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 5000.0 27.00 1150.44 21337.5 0.4418 9427.01 5.9535 281.60 14.433 2328.3 2271.6 1807.5 + core size:20.42 Q: 77.05 Maximum Thrust: 35562.4 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1150.44 12.771 534.44 127.73 0.0000 1343.83 12.228 527.84 9408.7 0.2500 1.40022 +FS_2 Inlet.Fl_O 1150.44 12.694 534.44 127.73 0.0000 1351.95 11.197 515.61 5943.4 0.4271 1.40022 +FS_21 Fan.Fl_O 1150.44 17.875 594.72 142.21 0.0000 1012.82 15.834 574.50 4515.2 0.4198 1.39912 +FS_13 Splitter.Fl_O2 984.99 17.875 594.72 142.21 0.0000 867.17 15.745 573.57 3795.6 0.4297 1.39912 +FS_22 Splitter.Fl_O1 165.45 17.875 594.72 142.21 0.0000 145.66 16.260 578.87 719.5 0.3704 1.39912 +FS_23 Duct1.Fl_O 165.45 17.830 594.72 142.21 0.0000 146.02 16.219 578.87 721.3 0.3704 1.39912 +FS_24 LPC.Fl_O 165.45 34.765 740.06 177.26 0.0000 83.54 30.629 713.98 366.0 0.4299 1.39465 +FS_25 Duct2.Fl_O 165.45 34.678 740.06 177.26 0.0000 83.75 30.552 713.98 366.9 0.4299 1.39465 +FS_3 HPC.Fl_O 165.45 184.319 1242.42 302.15 0.0000 20.42 172.900 1221.31 119.9 0.3072 1.36548 +FS_36 Bld3.Fl_O 150.56 184.319 1242.42 302.15 0.0000 18.58 172.900 1221.31 109.1 0.3072 1.36548 +FS_4 Burner.Fl_O 153.18 174.181 2328.33 609.75 0.0174 27.38 173.060 2324.81 483.4 0.0995 1.30606 +FS_45 HPT.Fl_O 168.07 63.603 1807.48 459.55 0.0158 72.49 59.910 1781.15 439.1 0.3015 1.32448 +FS_48 Duct3.Fl_O 168.07 63.285 1807.48 459.55 0.0158 72.86 59.610 1781.15 441.4 0.3015 1.32448 +FS_5 LPT.Fl_O 168.07 15.877 1317.13 325.99 0.0158 247.90 14.924 1296.12 1477.4 0.3040 1.34988 +FS_7 Duct4.Fl_O 168.07 15.719 1317.13 325.99 0.0158 250.40 15.219 1306.15 2018.9 0.2190 1.34988 +FS_9 Core_Nozz.Fl_O 168.07 15.719 1317.13 325.99 0.0158 250.40 12.227 1233.68 862.8 0.6189 1.34988 +FS_15 BypBld.Fl_O 984.99 17.875 594.72 142.21 0.0000 867.17 15.745 573.57 3795.6 0.4297 1.39912 +FS_17 Duct5.Fl_O 984.99 17.741 594.72 142.21 0.0000 873.72 15.627 573.57 3824.3 0.4297 1.39912 +FS_19 Byp_Nozz.Fl_O 984.99 17.741 594.72 142.21 0.0000 873.72 12.228 534.74 2706.4 0.7490 1.39912 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1351.95 1.408 0.9105 3135.782 1.1128 0.9148 -23555.6 38.40 16.89 +LPC 146.02 1.950 0.8555 2972.623 1.2444 0.8683 -8205.7 28.34 17.18 +HPC 83.75 5.315 0.8649 6282.584 1.6788 0.8912 -29234.8 25.03 25.15 +HPT 27.38 2.739 0.9149 155.526 1.2427 0.9049 29234.8 +LPT 72.86 3.986 0.9221 74.871 1.3723 0.9082 31760.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2592.19 1.284 0.9407 0.795 1.8802 0.5215 1.4369 0.9679 3943.9586 +LPC 156.63 1.291 0.8911 0.812 1.6799 0.9323 3.2631 0.9600 3662.6571 +HPC 199.11 20.948 0.8532 0.988 2.1442 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.092 0.9333 101.577 5.0919 1.4085 0.4249 0.9803 1.5311 +LPT 151.39 5.165 0.9209 92.307 5.1652 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 9408.73 10069.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 919.12 220.97 56.600 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 919.12 220.97 56.600 +Duct1 0.0025 0.3704 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 919.12 220.97 56.600 +Duct2 0.0025 0.4299 365.99 +Duct3 0.0050 0.3015 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3040 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.7906 1242.42 302.15 184.319 +Duct5 0.0075 0.4297 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.0996 1242.42 302.15 184.319 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 594.72 142.21 17.875 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9535 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7504.6 20460.1 29234.8 +LP_Shaft 3183.1 52404.4 31760.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2328.33 0.9940 0.0550 2.61861 0.01739 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.451 0.9975 1.0000 0.9975 2706.36 0.749 847.0 25931.3 +Core_Nozz 1.285 0.9999 1.0000 0.9999 862.88 0.619 1048.2 5475.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 107 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 5000.0 27.00 988.68 14224.8 0.4526 6437.67 6.3834 281.60 11.041 2089.4 2039.8 1612.1 + core size:20.76 Q: 77.05 Maximum Thrust: 35562.4 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 988.68 12.771 534.44 127.73 0.0000 1154.88 12.228 527.84 8085.8 0.2500 1.40022 +FS_2 Inlet.Fl_O 988.68 12.694 534.44 127.73 0.0000 1161.85 11.633 521.27 5943.4 0.3552 1.40022 +FS_21 Fan.Fl_O 988.68 16.355 578.59 138.33 0.0000 938.33 14.787 562.19 4515.2 0.3822 1.39938 +FS_13 Splitter.Fl_O2 854.78 16.355 578.59 138.33 0.0000 811.24 14.684 561.07 3795.6 0.3954 1.39938 +FS_22 Splitter.Fl_O1 133.91 16.355 578.59 138.33 0.0000 127.09 15.260 567.26 719.5 0.3162 1.39938 +FS_23 Duct1.Fl_O 133.91 16.314 578.59 138.33 0.0000 127.40 15.222 567.26 721.3 0.3162 1.39938 +FS_24 LPC.Fl_O 133.91 27.936 691.56 165.53 0.0000 81.34 24.814 668.67 366.0 0.4154 1.39630 +FS_25 Duct2.Fl_O 133.91 27.866 691.56 165.53 0.0000 81.54 24.752 668.67 366.9 0.4154 1.39630 +FS_3 HPC.Fl_O 133.91 141.010 1148.23 278.17 0.0000 20.76 131.953 1127.75 119.9 0.3124 1.37140 +FS_36 Bld3.Fl_O 121.85 141.010 1148.23 278.17 0.0000 18.90 131.953 1127.75 109.1 0.3124 1.37140 +FS_4 Burner.Fl_O 123.64 133.254 2089.36 538.75 0.0147 27.37 132.398 2086.13 483.4 0.0991 1.31469 +FS_45 HPT.Fl_O 135.69 48.157 1612.12 404.45 0.0134 73.00 45.320 1587.69 439.1 0.3026 1.33518 +FS_48 Duct3.Fl_O 135.69 47.916 1612.12 404.45 0.0134 73.37 45.093 1587.69 441.4 0.3026 1.33518 +FS_5 LPT.Fl_O 135.69 14.460 1222.16 300.40 0.0134 211.69 13.840 1208.11 1477.4 0.2548 1.35749 +FS_7 Duct4.Fl_O 135.69 14.316 1222.16 300.40 0.0134 213.83 13.988 1214.72 2018.9 0.1851 1.35749 +FS_9 Core_Nozz.Fl_O 135.69 14.316 1222.16 300.40 0.0134 213.83 12.228 1172.37 862.9 0.4861 1.35749 +FS_15 BypBld.Fl_O 854.78 16.355 578.59 138.33 0.0000 811.24 14.684 561.07 3795.6 0.3954 1.39938 +FS_17 Duct5.Fl_O 854.78 16.232 578.59 138.33 0.0000 817.37 14.574 561.07 3824.3 0.3954 1.39938 +FS_19 Byp_Nozz.Fl_O 854.78 16.232 578.59 138.33 0.0000 817.37 12.228 533.60 2706.4 0.6493 1.39938 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1161.85 1.288 0.9088 2716.930 1.0826 0.9121 -14823.2 39.55 15.69 +LPC 127.40 1.712 0.8478 2611.216 1.1953 0.8590 -5152.8 30.39 14.64 +HPC 81.54 5.060 0.8645 6239.761 1.6603 0.8907 -21340.3 28.80 28.97 +HPT 27.37 2.767 0.9153 157.628 1.2519 0.9050 21340.3 +LPT 73.37 3.314 0.9123 68.689 1.3191 0.8987 19975.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2227.70 1.201 0.9389 0.689 1.8394 0.5215 1.4369 0.9679 3943.9586 +LPC 136.66 1.218 0.8831 0.713 1.6788 0.9323 3.2631 0.9600 3662.6571 +HPC 193.86 19.770 0.8529 0.982 2.1772 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.159 0.9337 102.949 5.1590 1.4085 0.4249 0.9803 1.5311 +LPT 152.46 4.228 0.9112 84.685 4.2275 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 8085.81 8653.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 853.83 204.95 44.442 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 853.83 204.95 44.442 +Duct1 0.0025 0.3162 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 853.83 204.95 44.442 +Duct2 0.0025 0.4154 365.99 +Duct3 0.0050 0.3026 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2548 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.6867 1148.23 278.17 141.010 +Duct5 0.0075 0.3954 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.3648 1148.23 278.17 141.010 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 578.59 138.33 16.355 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.3834 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7205.1 15555.9 21340.3 +LP_Shaft 2757.9 38040.5 19975.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2089.36 0.9940 0.0550 1.78824 0.01468 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.327 0.9975 1.0000 0.9975 2706.36 0.649 733.5 19486.6 +Core_Nozz 1.171 0.9999 1.0000 0.9999 862.88 0.486 804.2 3391.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 108 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 5000.0 27.00 776.82 7112.4 0.5070 3605.91 6.8699 281.60 7.459 1763.4 1723.8 1349.2 + core size:21.36 Q: 77.05 Maximum Thrust: 35562.4 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 776.82 12.771 534.44 127.73 0.0000 907.40 12.228 527.84 6353.1 0.2500 1.40022 +FS_2 Inlet.Fl_O 776.82 12.694 534.44 127.73 0.0000 912.89 12.064 526.72 5943.4 0.2706 1.40022 +FS_21 Fan.Fl_O 776.82 14.756 560.27 133.93 0.0000 804.07 13.751 549.10 4515.2 0.3191 1.39971 +FS_13 Splitter.Fl_O2 678.11 14.756 560.27 133.93 0.0000 701.90 13.665 548.11 3795.6 0.3331 1.39971 +FS_22 Splitter.Fl_O1 98.71 14.756 560.27 133.93 0.0000 102.17 14.136 553.44 719.5 0.2485 1.39971 +FS_23 Duct1.Fl_O 98.71 14.719 560.27 133.93 0.0000 102.43 14.101 553.44 721.3 0.2485 1.39971 +FS_24 LPC.Fl_O 98.71 20.730 629.27 150.51 0.0000 77.07 18.683 610.89 366.0 0.3885 1.39844 +FS_25 Duct2.Fl_O 98.71 20.679 629.27 150.51 0.0000 77.27 18.636 610.89 366.9 0.3885 1.39844 +FS_3 HPC.Fl_O 98.71 95.259 1020.22 246.02 0.0000 21.36 88.759 1000.56 119.9 0.3215 1.37945 +FS_36 Bld3.Fl_O 89.82 95.259 1020.22 246.02 0.0000 19.43 88.759 1000.56 109.1 0.3215 1.37945 +FS_4 Burner.Fl_O 90.83 90.020 1763.43 445.07 0.0112 27.34 89.443 1760.62 483.4 0.0984 1.32961 +FS_45 HPT.Fl_O 99.71 32.180 1349.22 332.78 0.0101 73.44 30.261 1327.78 439.1 0.3027 1.35175 +FS_48 Duct3.Fl_O 99.71 32.019 1349.22 332.78 0.0101 73.81 30.110 1327.78 441.4 0.3027 1.35175 +FS_5 LPT.Fl_O 99.71 13.363 1099.63 268.08 0.0101 159.66 13.044 1092.50 1477.4 0.1883 1.36747 +FS_7 Duct4.Fl_O 99.71 13.230 1099.63 268.08 0.0101 161.27 13.059 1095.80 2018.9 0.1378 1.36747 +FS_9 Core_Nozz.Fl_O 99.71 13.230 1099.63 268.08 0.0101 161.27 12.228 1076.53 862.9 0.3412 1.36747 +FS_15 BypBld.Fl_O 678.11 14.756 560.27 133.93 0.0000 701.90 13.665 548.11 3795.6 0.3331 1.39971 +FS_17 Duct5.Fl_O 678.11 14.646 560.27 133.93 0.0000 707.21 13.562 548.11 3824.3 0.3331 1.39971 +FS_19 Byp_Nozz.Fl_O 678.11 14.646 560.27 133.93 0.0000 707.21 12.228 532.11 2706.4 0.5144 1.39971 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 912.89 1.162 0.9095 2110.065 1.0483 0.9115 -6812.2 44.80 12.09 +LPC 102.43 1.408 0.8335 2060.850 1.1231 0.8413 -2315.5 39.46 12.49 +HPC 77.27 4.607 0.8627 6163.862 1.6213 0.8882 -13338.2 35.93 36.33 +HPT 27.34 2.797 0.9163 161.676 1.2658 0.9054 13338.4 +LPT 73.81 2.396 0.8964 58.312 1.2270 0.8851 9127.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1750.33 1.113 0.9396 0.535 1.8554 0.5215 1.4369 0.9679 3943.9586 +LPC 109.87 1.125 0.8682 0.563 1.7812 0.9323 3.2631 0.9600 3662.6571 +HPC 183.69 17.673 0.8511 0.970 2.2280 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.230 0.9346 105.593 5.2304 1.4085 0.4249 0.9803 1.5311 +LPT 153.37 2.947 0.8952 71.892 2.9474 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 6353.13 6799.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 767.60 183.94 31.605 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 767.60 183.94 31.605 +Duct1 0.0025 0.2485 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 767.60 183.94 31.605 +Duct2 0.0025 0.3885 365.99 +Duct3 0.0050 0.3027 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1883 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.4548 1020.22 246.02 95.259 +Duct5 0.0075 0.3331 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.4289 1020.22 246.02 95.259 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 560.27 133.93 14.756 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.8699 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6789.3 10318.5 13338.4 +LP_Shaft 2141.9 22381.1 9127.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1763.43 0.9940 0.0550 1.00164 0.01115 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.198 0.9975 1.0000 0.9975 2706.36 0.514 580.3 12229.7 +Core_Nozz 1.082 0.9999 1.0000 0.9999 862.88 0.341 542.7 1681.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 109 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 2/ 12/ 1/ 0 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 5000.0 27.00 1412.80 34190.3 0.4834 16529.25 5.2399 337.92 21.071 2730.0 2661.3 2139.6 + core size:19.90 Q: 110.96 Maximum Thrust: 34190.3 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1412.80 13.015 537.35 128.43 0.0000 1623.69 12.228 527.84 9628.7 0.3000 1.40016 +FS_2 Inlet.Fl_O 1412.80 12.937 537.35 128.43 0.0000 1633.50 10.499 506.20 5943.4 0.5542 1.40016 +FS_21 Fan.Fl_O 1412.80 20.948 625.98 149.72 0.0000 1088.84 18.110 600.53 4515.2 0.4610 1.39853 +FS_13 Splitter.Fl_O2 1186.39 20.948 625.98 149.72 0.0000 914.34 18.117 600.60 3795.6 0.4603 1.39853 +FS_22 Splitter.Fl_O1 226.41 20.948 625.98 149.72 0.0000 174.50 18.071 600.16 719.5 0.4644 1.39853 +FS_23 Duct1.Fl_O 226.41 20.896 625.98 149.72 0.0000 174.93 18.026 600.16 721.3 0.4644 1.39853 +FS_24 LPC.Fl_O 226.41 48.634 821.27 197.00 0.0000 86.09 42.420 790.27 366.0 0.4474 1.39093 +FS_25 Duct2.Fl_O 226.41 48.513 821.27 197.00 0.0000 86.31 42.314 790.27 366.9 0.4474 1.39093 +FS_3 HPC.Fl_O 226.41 274.253 1395.93 341.85 0.0000 19.90 258.160 1373.91 119.9 0.2997 1.35613 +FS_36 Bld3.Fl_O 206.04 274.253 1395.93 341.85 0.0000 18.11 258.160 1373.91 109.1 0.2997 1.35613 +FS_4 Burner.Fl_O 210.63 259.169 2729.99 733.21 0.0223 27.40 257.499 2725.98 483.4 0.1000 1.29375 +FS_45 HPT.Fl_O 231.00 96.470 2139.57 556.72 0.0203 71.47 91.032 2110.41 439.1 0.2986 1.30931 +FS_48 Duct3.Fl_O 231.00 95.987 2139.57 556.72 0.0203 71.83 90.576 2110.41 441.4 0.2986 1.30931 +FS_5 LPT.Fl_O 231.00 20.310 1513.47 380.17 0.0203 285.52 18.647 1481.26 1477.4 0.3593 1.33562 +FS_7 Duct4.Fl_O 231.00 20.107 1513.47 380.17 0.0203 288.41 19.249 1496.95 2018.9 0.2562 1.33562 +FS_9 Core_Nozz.Fl_O 231.00 20.107 1513.47 380.17 0.0203 288.41 12.228 1333.83 862.9 0.8874 1.33562 +FS_15 BypBld.Fl_O 1186.39 20.948 625.98 149.72 0.0000 914.34 18.117 600.60 3795.6 0.4603 1.39853 +FS_17 Duct5.Fl_O 1186.39 20.791 625.98 149.72 0.0000 921.25 17.981 600.60 3824.3 0.4603 1.39853 +FS_19 Byp_Nozz.Fl_O 1186.39 20.791 625.98 149.72 0.0000 921.25 12.228 537.96 2706.4 0.9049 1.39853 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1633.50 1.619 0.8942 3751.872 1.1649 0.9011 -42558.5 27.26 17.08 +LPC 174.93 2.327 0.8666 3476.120 1.3120 0.8814 -15144.8 29.37 22.64 +HPC 86.31 5.653 0.8635 6345.557 1.6997 0.8908 -46400.7 20.06 20.07 +HPT 27.40 2.687 0.9142 152.822 1.2287 0.9048 46400.7 +LPT 71.83 4.726 0.9295 82.559 1.4137 0.9154 57703.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3132.01 1.431 0.9238 0.951 2.1379 0.5215 1.4369 0.9679 3943.9586 +LPC 187.65 1.407 0.9027 0.949 1.7653 0.9323 3.2631 0.9600 3662.6571 +HPC 205.18 22.511 0.8519 0.998 2.0675 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.969 0.9326 99.811 4.9694 1.4085 0.4249 0.9803 1.5311 +LPT 149.26 6.198 0.9283 101.785 6.1977 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 9628.68 14838.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1026.95 247.70 81.584 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1026.95 247.70 81.584 +Duct1 0.0025 0.4644 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1026.95 247.70 81.584 +Duct2 0.0025 0.4474 365.99 +Duct3 0.0050 0.2986 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3593 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.9245 1395.93 341.85 274.253 +Duct5 0.0075 0.4603 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.4527 1395.93 341.85 274.253 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 625.98 149.72 20.948 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.2399 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7984.9 30520.5 46400.7 +LP_Shaft 3818.8 79361.3 57703.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2729.99 0.9940 0.0550 4.59146 0.02228 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.700 0.9975 1.0000 0.9975 2706.36 0.905 1026.4 37845.7 +Core_Nozz 1.644 0.9999 1.0000 0.9999 862.88 0.887 1557.6 11183.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 110 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 5000.0 27.00 1362.30 30772.0 0.4745 14602.40 5.4254 337.92 19.351 2631.3 2565.6 2057.0 + core size:20.03 Q: 110.96 Maximum Thrust: 34190.3 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1362.30 13.015 537.35 128.43 0.0000 1565.66 12.228 527.84 9284.5 0.3000 1.40016 +FS_2 Inlet.Fl_O 1362.30 12.937 537.35 128.43 0.0000 1575.12 10.721 509.25 5943.4 0.5249 1.40016 +FS_21 Fan.Fl_O 1362.30 20.313 618.94 148.03 0.0000 1076.67 17.634 594.48 4515.2 0.4542 1.39869 +FS_13 Splitter.Fl_O2 1150.28 20.313 618.94 148.03 0.0000 909.10 17.605 594.20 3795.6 0.4568 1.39869 +FS_22 Splitter.Fl_O1 212.02 20.313 618.94 148.03 0.0000 167.57 17.781 595.88 719.5 0.4404 1.39869 +FS_23 Duct1.Fl_O 212.02 20.262 618.94 148.03 0.0000 167.99 17.736 595.88 721.3 0.4404 1.39869 +FS_24 LPC.Fl_O 212.02 45.229 802.05 192.31 0.0000 85.67 39.519 772.11 366.0 0.4444 1.39185 +FS_25 Duct2.Fl_O 212.02 45.116 802.05 192.31 0.0000 85.88 39.420 772.11 366.9 0.4444 1.39185 +FS_3 HPC.Fl_O 212.02 251.866 1360.16 332.53 0.0000 20.03 236.880 1338.30 119.9 0.3016 1.35825 +FS_36 Bld3.Fl_O 192.94 251.866 1360.16 332.53 0.0000 18.23 236.880 1338.30 109.1 0.3016 1.35825 +FS_4 Burner.Fl_O 196.99 238.013 2631.31 702.39 0.0210 27.40 236.480 2627.42 483.4 0.0999 1.29653 +FS_45 HPT.Fl_O 216.08 88.068 2056.96 532.14 0.0191 71.81 83.054 2028.40 439.1 0.2997 1.31272 +FS_48 Duct3.Fl_O 216.08 87.627 2056.96 532.14 0.0191 72.17 82.639 2028.40 441.4 0.2997 1.31272 +FS_5 LPT.Fl_O 216.08 18.989 1459.60 365.13 0.0191 280.53 17.494 1429.54 1477.4 0.3515 1.33929 +FS_7 Duct4.Fl_O 216.08 18.799 1459.60 365.13 0.0191 283.36 18.026 1444.14 2018.9 0.2510 1.33929 +FS_9 Core_Nozz.Fl_O 216.08 18.799 1459.60 365.13 0.0191 283.36 12.228 1307.56 862.9 0.8211 1.33929 +FS_15 BypBld.Fl_O 1150.28 20.313 618.94 148.03 0.0000 909.10 17.605 594.20 3795.6 0.4568 1.39869 +FS_17 Duct5.Fl_O 1150.28 20.160 618.94 148.03 0.0000 915.97 17.473 594.20 3824.3 0.4568 1.39869 +FS_19 Byp_Nozz.Fl_O 1150.28 20.160 618.94 148.03 0.0000 915.97 12.228 536.60 2706.3 0.8763 1.39869 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1575.12 1.570 0.9053 3603.990 1.1518 0.9111 -37773.9 30.65 17.37 +LPC 167.99 2.232 0.8642 3358.041 1.2958 0.8785 -13284.8 29.13 21.26 +HPC 85.88 5.583 0.8638 6333.376 1.6959 0.8910 -42060.8 21.21 21.24 +HPT 27.40 2.703 0.9145 153.534 1.2324 0.9049 42061.2 +LPT 72.17 4.615 0.9278 80.882 1.4093 0.9135 51057.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3020.30 1.397 0.9353 0.914 2.0332 0.5215 1.4369 0.9679 3943.9586 +LPC 180.19 1.378 0.9002 0.917 1.7417 0.9323 3.2631 0.9600 3662.6571 +HPC 204.17 22.184 0.8521 0.996 2.0936 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.007 0.9329 100.276 5.0073 1.4085 0.4249 0.9803 1.5311 +LPT 149.95 6.042 0.9266 99.718 6.0424 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 9284.53 14308.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1001.63 241.39 75.405 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1001.63 241.39 75.405 +Duct1 0.0025 0.4404 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1001.63 241.39 75.405 +Duct2 0.0025 0.4444 365.99 +Duct3 0.0050 0.2997 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3515 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.4207 1360.16 332.53 251.866 +Duct5 0.0075 0.4568 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.6611 1360.16 332.53 251.866 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 618.94 148.03 20.313 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.4254 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7875.7 28049.5 42061.2 +LP_Shaft 3668.3 73102.2 51057.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2631.31 0.9940 0.0550 4.05622 0.02102 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.649 0.9975 1.0000 0.9975 2706.36 0.876 992.7 35488.9 +Core_Nozz 1.537 0.9999 1.0000 0.9999 862.88 0.821 1428.1 9591.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 111 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 5000.0 27.00 1306.21 27352.3 0.4694 12840.52 5.6035 337.92 17.702 2534.9 2472.1 1977.8 + core size:20.16 Q: 110.96 Maximum Thrust: 34190.3 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1306.21 13.015 537.35 128.43 0.0000 1501.19 12.228 527.84 8902.2 0.3000 1.40016 +FS_2 Inlet.Fl_O 1306.21 12.937 537.35 128.43 0.0000 1510.26 10.945 512.26 5943.4 0.4945 1.40016 +FS_21 Fan.Fl_O 1306.21 19.630 611.98 146.35 0.0000 1062.23 17.123 588.59 4515.2 0.4462 1.39884 +FS_13 Splitter.Fl_O2 1108.40 19.630 611.98 146.35 0.0000 901.38 17.066 588.03 3795.6 0.4517 1.39884 +FS_22 Splitter.Fl_O1 197.80 19.630 611.98 146.35 0.0000 160.86 17.406 591.35 719.5 0.4181 1.39884 +FS_23 Duct1.Fl_O 197.80 19.581 611.98 146.35 0.0000 161.26 17.362 591.35 721.3 0.4181 1.39884 +FS_24 LPC.Fl_O 197.80 42.167 784.77 188.11 0.0000 84.80 36.970 756.16 366.0 0.4384 1.39268 +FS_25 Duct2.Fl_O 197.80 42.061 784.77 188.11 0.0000 85.01 36.877 756.16 366.9 0.4384 1.39268 +FS_3 HPC.Fl_O 197.80 230.402 1324.81 323.36 0.0000 20.16 216.502 1303.12 119.9 0.3036 1.36038 +FS_36 Bld3.Fl_O 180.00 230.402 1324.81 323.36 0.0000 18.35 216.502 1303.12 109.1 0.3036 1.36038 +FS_4 Burner.Fl_O 183.57 217.730 2534.85 672.56 0.0198 27.39 216.328 2531.08 483.4 0.0998 1.29947 +FS_45 HPT.Fl_O 201.37 80.285 1977.80 508.83 0.0180 71.98 75.691 1949.97 439.1 0.3001 1.31623 +FS_48 Duct3.Fl_O 201.37 79.883 1977.80 508.83 0.0180 72.34 75.313 1949.97 441.4 0.3001 1.31623 +FS_5 LPT.Fl_O 201.37 17.865 1410.58 351.56 0.0180 273.17 16.540 1383.03 1477.4 0.3403 1.34280 +FS_7 Duct4.Fl_O 201.37 17.687 1410.58 351.56 0.0180 275.93 16.999 1396.36 2018.9 0.2436 1.34280 +FS_9 Core_Nozz.Fl_O 201.37 17.687 1410.58 351.56 0.0180 275.93 12.228 1282.68 862.9 0.7573 1.34280 +FS_15 BypBld.Fl_O 1108.40 19.630 611.98 146.35 0.0000 901.38 17.066 588.03 3795.6 0.4517 1.39884 +FS_17 Duct5.Fl_O 1108.40 19.482 611.98 146.35 0.0000 908.19 16.938 588.03 3824.3 0.4517 1.39884 +FS_19 Byp_Nozz.Fl_O 1108.40 19.482 611.98 146.35 0.0000 908.19 12.228 535.76 2706.4 0.8437 1.39884 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1510.26 1.517 0.9103 3467.405 1.1389 0.9154 -33123.1 34.11 17.59 +LPC 161.26 2.154 0.8613 3249.111 1.2823 0.8752 -11685.8 28.45 19.67 +HPC 85.01 5.478 0.8646 6311.145 1.6882 0.8914 -37852.5 22.61 22.70 +HPT 27.39 2.712 0.9146 154.190 1.2353 0.9047 37852.5 +LPT 72.34 4.471 0.9257 79.359 1.4021 0.9113 44808.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2895.74 1.360 0.9404 0.879 1.9696 0.5215 1.4369 0.9679 3943.9586 +LPC 172.98 1.354 0.8971 0.887 1.7107 0.9323 3.2631 0.9600 3662.6571 +HPC 202.10 21.700 0.8530 0.993 2.1106 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.029 0.9330 100.704 5.0293 1.4085 0.4249 0.9803 1.5311 +LPT 150.32 5.842 0.9245 97.840 5.8425 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 8902.21 13718.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 977.70 235.45 69.653 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 977.70 235.45 69.653 +Duct1 0.0025 0.4181 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 977.70 235.45 69.653 +Duct2 0.0025 0.4384 365.99 +Duct3 0.0050 0.3001 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3403 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.9232 1324.81 323.36 230.402 +Duct5 0.0075 0.4517 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.8792 1324.81 323.36 230.402 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 611.98 146.35 19.630 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.6035 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7763.1 25609.2 37852.5 +LP_Shaft 3529.3 66682.5 44808.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2534.85 0.9940 0.0550 3.56681 0.01982 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.593 0.9975 1.0000 0.9975 2706.36 0.844 955.0 32898.8 +Core_Nozz 1.446 0.9999 1.0000 0.9999 862.88 0.757 1305.7 8172.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 112 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 5000.0 27.00 1177.70 20514.4 0.4674 9588.92 6.0062 337.92 14.408 2334.3 2277.6 1812.7 + core size:20.43 Q: 110.96 Maximum Thrust: 34190.3 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1177.70 13.015 537.35 128.43 0.0000 1353.50 12.228 527.84 8026.4 0.3000 1.40016 +FS_2 Inlet.Fl_O 1177.70 12.937 537.35 128.43 0.0000 1361.68 11.386 518.08 5943.4 0.4310 1.40016 +FS_21 Fan.Fl_O 1177.70 18.195 597.63 142.91 0.0000 1021.06 16.078 576.91 4515.2 0.4242 1.39908 +FS_13 Splitter.Fl_O2 1009.61 18.195 597.63 142.91 0.0000 875.33 15.979 575.89 3795.6 0.4348 1.39908 +FS_22 Splitter.Fl_O1 168.09 18.195 597.63 142.91 0.0000 145.74 16.549 581.68 719.5 0.3706 1.39908 +FS_23 Duct1.Fl_O 168.09 18.149 597.63 142.91 0.0000 146.10 16.508 581.68 721.3 0.3706 1.39908 +FS_24 LPC.Fl_O 168.09 35.553 744.85 178.42 0.0000 83.26 31.356 718.82 366.0 0.4281 1.39447 +FS_25 Duct2.Fl_O 168.09 35.464 744.85 178.42 0.0000 83.47 31.278 718.82 366.9 0.4281 1.39447 +FS_3 HPC.Fl_O 168.09 187.520 1248.04 303.59 0.0000 20.43 175.880 1226.80 119.9 0.3076 1.36513 +FS_36 Bld3.Fl_O 152.97 187.520 1248.04 303.59 0.0000 18.60 175.880 1226.80 109.1 0.3076 1.36513 +FS_4 Burner.Fl_O 155.63 177.206 2334.31 611.51 0.0174 27.38 176.066 2330.79 483.4 0.0995 1.30588 +FS_45 HPT.Fl_O 170.76 64.742 1812.67 461.02 0.0158 72.46 60.986 1786.31 439.1 0.3014 1.32425 +FS_48 Duct3.Fl_O 170.76 64.418 1812.67 461.02 0.0158 72.83 60.681 1786.31 441.4 0.3014 1.32425 +FS_5 LPT.Fl_O 170.76 15.997 1318.02 326.23 0.0158 250.06 15.018 1296.59 1477.4 0.3070 1.34982 +FS_7 Duct4.Fl_O 170.76 15.837 1318.02 326.23 0.0158 252.58 15.325 1306.83 2018.9 0.2211 1.34982 +FS_9 Core_Nozz.Fl_O 170.76 15.837 1318.02 326.23 0.0158 252.58 12.227 1232.09 862.8 0.6284 1.34982 +FS_15 BypBld.Fl_O 1009.61 18.195 597.63 142.91 0.0000 875.33 15.979 575.89 3795.6 0.4348 1.39908 +FS_17 Duct5.Fl_O 1009.61 18.058 597.63 142.91 0.0000 881.94 15.859 575.89 3824.3 0.4348 1.39908 +FS_19 Byp_Nozz.Fl_O 1009.61 18.058 597.63 142.91 0.0000 881.94 12.228 534.64 2706.4 0.7677 1.39908 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1361.68 1.406 0.9119 3143.012 1.1122 0.9161 -24119.0 39.29 17.46 +LPC 146.10 1.959 0.8550 2980.276 1.2463 0.8679 -8446.1 27.94 16.97 +HPC 83.47 5.288 0.8650 6276.807 1.6756 0.8913 -29768.9 25.36 25.49 +HPT 27.38 2.737 0.9149 155.685 1.2424 0.9050 29768.8 +LPT 72.83 4.027 0.9221 75.140 1.3753 0.9081 32564.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2610.84 1.283 0.9421 0.797 1.9065 0.5215 1.4369 0.9679 3943.9586 +LPC 156.72 1.294 0.8906 0.814 1.6709 0.9323 3.2631 0.9600 3662.6571 +HPC 198.45 20.821 0.8534 0.987 2.1447 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.089 0.9333 101.681 5.0885 1.4085 0.4249 0.9803 1.5311 +LPT 151.33 5.222 0.9209 92.638 5.2222 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 8026.40 12369.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 924.22 222.23 57.740 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 924.22 222.23 57.740 +Duct1 0.0025 0.3706 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 924.22 222.23 57.740 +Duct2 0.0025 0.4281 365.99 +Duct3 0.0050 0.3014 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3070 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.8833 1248.04 303.59 187.520 +Duct5 0.0075 0.4348 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.2452 1248.04 303.59 187.520 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 597.63 142.91 18.195 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.0062 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7521.9 20785.9 29768.8 +LP_Shaft 3199.1 53462.1 32564.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2334.31 0.9940 0.0550 2.66359 0.01741 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.477 0.9975 1.0000 0.9975 2706.36 0.768 868.0 27238.6 +Core_Nozz 1.295 0.9999 1.0000 0.9999 862.88 0.628 1063.7 5645.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 113 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 5000.0 27.00 1021.42 13676.0 0.4821 6593.84 6.4732 337.92 11.084 2098.7 2049.0 1620.0 + core size:20.78 Q: 110.96 Maximum Thrust: 34190.3 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1021.42 13.015 537.35 128.43 0.0000 1173.89 12.228 527.84 6961.3 0.3000 1.40016 +FS_2 Inlet.Fl_O 1021.42 12.937 537.35 128.43 0.0000 1180.98 11.816 523.60 5943.4 0.3622 1.40016 +FS_21 Fan.Fl_O 1021.42 16.673 581.67 139.07 0.0000 953.39 15.017 564.55 4515.2 0.3896 1.39933 +FS_13 Splitter.Fl_O2 884.74 16.673 581.67 139.07 0.0000 825.82 14.899 563.29 3795.6 0.4041 1.39933 +FS_22 Splitter.Fl_O1 136.68 16.673 581.67 139.07 0.0000 127.57 15.548 570.19 719.5 0.3175 1.39933 +FS_23 Duct1.Fl_O 136.68 16.632 581.67 139.07 0.0000 127.89 15.509 570.19 721.3 0.3175 1.39933 +FS_24 LPC.Fl_O 136.68 28.724 697.21 166.89 0.0000 81.07 25.538 674.32 366.0 0.4137 1.39610 +FS_25 Duct2.Fl_O 136.68 28.652 697.21 166.89 0.0000 81.28 25.474 674.32 366.9 0.4137 1.39610 +FS_3 HPC.Fl_O 136.68 144.264 1155.46 280.00 0.0000 20.78 134.981 1134.83 119.9 0.3127 1.37095 +FS_36 Bld3.Fl_O 124.38 144.264 1155.46 280.00 0.0000 18.91 134.981 1134.83 109.1 0.3127 1.37095 +FS_4 Burner.Fl_O 126.21 136.329 2098.67 541.45 0.0147 27.37 135.453 2095.43 483.4 0.0991 1.31435 +FS_45 HPT.Fl_O 138.51 49.299 1619.98 406.62 0.0134 72.97 46.398 1595.49 439.1 0.3025 1.33477 +FS_48 Duct3.Fl_O 138.51 49.053 1619.98 406.62 0.0134 73.34 46.166 1595.49 441.4 0.3025 1.33477 +FS_5 LPT.Fl_O 138.51 14.552 1223.26 300.70 0.0134 214.81 13.908 1208.75 1477.4 0.2589 1.35739 +FS_7 Duct4.Fl_O 138.51 14.407 1223.26 300.70 0.0134 216.98 14.067 1215.58 2018.9 0.1879 1.35739 +FS_9 Core_Nozz.Fl_O 138.51 14.407 1223.26 300.70 0.0134 216.98 12.228 1171.46 862.9 0.4960 1.35739 +FS_15 BypBld.Fl_O 884.74 16.673 581.67 139.07 0.0000 825.82 14.899 563.29 3795.6 0.4041 1.39933 +FS_17 Duct5.Fl_O 884.74 16.548 581.67 139.07 0.0000 832.06 14.788 563.29 3824.3 0.4041 1.39933 +FS_19 Byp_Nozz.Fl_O 884.74 16.548 581.67 139.07 0.0000 832.06 12.228 533.50 2706.4 0.6720 1.39933 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1180.98 1.289 0.9113 2735.686 1.0825 0.9145 -15376.7 41.13 16.59 +LPC 127.89 1.727 0.8475 2629.387 1.1986 0.8588 -5380.0 29.67 14.45 +HPC 81.28 5.035 0.8645 6235.088 1.6573 0.8906 -21872.3 29.11 29.30 +HPT 27.37 2.765 0.9154 157.800 1.2515 0.9050 21872.4 +LPT 73.34 3.371 0.9130 69.182 1.3243 0.8992 20756.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2264.38 1.201 0.9415 0.694 1.8800 0.5215 1.4369 0.9679 3943.9586 +LPC 137.19 1.223 0.8828 0.718 1.6658 0.9323 3.2631 0.9600 3662.6571 +HPC 193.23 19.653 0.8529 0.981 2.1771 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.155 0.9337 103.062 5.1549 1.4085 0.4249 0.9803 1.5311 +LPT 152.39 4.307 0.9118 85.293 4.3072 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 6961.30 10727.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 860.07 206.48 45.589 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 860.07 206.48 45.589 +Duct1 0.0025 0.3175 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 860.07 206.48 45.589 +Duct2 0.0025 0.4137 365.99 +Duct3 0.0050 0.3025 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2589 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.7837 1155.46 280.00 144.264 +Duct5 0.0075 0.4041 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.5172 1155.46 280.00 144.264 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 581.67 139.07 16.673 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.4732 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7229.0 15891.0 21872.4 +LP_Shaft 2784.5 39150.2 20756.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2098.67 0.9940 0.0550 1.83162 0.01473 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.353 0.9975 1.0000 0.9975 2706.36 0.672 759.1 20872.8 +Core_Nozz 1.178 0.9999 1.0000 0.9999 862.88 0.496 820.2 3531.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 114 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 5000.0 27.00 817.82 6838.0 0.5475 3743.86 7.0606 337.92 7.557 1778.9 1738.9 1361.8 + core size:21.36 Q: 110.96 Maximum Thrust: 34190.3 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 817.82 13.015 537.35 128.43 0.0000 939.90 12.228 527.84 5573.7 0.3000 1.40016 +FS_2 Inlet.Fl_O 817.82 12.937 537.35 128.43 0.0000 945.58 12.245 528.97 5943.4 0.2812 1.40016 +FS_21 Fan.Fl_O 817.82 15.059 563.50 134.71 0.0000 831.86 13.955 551.37 4515.2 0.3317 1.39965 +FS_13 Splitter.Fl_O2 716.36 15.059 563.50 134.71 0.0000 728.66 13.850 550.19 3795.6 0.3479 1.39965 +FS_22 Splitter.Fl_O1 101.46 15.059 563.50 134.71 0.0000 103.20 14.413 556.48 719.5 0.2512 1.39965 +FS_23 Duct1.Fl_O 101.46 15.022 563.50 134.71 0.0000 103.46 14.377 556.48 721.3 0.2512 1.39965 +FS_24 LPC.Fl_O 101.46 21.445 635.69 152.06 0.0000 76.97 19.333 617.19 366.0 0.3879 1.39827 +FS_25 Duct2.Fl_O 101.46 21.391 635.69 152.06 0.0000 77.17 19.284 617.19 366.9 0.3879 1.39827 +FS_3 HPC.Fl_O 101.46 98.356 1029.70 248.38 0.0000 21.36 91.641 1009.86 119.9 0.3216 1.37886 +FS_36 Bld3.Fl_O 92.33 98.356 1029.70 248.38 0.0000 19.44 91.641 1009.86 109.1 0.3216 1.37886 +FS_4 Burner.Fl_O 93.37 92.946 1778.86 449.39 0.0113 27.34 92.350 1776.03 483.4 0.0985 1.32885 +FS_45 HPT.Fl_O 102.50 33.247 1361.82 336.14 0.0103 73.41 31.266 1340.23 439.1 0.3026 1.35091 +FS_48 Duct3.Fl_O 102.50 33.081 1361.82 336.14 0.0103 73.78 31.110 1340.23 441.4 0.3026 1.35091 +FS_5 LPT.Fl_O 102.50 13.424 1102.67 268.88 0.0103 163.61 13.087 1095.16 1477.4 0.1932 1.36721 +FS_7 Duct4.Fl_O 102.50 13.290 1102.67 268.88 0.0103 165.26 13.110 1098.64 2018.9 0.1413 1.36721 +FS_9 Core_Nozz.Fl_O 102.50 13.290 1102.67 268.88 0.0103 165.26 12.228 1078.20 862.9 0.3511 1.36721 +FS_15 BypBld.Fl_O 716.36 15.059 563.50 134.71 0.0000 728.66 13.850 550.19 3795.6 0.3479 1.39965 +FS_17 Duct5.Fl_O 716.36 14.946 563.50 134.71 0.0000 734.17 13.746 550.19 3824.3 0.3479 1.39965 +FS_19 Byp_Nozz.Fl_O 716.36 14.946 563.50 134.71 0.0000 734.17 12.228 532.08 2706.4 0.5434 1.39965 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 945.58 1.164 0.9114 2145.116 1.0487 0.9134 -7262.8 47.53 13.56 +LPC 103.46 1.428 0.8343 2094.740 1.1281 0.8424 -2490.7 38.06 12.32 +HPC 77.17 4.598 0.8628 6161.943 1.6198 0.8882 -13827.1 36.05 36.45 +HPT 27.34 2.796 0.9163 161.743 1.2651 0.9054 13827.3 +LPT 73.78 2.464 0.8974 59.166 1.2350 0.8858 9753.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1813.02 1.114 0.9416 0.544 1.9214 0.5215 1.4369 0.9679 3943.9586 +LPC 110.97 1.131 0.8690 0.572 1.7587 0.9323 3.2631 0.9600 3662.6571 +HPC 183.45 17.633 0.8511 0.969 2.2287 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.226 0.9346 105.637 5.2261 1.4085 0.4249 0.9803 1.5311 +LPT 153.31 3.043 0.8963 72.944 3.0426 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 5573.73 8589.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 775.15 185.77 32.666 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 775.15 185.77 32.666 +Duct1 0.0025 0.2512 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 775.15 185.77 32.666 +Duct2 0.0025 0.3879 365.99 +Duct3 0.0050 0.3026 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1932 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.5511 1029.70 248.38 98.356 +Duct5 0.0075 0.3479 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.5802 1029.70 248.38 98.356 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 563.50 134.71 15.059 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.0606 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6821.7 10645.8 13827.3 +LP_Shaft 2183.4 23461.3 9753.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1778.86 0.9940 0.0550 1.03996 0.01126 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.222 0.9975 1.0000 0.9975 2706.36 0.543 613.0 13647.6 +Core_Nozz 1.087 0.9999 1.0000 0.9999 862.88 0.351 558.7 1779.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 115 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 5000.0 27.00 1463.67 31918.3 0.5271 16823.06 5.3231 450.56 20.538 2730.0 2661.6 2139.4 + core size:19.95 Q: 197.26 Maximum Thrust: 31918.3 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1463.67 13.653 544.74 130.20 0.0000 1614.64 12.228 527.84 7481.6 0.4000 1.40001 +FS_2 Inlet.Fl_O 1463.67 13.584 544.74 130.20 0.0000 1622.77 11.069 513.77 5943.4 0.5487 1.40001 +FS_21 Fan.Fl_O 1463.67 21.762 632.26 151.23 0.0000 1091.28 18.798 606.41 4515.2 0.4623 1.39836 +FS_13 Splitter.Fl_O2 1232.19 21.762 632.26 151.23 0.0000 918.69 18.788 606.32 3795.6 0.4632 1.39836 +FS_22 Splitter.Fl_O1 231.48 21.762 632.26 151.23 0.0000 172.59 18.852 606.91 719.5 0.4577 1.39836 +FS_23 Duct1.Fl_O 231.48 21.708 632.26 151.23 0.0000 173.02 18.805 606.91 721.3 0.4577 1.39836 +FS_24 LPC.Fl_O 231.48 50.109 827.44 198.50 0.0000 85.75 43.767 796.54 366.0 0.4451 1.39064 +FS_25 Duct2.Fl_O 231.48 49.984 827.44 198.50 0.0000 85.96 43.658 796.54 366.9 0.4451 1.39064 +FS_3 HPC.Fl_O 231.48 280.397 1402.34 343.52 0.0000 19.95 263.863 1380.12 119.9 0.3005 1.35576 +FS_36 Bld3.Fl_O 210.65 280.397 1402.34 343.52 0.0000 18.15 263.863 1380.12 109.1 0.3005 1.35576 +FS_4 Burner.Fl_O 215.32 264.976 2730.00 733.12 0.0222 27.40 263.268 2726.00 483.4 0.1000 1.29382 +FS_45 HPT.Fl_O 236.15 98.535 2139.38 556.60 0.0202 71.53 92.971 2110.17 439.1 0.2989 1.30937 +FS_48 Duct3.Fl_O 236.15 98.043 2139.38 556.60 0.0202 71.89 92.506 2110.17 441.4 0.2989 1.30937 +FS_5 LPT.Fl_O 236.15 20.688 1512.76 379.94 0.0202 286.49 18.981 1480.31 1477.4 0.3607 1.33572 +FS_7 Duct4.Fl_O 236.15 20.481 1512.76 379.94 0.0202 289.39 19.601 1496.13 2018.9 0.2571 1.33572 +FS_9 Core_Nozz.Fl_O 236.15 20.481 1512.76 379.94 0.0202 289.39 12.228 1326.86 862.9 0.9047 1.33572 +FS_15 BypBld.Fl_O 1232.19 21.762 632.26 151.23 0.0000 918.69 18.788 606.32 3795.6 0.4632 1.39836 +FS_17 Duct5.Fl_O 1232.19 21.599 632.26 151.23 0.0000 925.64 18.647 606.32 3824.3 0.4632 1.39836 +FS_19 Byp_Nozz.Fl_O 1232.19 21.599 632.26 151.23 0.0000 925.64 12.228 537.49 2706.4 0.9394 1.39836 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1622.77 1.602 0.8960 3713.807 1.1607 0.9027 -43545.4 28.59 17.60 +LPC 173.02 2.308 0.8657 3447.204 1.3087 0.8805 -15482.5 29.02 22.06 +HPC 85.96 5.610 0.8640 6335.854 1.6948 0.8910 -47494.2 20.65 20.67 +HPT 27.40 2.689 0.9144 153.161 1.2291 0.9050 47493.9 +LPT 71.89 4.739 0.9288 82.286 1.4142 0.9146 59027.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3111.44 1.419 0.9257 0.942 2.1387 0.5215 1.4369 0.9679 3943.9586 +LPC 185.59 1.401 0.9018 0.941 1.7518 0.9323 3.2631 0.9600 3662.6571 +HPC 204.36 22.310 0.8523 0.997 2.0763 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 4.976 0.9328 100.032 4.9756 1.4085 0.4249 0.9803 1.5311 +LPT 149.38 6.216 0.9276 101.448 6.2159 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 7481.56 20497.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1033.22 249.26 83.739 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1033.22 249.26 83.739 +Duct1 0.0025 0.4577 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1033.22 249.26 83.739 +Duct2 0.0025 0.4451 365.99 +Duct3 0.0050 0.2989 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3607 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.1019 1402.34 343.52 280.397 +Duct5 0.0075 0.4632 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.7315 1402.34 343.52 280.397 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 632.26 151.23 21.762 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3231 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 8002.6 31170.5 47493.9 +LP_Shaft 3806.0 81455.9 59027.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.00 0.9940 0.0550 4.67307 0.02218 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.766 0.9975 1.0000 0.9975 2706.36 0.939 1065.1 40789.1 +Core_Nozz 1.675 0.9999 1.0000 0.9999 862.88 0.905 1584.0 11626.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:46 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 116 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 5000.0 27.00 1416.09 28726.5 0.5201 14940.33 5.5037 450.56 18.957 2634.4 2568.9 2059.9 + core size:20.08 Q: 197.26 Maximum Thrust: 31918.3 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1416.09 13.653 544.74 130.20 0.0000 1562.15 12.228 527.84 7238.3 0.4000 1.40001 +FS_2 Inlet.Fl_O 1416.09 13.584 544.74 130.20 0.0000 1570.02 11.277 516.51 5943.4 0.5225 1.40001 +FS_21 Fan.Fl_O 1416.09 21.126 625.58 149.62 0.0000 1081.84 18.308 600.55 4515.2 0.4570 1.39854 +FS_13 Splitter.Fl_O2 1198.36 21.126 625.58 149.62 0.0000 915.50 18.262 600.13 3795.6 0.4611 1.39854 +FS_22 Splitter.Fl_O1 217.74 21.126 625.58 149.62 0.0000 166.34 18.538 602.70 719.5 0.4363 1.39854 +FS_23 Duct1.Fl_O 217.74 21.073 625.58 149.62 0.0000 166.76 18.491 602.70 721.3 0.4363 1.39854 +FS_24 LPC.Fl_O 217.74 47.007 810.57 194.39 0.0000 85.10 41.165 780.83 366.0 0.4406 1.39144 +FS_25 Duct2.Fl_O 217.74 46.890 810.57 194.39 0.0000 85.31 41.062 780.83 366.9 0.4406 1.39144 +FS_3 HPC.Fl_O 217.74 258.815 1368.79 334.77 0.0000 20.08 243.331 1346.69 119.9 0.3025 1.35774 +FS_36 Bld3.Fl_O 198.14 258.815 1368.79 334.77 0.0000 18.28 243.331 1346.69 109.1 0.3025 1.35774 +FS_4 Burner.Fl_O 202.29 244.580 2634.38 703.24 0.0209 27.39 243.004 2630.49 483.4 0.0999 1.29652 +FS_45 HPT.Fl_O 221.89 90.509 2059.88 532.94 0.0191 71.80 85.358 2031.30 439.1 0.2997 1.31267 +FS_48 Duct3.Fl_O 221.89 90.057 2059.88 532.94 0.0191 72.16 84.931 2031.30 441.4 0.2997 1.31267 +FS_5 LPT.Fl_O 221.89 19.370 1459.47 365.07 0.0191 282.39 17.823 1428.95 1477.4 0.3542 1.33935 +FS_7 Duct4.Fl_O 221.89 19.176 1459.47 365.07 0.0191 285.24 18.377 1443.79 2018.9 0.2527 1.33935 +FS_9 Core_Nozz.Fl_O 221.89 19.176 1459.47 365.07 0.0191 285.24 12.228 1300.72 862.9 0.8409 1.33935 +FS_15 BypBld.Fl_O 1198.36 21.126 625.58 149.62 0.0000 915.50 18.262 600.13 3795.6 0.4611 1.39854 +FS_17 Duct5.Fl_O 1198.36 20.968 625.58 149.62 0.0000 922.42 18.126 600.13 3824.3 0.4611 1.39854 +FS_19 Byp_Nozz.Fl_O 1198.36 20.968 625.58 149.62 0.0000 922.42 12.228 536.32 2706.4 0.9126 1.39854 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1570.02 1.555 0.9052 3584.851 1.1484 0.9109 -38908.9 31.99 18.02 +LPC 166.76 2.231 0.8632 3345.229 1.2957 0.8776 -13790.7 28.49 20.61 +HPC 85.31 5.520 0.8645 6318.567 1.6887 0.8914 -43246.3 21.97 22.05 +HPT 27.39 2.702 0.9146 153.897 1.2324 0.9050 43246.3 +LPT 72.16 4.649 0.9275 80.947 1.4114 0.9130 52700.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3010.31 1.386 0.9352 0.909 2.0557 0.5215 1.4369 0.9679 3943.9586 +LPC 178.87 1.377 0.8992 0.913 1.7240 0.9323 3.2631 0.9600 3662.6571 +HPC 202.81 21.893 0.8528 0.994 2.0995 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.006 0.9329 100.513 5.0065 1.4085 0.4249 0.9803 1.5311 +LPT 149.94 6.091 0.9263 99.797 6.0906 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 7238.35 19830.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1010.20 243.52 77.937 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1010.20 243.52 77.937 +Duct1 0.0025 0.4363 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1010.20 243.52 77.937 +Duct2 0.0025 0.4406 365.99 +Duct3 0.0050 0.2997 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3542 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.6207 1368.79 334.77 258.815 +Duct5 0.0075 0.4611 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.9754 1368.79 334.77 258.815 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 625.58 149.62 21.126 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5037 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7898.9 28755.1 43246.3 +LP_Shaft 3673.8 75339.7 52700.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2634.38 0.9940 0.0550 4.15009 0.02095 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.715 0.9975 1.0000 0.9975 2706.36 0.913 1033.6 38495.8 +Core_Nozz 1.568 0.9999 1.0000 0.9999 862.88 0.841 1458.9 10061.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 117 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 5000.0 27.00 1363.46 25534.6 0.5168 13196.99 5.6919 450.56 17.405 2541.0 2478.4 1983.3 + core size:20.21 Q: 197.26 Maximum Thrust: 31918.3 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1363.46 13.653 544.74 130.20 0.0000 1504.09 12.228 527.84 6969.3 0.4000 1.40001 +FS_2 Inlet.Fl_O 1363.46 13.584 544.74 130.20 0.0000 1511.67 11.488 519.26 5943.4 0.4951 1.40001 +FS_21 Fan.Fl_O 1363.46 20.449 618.86 148.01 0.0000 1070.36 17.790 594.76 4515.2 0.4507 1.39869 +FS_13 Splitter.Fl_O2 1159.72 20.449 618.86 148.01 0.0000 910.41 17.714 594.04 3795.6 0.4577 1.39869 +FS_22 Splitter.Fl_O1 203.75 20.449 618.86 148.01 0.0000 159.95 18.162 598.29 719.5 0.4152 1.39869 +FS_23 Duct1.Fl_O 203.75 20.398 618.86 148.01 0.0000 160.35 18.117 598.29 721.3 0.4152 1.39869 +FS_24 LPC.Fl_O 203.75 44.003 794.15 190.39 0.0000 84.20 38.669 765.73 366.0 0.4346 1.39223 +FS_25 Duct2.Fl_O 203.75 43.893 794.15 190.39 0.0000 84.41 38.572 765.73 366.9 0.4346 1.39223 +FS_3 HPC.Fl_O 203.75 237.626 1334.85 325.96 0.0000 20.21 223.212 1312.91 119.9 0.3045 1.35977 +FS_36 Bld3.Fl_O 185.41 237.626 1334.85 325.96 0.0000 18.40 223.212 1312.91 109.1 0.3045 1.35977 +FS_4 Burner.Fl_O 189.08 224.556 2541.00 674.35 0.0198 27.39 223.110 2537.22 483.4 0.0997 1.29936 +FS_45 HPT.Fl_O 207.41 82.832 1983.29 510.38 0.0180 71.96 78.096 1955.42 439.1 0.3001 1.31605 +FS_48 Duct3.Fl_O 207.41 82.418 1983.29 510.38 0.0180 72.32 77.705 1955.42 441.4 0.3001 1.31605 +FS_5 LPT.Fl_O 207.41 18.220 1411.15 351.70 0.0180 275.95 16.837 1382.95 1477.4 0.3443 1.34280 +FS_7 Duct4.Fl_O 207.41 18.038 1411.15 351.70 0.0180 278.74 17.321 1396.61 2018.9 0.2462 1.34280 +FS_9 Core_Nozz.Fl_O 207.41 18.038 1411.15 351.70 0.0180 278.74 12.228 1276.67 862.9 0.7781 1.34280 +FS_15 BypBld.Fl_O 1159.72 20.449 618.86 148.01 0.0000 910.41 17.714 594.04 3795.6 0.4577 1.39869 +FS_17 Duct5.Fl_O 1159.72 20.295 618.86 148.01 0.0000 917.29 17.581 594.04 3824.3 0.4577 1.39869 +FS_19 Byp_Nozz.Fl_O 1159.72 20.295 618.86 148.01 0.0000 917.29 12.228 535.51 2706.4 0.8825 1.39869 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1511.67 1.505 0.9102 3456.507 1.1361 0.9152 -34347.8 35.49 18.38 +LPC 160.35 2.157 0.8602 3242.911 1.2832 0.8743 -12217.5 27.75 19.07 +HPC 84.41 5.414 0.8651 6297.224 1.6809 0.8916 -39081.1 23.38 23.49 +HPT 27.39 2.711 0.9147 154.580 1.2352 0.9048 39081.0 +LPT 72.32 4.523 0.9254 79.541 1.4054 0.9109 46565.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2898.43 1.352 0.9403 0.876 2.0052 0.5215 1.4369 0.9679 3943.9586 +LPC 171.99 1.355 0.8960 0.885 1.6926 0.9323 3.2631 0.9600 3662.6571 +HPC 200.68 21.404 0.8534 0.991 2.1154 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.027 0.9330 100.959 5.0270 1.4085 0.4249 0.9803 1.5311 +LPT 150.28 5.915 0.9242 98.065 5.9152 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6969.32 19093.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 987.34 237.84 72.275 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 987.34 237.84 72.275 +Duct1 0.0025 0.4152 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 987.34 237.84 72.275 +Duct2 0.0025 0.4346 365.99 +Duct3 0.0050 0.3001 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3443 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.1311 1334.85 325.96 237.626 +Duct5 0.0075 0.4577 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.2061 1334.85 325.96 237.626 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 618.86 148.01 20.449 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.6919 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7792.1 26341.8 39081.0 +LP_Shaft 3542.3 69041.7 46565.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2541.00 0.9940 0.0550 3.66583 0.01977 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.660 0.9975 1.0000 0.9975 2706.36 0.883 998.7 35998.7 +Core_Nozz 1.475 0.9999 1.0000 0.9999 862.88 0.778 1338.6 8629.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 118 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 5000.0 27.00 1243.18 19151.2 0.5194 9947.29 6.1311 450.56 14.280 2345.4 2288.7 1822.4 + core size:20.49 Q: 197.26 Maximum Thrust: 31918.3 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1243.18 13.653 544.74 130.20 0.0000 1371.41 12.228 527.84 6354.5 0.4000 1.40001 +FS_2 Inlet.Fl_O 1243.18 13.584 544.74 130.20 0.0000 1378.31 11.908 524.61 5943.4 0.4378 1.40001 +FS_21 Fan.Fl_O 1243.18 19.015 604.87 144.64 0.0000 1037.57 16.718 583.06 4515.2 0.4329 1.39897 +FS_13 Splitter.Fl_O2 1068.85 19.015 604.87 144.64 0.0000 892.07 16.593 581.80 3795.6 0.4456 1.39897 +FS_22 Splitter.Fl_O1 174.33 19.015 604.87 144.64 0.0000 145.50 17.301 588.79 719.5 0.3699 1.39897 +FS_23 Duct1.Fl_O 174.33 18.968 604.87 144.64 0.0000 145.86 17.258 588.79 721.3 0.3699 1.39897 +FS_24 LPC.Fl_O 174.33 37.466 756.03 181.13 0.0000 82.56 33.130 730.17 366.0 0.4236 1.39401 +FS_25 Duct2.Fl_O 174.33 37.372 756.03 181.13 0.0000 82.77 33.047 730.17 366.9 0.4236 1.39401 +FS_3 HPC.Fl_O 174.33 194.965 1260.64 306.82 0.0000 20.49 182.796 1239.10 119.9 0.3085 1.36434 +FS_36 Bld3.Fl_O 158.64 194.965 1260.64 306.82 0.0000 18.64 182.796 1239.10 109.1 0.3085 1.36434 +FS_4 Burner.Fl_O 161.41 184.242 2345.42 614.77 0.0174 27.38 183.056 2341.87 483.4 0.0995 1.30558 +FS_45 HPT.Fl_O 177.09 67.379 1822.45 463.76 0.0158 72.40 63.477 1796.01 439.1 0.3012 1.32383 +FS_48 Duct3.Fl_O 177.09 67.042 1822.45 463.76 0.0158 72.77 63.159 1796.01 441.4 0.3012 1.32383 +FS_5 LPT.Fl_O 177.09 16.285 1318.95 326.48 0.0158 254.85 15.247 1296.59 1477.4 0.3136 1.34976 +FS_7 Duct4.Fl_O 177.09 16.122 1318.95 326.48 0.0158 257.42 15.580 1307.30 2018.9 0.2256 1.34976 +FS_9 Core_Nozz.Fl_O 177.09 16.122 1318.95 326.48 0.0158 257.42 12.227 1227.23 862.8 0.6504 1.34976 +FS_15 BypBld.Fl_O 1068.85 19.015 604.87 144.64 0.0000 892.07 16.593 581.80 3795.6 0.4456 1.39897 +FS_17 Duct5.Fl_O 1068.85 18.873 604.87 144.64 0.0000 898.81 16.468 581.80 3824.3 0.4456 1.39897 +FS_19 Byp_Nozz.Fl_O 1068.85 18.873 604.87 144.64 0.0000 898.81 12.228 534.35 2706.4 0.8125 1.39897 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1378.31 1.400 0.9132 3151.327 1.1104 0.9173 -25398.6 41.22 18.68 +LPC 145.86 1.975 0.8537 2990.602 1.2499 0.8668 -8999.4 26.97 16.40 +HPC 82.77 5.217 0.8653 6262.709 1.6674 0.8913 -31002.0 26.22 26.36 +HPT 27.38 2.734 0.9150 156.126 1.2419 0.9051 31001.9 +LPT 72.77 4.117 0.9218 75.651 1.3817 0.9075 34397.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2642.74 1.278 0.9435 0.799 1.9618 0.5215 1.4369 0.9679 3943.9586 +LPC 156.46 1.299 0.8892 0.817 1.6486 0.9323 3.2631 0.9600 3662.6571 +HPC 196.77 20.494 0.8536 0.985 2.1469 0.4206 0.2163 1.0137 6357.1603 +HPT 30.12 5.082 0.9333 101.969 5.0821 1.4085 0.4249 0.9803 1.5311 +LPT 151.21 5.348 0.9206 93.268 5.3478 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6354.52 17409.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 935.95 225.12 60.459 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 935.95 225.12 60.459 +Duct1 0.0025 0.3699 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 935.95 225.12 60.459 +Duct2 0.0025 0.4236 365.99 +Duct3 0.0050 0.3012 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3136 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.1016 1260.64 306.82 194.965 +Duct5 0.0075 0.4456 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.5883 1260.64 306.82 194.965 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 604.87 144.64 19.015 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.1311 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7561.1 21534.6 31001.9 +LP_Shaft 3229.6 55938.8 34397.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2345.42 0.9940 0.0550 2.76314 0.01742 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.543 0.9975 1.0000 0.9975 2706.36 0.813 918.5 30512.6 +Core_Nozz 1.319 0.9999 1.0000 0.9999 862.88 0.650 1098.8 6047.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 119 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 5000.0 27.00 1097.58 12767.2 0.5420 6920.37 6.6761 450.56 11.100 2115.1 2065.4 1634.0 + core size:20.84 Q: 197.26 Maximum Thrust: 31918.3 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1097.58 13.653 544.74 130.20 0.0000 1210.79 12.228 527.84 5610.3 0.4000 1.40001 +FS_2 Inlet.Fl_O 1097.58 13.584 544.74 130.20 0.0000 1216.89 12.325 529.81 5943.4 0.3753 1.40001 +FS_21 Fan.Fl_O 1097.58 17.477 589.25 140.89 0.0000 983.69 15.612 570.57 4515.2 0.4048 1.39921 +FS_13 Splitter.Fl_O2 954.60 17.477 589.25 140.89 0.0000 855.54 15.460 568.97 3795.6 0.4224 1.39921 +FS_22 Splitter.Fl_O1 142.99 17.477 589.25 140.89 0.0000 128.15 16.287 577.50 719.5 0.3192 1.39921 +FS_23 Duct1.Fl_O 142.99 17.434 589.25 140.89 0.0000 128.47 16.246 577.50 721.3 0.3192 1.39921 +FS_24 LPC.Fl_O 142.99 30.606 710.21 170.03 0.0000 80.34 27.281 687.41 366.0 0.4091 1.39567 +FS_25 Duct2.Fl_O 142.99 30.529 710.21 170.03 0.0000 80.54 27.213 687.41 366.9 0.4091 1.39567 +FS_3 HPC.Fl_O 142.99 151.542 1171.10 283.96 0.0000 20.84 141.734 1150.10 119.9 0.3138 1.36996 +FS_36 Bld3.Fl_O 130.12 151.542 1171.10 283.96 0.0000 18.96 141.734 1150.10 109.1 0.3138 1.36996 +FS_4 Burner.Fl_O 132.04 143.207 2115.06 546.18 0.0148 27.36 142.287 2111.81 483.4 0.0991 1.31380 +FS_45 HPT.Fl_O 144.91 51.849 1634.02 410.47 0.0134 72.90 48.803 1609.40 439.1 0.3023 1.33405 +FS_48 Duct3.Fl_O 144.91 51.589 1634.02 410.47 0.0134 73.27 48.559 1609.40 441.4 0.3023 1.33405 +FS_5 LPT.Fl_O 144.91 14.765 1223.51 300.78 0.0134 221.52 14.068 1208.01 1477.4 0.2677 1.35735 +FS_7 Duct4.Fl_O 144.91 14.617 1223.51 300.78 0.0134 223.76 14.250 1215.33 2018.9 0.1940 1.35735 +FS_9 Core_Nozz.Fl_O 144.91 14.617 1223.51 300.78 0.0134 223.76 12.228 1167.22 862.9 0.5179 1.35735 +FS_15 BypBld.Fl_O 954.60 17.477 589.25 140.89 0.0000 855.54 15.460 568.97 3795.6 0.4224 1.39921 +FS_17 Duct5.Fl_O 954.60 17.346 589.25 140.89 0.0000 862.01 15.344 568.97 3824.3 0.4224 1.39921 +FS_19 Byp_Nozz.Fl_O 954.60 17.346 589.25 140.89 0.0000 862.01 12.228 533.23 2706.4 0.7249 1.39921 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1216.89 1.287 0.9134 2767.799 1.0817 0.9165 -16595.2 44.49 18.47 +LPC 128.47 1.756 0.8461 2661.218 1.2053 0.8579 -5895.8 28.09 13.92 +HPC 80.54 4.964 0.8645 6222.539 1.6490 0.8903 -23048.8 30.05 30.25 +HPT 27.36 2.762 0.9155 158.326 1.2508 0.9051 23048.9 +LPT 73.27 3.494 0.9144 70.171 1.3355 0.9003 22490.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2333.22 1.199 0.9437 0.702 1.9655 0.5215 1.4369 0.9679 3943.9586 +LPC 137.81 1.232 0.8814 0.727 1.6352 0.9323 3.2631 0.9600 3662.6571 +HPC 191.48 19.324 0.8528 0.979 2.1780 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.147 0.9338 103.405 5.1471 1.4085 0.4249 0.9803 1.5311 +LPT 152.25 4.479 0.9132 86.512 4.4791 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5610.29 15370.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 874.08 209.91 48.258 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 874.08 209.91 48.258 +Duct1 0.0025 0.3192 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 874.08 209.91 48.258 +Duct2 0.0025 0.4091 365.99 +Duct3 0.0050 0.3023 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2677 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.0046 1171.10 283.96 151.542 +Duct5 0.0075 0.4224 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.8643 1171.10 283.96 151.542 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 589.25 140.89 17.477 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6761 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7281.4 16625.3 23048.9 +LP_Shaft 2836.5 41643.7 22490.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2115.06 0.9940 0.0550 1.92232 0.01477 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.419 0.9975 1.0000 0.9975 2706.36 0.725 818.6 24286.6 +Core_Nozz 1.195 0.9999 1.0000 0.9999 862.88 0.518 855.0 3850.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 120 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 5000.0 27.00 910.21 6383.7 0.6302 4022.68 7.4553 450.56 7.703 1805.5 1765.2 1383.7 + core size:21.40 Q: 197.26 Maximum Thrust: 31918.3 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 910.21 13.653 544.74 130.20 0.0000 1004.09 12.228 527.84 4652.5 0.4000 1.40001 +FS_2 Inlet.Fl_O 910.21 13.584 544.74 130.20 0.0000 1009.15 12.749 534.96 5943.4 0.3023 1.40001 +FS_21 Fan.Fl_O 910.21 15.822 571.41 136.61 0.0000 887.38 14.484 557.17 4515.2 0.3576 1.39951 +FS_13 Splitter.Fl_O2 802.56 15.822 571.41 136.61 0.0000 782.43 14.333 555.51 3795.6 0.3784 1.39951 +FS_22 Splitter.Fl_O1 107.65 15.822 571.41 136.61 0.0000 104.95 15.118 564.04 719.5 0.2558 1.39951 +FS_23 Duct1.Fl_O 107.65 15.782 571.41 136.61 0.0000 105.21 15.080 564.04 721.3 0.2558 1.39951 +FS_24 LPC.Fl_O 107.65 23.156 650.45 155.61 0.0000 76.51 20.906 631.80 366.0 0.3851 1.39780 +FS_25 Duct2.Fl_O 107.65 23.098 650.45 155.61 0.0000 76.70 20.854 631.80 366.9 0.3851 1.39780 +FS_3 HPC.Fl_O 107.65 105.165 1049.71 253.38 0.0000 21.40 97.955 1029.44 119.9 0.3225 1.37760 +FS_36 Bld3.Fl_O 97.96 105.165 1049.71 253.38 0.0000 19.47 97.955 1029.44 109.1 0.3225 1.37760 +FS_4 Burner.Fl_O 99.08 99.381 1805.51 456.85 0.0114 27.34 98.743 1802.65 483.4 0.0985 1.32760 +FS_45 HPT.Fl_O 108.77 35.581 1383.72 341.97 0.0104 73.38 33.463 1361.87 439.1 0.3026 1.34951 +FS_48 Duct3.Fl_O 108.77 35.403 1383.72 341.97 0.0104 73.75 33.296 1361.87 441.4 0.3026 1.34951 +FS_5 LPT.Fl_O 108.77 13.564 1105.29 269.58 0.0104 172.03 13.186 1096.93 1477.4 0.2036 1.36695 +FS_7 Duct4.Fl_O 108.77 13.428 1105.29 269.58 0.0104 173.77 13.227 1100.81 2018.9 0.1488 1.36695 +FS_9 Core_Nozz.Fl_O 108.77 13.428 1105.29 269.58 0.0104 173.77 12.228 1077.76 862.9 0.3725 1.36695 +FS_15 BypBld.Fl_O 802.56 15.822 571.41 136.61 0.0000 782.43 14.333 555.51 3795.6 0.3784 1.39951 +FS_17 Duct5.Fl_O 802.56 15.703 571.41 136.61 0.0000 788.35 14.225 555.51 3824.3 0.3784 1.39951 +FS_19 Byp_Nozz.Fl_O 802.56 15.703 571.41 136.61 0.0000 788.35 12.228 531.99 2706.4 0.6087 1.39951 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1009.15 1.165 0.9094 2212.140 1.0490 0.9114 -8245.1 53.01 16.70 +LPC 105.21 1.467 0.8350 2159.893 1.1383 0.8437 -2894.7 35.11 11.83 +HPC 76.70 4.553 0.8627 6153.043 1.6138 0.8879 -14890.9 36.75 37.19 +HPT 27.34 2.793 0.9163 162.163 1.2641 0.9055 14890.8 +LPT 73.75 2.610 0.9000 60.945 1.2519 0.8878 11139.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1934.91 1.115 0.9395 0.561 2.0579 0.5215 1.4369 0.9679 3943.9586 +LPC 112.85 1.143 0.8697 0.590 1.7092 0.9323 3.2631 0.9600 3662.6571 +HPC 182.35 17.425 0.8510 0.968 2.2350 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.220 0.9347 105.912 5.2203 1.4085 0.4249 0.9803 1.5311 +LPT 153.24 3.246 0.8988 75.137 3.2461 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4652.54 12746.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 791.84 189.83 35.121 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 791.84 189.83 35.121 +Duct1 0.0025 0.2558 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 791.84 189.83 35.121 +Duct2 0.0025 0.3851 365.99 +Duct3 0.0050 0.3026 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2036 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.7678 1049.71 253.38 105.165 +Duct5 0.0075 0.3784 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.9208 1049.71 253.38 105.165 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 571.41 136.61 15.822 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.4553 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6890.5 11350.1 14890.8 +LP_Shaft 2267.1 25807.7 11139.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1805.51 0.9940 0.0550 1.11741 0.01141 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.284 0.9975 1.0000 0.9975 2706.36 0.609 686.6 17126.7 +Core_Nozz 1.098 0.9999 1.0000 0.9999 862.88 0.372 592.6 2003.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 121 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 5000.0 27.00 1526.14 30031.2 0.5722 17184.35 5.4165 563.20 19.863 2730.0 2661.9 2139.3 + core size:20.01 Q: 308.21 Maximum Thrust: 30031.2 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1526.14 14.504 554.24 132.48 0.0000 1598.45 12.228 527.84 6240.7 0.5000 1.39982 +FS_2 Inlet.Fl_O 1526.14 14.432 554.24 132.48 0.0000 1606.50 11.830 523.63 5943.4 0.5405 1.39982 +FS_21 Fan.Fl_O 1526.14 22.836 640.48 153.21 0.0000 1091.41 19.724 614.30 4515.2 0.4624 1.39812 +FS_13 Splitter.Fl_O2 1288.29 22.836 640.48 153.21 0.0000 921.31 19.692 614.02 3795.6 0.4650 1.39812 +FS_22 Splitter.Fl_O1 237.85 22.836 640.48 153.21 0.0000 170.10 19.886 615.73 719.5 0.4491 1.39812 +FS_23 Duct1.Fl_O 237.85 22.778 640.48 153.21 0.0000 170.52 19.836 615.73 721.3 0.4491 1.39812 +FS_24 LPC.Fl_O 237.85 52.040 835.63 200.50 0.0000 85.25 45.543 804.88 366.0 0.4419 1.39026 +FS_25 Duct2.Fl_O 237.85 51.910 835.63 200.50 0.0000 85.47 45.429 804.88 366.9 0.4419 1.39026 +FS_3 HPC.Fl_O 237.85 288.102 1410.61 345.68 0.0000 20.01 271.004 1388.14 119.9 0.3015 1.35528 +FS_36 Bld3.Fl_O 216.44 288.102 1410.61 345.68 0.0000 18.21 271.004 1388.14 109.1 0.3015 1.35528 +FS_4 Burner.Fl_O 221.21 272.257 2730.00 733.00 0.0221 27.39 270.502 2726.00 483.4 0.1000 1.29391 +FS_45 HPT.Fl_O 242.62 101.127 2139.29 556.50 0.0201 71.61 95.404 2110.01 439.1 0.2992 1.30946 +FS_48 Duct3.Fl_O 242.62 100.621 2139.29 556.50 0.0201 71.97 94.927 2110.01 441.4 0.2992 1.30946 +FS_5 LPT.Fl_O 242.62 21.179 1512.28 379.77 0.0201 287.47 19.419 1479.58 1477.4 0.3622 1.33582 +FS_7 Duct4.Fl_O 242.62 20.967 1512.28 379.77 0.0201 290.37 20.060 1495.53 2018.9 0.2580 1.33582 +FS_9 Core_Nozz.Fl_O 242.62 20.967 1512.28 379.77 0.0201 290.37 12.228 1318.41 862.9 0.9263 1.33582 +FS_15 BypBld.Fl_O 1288.29 22.836 640.48 153.21 0.0000 921.31 19.692 614.02 3795.6 0.4650 1.39812 +FS_17 Duct5.Fl_O 1288.29 22.664 640.48 153.21 0.0000 928.28 19.545 614.02 3824.3 0.4650 1.39812 +FS_19 Byp_Nozz.Fl_O 1288.29 22.664 640.48 153.21 0.0000 928.28 12.228 537.06 2706.4 0.9818 1.39812 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1606.50 1.582 0.8989 3666.061 1.1556 0.9052 -44753.6 30.10 18.03 +LPC 170.52 2.285 0.8645 3410.332 1.3047 0.8792 -15914.6 28.51 21.28 +HPC 85.47 5.550 0.8645 6322.734 1.6881 0.8913 -48855.4 21.43 21.49 +HPT 27.39 2.692 0.9145 153.597 1.2294 0.9051 48855.5 +LPT 71.97 4.751 0.9280 81.935 1.4146 0.9137 60669.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3080.22 1.405 0.9287 0.930 2.1235 0.5215 1.4369 0.9679 3943.9586 +LPC 182.90 1.394 0.9005 0.931 1.7336 0.9323 3.2631 0.9600 3662.6571 +HPC 203.19 22.034 0.8529 0.995 2.0864 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 4.983 0.9329 100.317 4.9828 1.4085 0.4249 0.9803 1.5311 +LPT 149.54 6.233 0.9268 101.016 6.2325 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6240.68 26714.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1041.45 251.32 86.512 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1041.45 251.32 86.512 +Duct1 0.0025 0.4491 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1041.45 251.32 86.512 +Duct2 0.0025 0.4419 365.99 +Duct3 0.0050 0.2992 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3622 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 8.3247 1410.61 345.68 288.102 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 13.0816 1410.61 345.68 288.102 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 640.48 153.21 22.836 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.4165 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 8025.4 31972.9 48855.5 +LP_Shaft 3789.7 84080.6 60669.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.00 0.9940 0.0550 4.77343 0.02205 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.854 0.9975 1.0000 0.9975 2706.36 0.982 1112.7 44552.4 +Core_Nozz 1.715 0.9999 1.0000 0.9999 862.88 0.926 1617.0 12193.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 122 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 4/ 14/ 1/ 2 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 5000.0 27.00 1481.28 27028.4 0.5675 15339.63 5.5921 563.20 18.427 2637.6 2572.5 2063.0 + core size:20.15 Q: 308.21 Maximum Thrust: 30031.2 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1481.28 14.504 554.24 132.48 0.0000 1551.47 12.228 527.84 6057.3 0.5000 1.39982 +FS_2 Inlet.Fl_O 1481.28 14.432 554.24 132.48 0.0000 1559.28 12.023 526.07 5943.4 0.5174 1.39982 +FS_21 Fan.Fl_O 1481.28 22.192 634.17 151.69 0.0000 1084.68 19.213 608.65 4515.2 0.4587 1.39831 +FS_13 Splitter.Fl_O2 1256.58 22.192 634.17 151.69 0.0000 920.14 19.147 608.05 3795.6 0.4642 1.39831 +FS_22 Splitter.Fl_O1 224.71 22.192 634.17 151.69 0.0000 164.54 19.541 611.60 719.5 0.4303 1.39831 +FS_23 Duct1.Fl_O 224.71 22.136 634.17 151.69 0.0000 164.96 19.492 611.60 721.3 0.4303 1.39831 +FS_24 LPC.Fl_O 224.71 49.245 821.18 196.98 0.0000 84.38 43.245 791.70 366.0 0.4359 1.39093 +FS_25 Duct2.Fl_O 224.71 49.122 821.18 196.98 0.0000 84.59 43.137 791.70 366.9 0.4359 1.39093 +FS_3 HPC.Fl_O 224.71 267.276 1379.47 337.55 0.0000 20.15 251.174 1357.06 119.9 0.3037 1.35710 +FS_36 Bld3.Fl_O 204.48 267.276 1379.47 337.55 0.0000 18.34 251.174 1357.06 109.1 0.3037 1.35710 +FS_4 Burner.Fl_O 208.74 252.576 2637.60 704.11 0.0208 27.39 250.949 2633.71 483.4 0.0999 1.29652 +FS_45 HPT.Fl_O 228.97 93.470 2062.98 533.78 0.0190 71.80 88.151 2034.36 439.1 0.2997 1.31263 +FS_48 Duct3.Fl_O 228.97 93.003 2062.98 533.78 0.0190 72.16 87.710 2034.36 441.4 0.2997 1.31263 +FS_5 LPT.Fl_O 228.97 19.853 1459.55 365.06 0.0190 284.32 18.243 1428.55 1477.4 0.3570 1.33941 +FS_7 Duct4.Fl_O 228.97 19.655 1459.55 365.06 0.0190 287.19 18.823 1443.64 2018.9 0.2546 1.33941 +FS_9 Core_Nozz.Fl_O 228.97 19.655 1459.55 365.06 0.0190 287.19 12.227 1292.50 862.9 0.8648 1.33941 +FS_15 BypBld.Fl_O 1256.58 22.192 634.17 151.69 0.0000 920.14 19.147 608.05 3795.6 0.4642 1.39831 +FS_17 Duct5.Fl_O 1256.58 22.025 634.17 151.69 0.0000 927.09 19.003 608.05 3824.3 0.4642 1.39831 +FS_19 Byp_Nozz.Fl_O 1256.58 22.025 634.17 151.69 0.0000 927.09 12.228 536.12 2706.4 0.9568 1.39831 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1559.28 1.538 0.9058 3556.500 1.1442 0.9113 -40255.9 33.49 18.58 +LPC 164.96 2.225 0.8618 3324.828 1.2949 0.8763 -14397.1 27.70 19.78 +HPC 84.59 5.441 0.8651 6301.348 1.6799 0.8916 -44692.9 22.93 23.03 +HPT 27.39 2.702 0.9146 154.384 1.2324 0.9050 44692.4 +LPT 72.16 4.685 0.9270 80.943 1.4134 0.9124 54656.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2989.59 1.374 0.9357 0.902 2.0648 0.5215 1.4369 0.9679 3943.9586 +LPC 176.93 1.375 0.8977 0.908 1.7015 0.9323 3.2631 0.9600 3662.6571 +HPC 201.10 21.530 0.8535 0.991 2.1068 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.006 0.9330 100.831 5.0063 1.4085 0.4249 0.9803 1.5311 +LPT 149.94 6.140 0.9258 99.793 6.1398 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6057.25 25929.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1020.86 246.18 81.081 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1020.86 246.18 81.081 +Duct1 0.0025 0.4303 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1020.86 246.18 81.081 +Duct2 0.0025 0.4359 365.99 +Duct3 0.0050 0.2997 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3570 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.8648 1379.47 337.55 267.276 +Duct5 0.0075 0.4642 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 12.3589 1379.47 337.55 267.276 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 634.17 151.69 22.192 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5921 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7928.8 29604.7 44692.4 +LP_Shaft 3676.4 78081.3 54656.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2637.60 0.9940 0.0550 4.26101 0.02084 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.801 0.9975 1.0000 0.9975 2706.36 0.957 1083.4 42311.1 +Core_Nozz 1.607 0.9999 1.0000 0.9999 862.88 0.865 1496.1 10646.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 123 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 5000.0 27.00 1431.94 24025.0 0.5665 13610.53 5.7911 563.20 16.978 2547.6 2485.3 1989.2 + core size:20.28 Q: 308.21 Maximum Thrust: 30031.2 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1431.94 14.504 554.24 132.48 0.0000 1499.79 12.228 527.84 5855.5 0.5000 1.39982 +FS_2 Inlet.Fl_O 1431.94 14.432 554.24 132.48 0.0000 1507.34 12.220 528.52 5943.4 0.4932 1.39982 +FS_21 Fan.Fl_O 1431.94 21.514 627.75 150.15 0.0000 1076.08 18.681 602.98 4515.2 0.4539 1.39848 +FS_13 Splitter.Fl_O2 1221.08 21.514 627.75 150.15 0.0000 917.63 18.581 602.07 3795.6 0.4625 1.39848 +FS_22 Splitter.Fl_O1 210.85 21.514 627.75 150.15 0.0000 158.45 19.160 607.36 719.5 0.4104 1.39848 +FS_23 Duct1.Fl_O 210.85 21.460 627.75 150.15 0.0000 158.85 19.112 607.36 721.3 0.4104 1.39848 +FS_24 LPC.Fl_O 210.85 46.263 805.56 193.17 0.0000 83.47 40.768 777.36 366.0 0.4299 1.39168 +FS_25 Duct2.Fl_O 210.85 46.147 805.56 193.17 0.0000 83.68 40.666 777.36 366.9 0.4299 1.39168 +FS_3 HPC.Fl_O 210.85 246.251 1346.99 329.11 0.0000 20.28 231.212 1324.72 119.9 0.3056 1.35904 +FS_36 Bld3.Fl_O 191.88 246.251 1346.99 329.11 0.0000 18.45 231.212 1324.72 109.1 0.3056 1.35904 +FS_4 Burner.Fl_O 195.66 232.708 2547.63 676.27 0.0197 27.38 231.209 2543.84 483.4 0.0997 1.29926 +FS_45 HPT.Fl_O 214.63 85.856 1989.21 512.03 0.0179 71.95 80.948 1961.26 439.1 0.3000 1.31588 +FS_48 Duct3.Fl_O 214.63 85.426 1989.21 512.03 0.0179 72.31 80.543 1961.26 441.4 0.3000 1.31588 +FS_5 LPT.Fl_O 214.63 18.661 1412.08 351.93 0.0179 278.89 17.212 1383.17 1477.4 0.3486 1.34278 +FS_7 Duct4.Fl_O 214.63 18.475 1412.08 351.93 0.0179 281.71 17.724 1397.20 2018.9 0.2490 1.34278 +FS_9 Core_Nozz.Fl_O 214.63 18.475 1412.08 351.93 0.0179 281.71 12.228 1269.59 862.9 0.8028 1.34278 +FS_15 BypBld.Fl_O 1221.08 21.514 627.75 150.15 0.0000 917.63 18.581 602.07 3795.6 0.4625 1.39848 +FS_17 Duct5.Fl_O 1221.08 21.353 627.75 150.15 0.0000 924.56 18.442 602.07 3824.3 0.4625 1.39848 +FS_19 Byp_Nozz.Fl_O 1221.08 21.353 627.75 150.15 0.0000 924.56 12.228 535.40 2706.4 0.9291 1.39848 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1507.34 1.491 0.9099 3435.866 1.1326 0.9149 -35784.2 36.95 19.07 +LPC 158.85 2.156 0.8586 3228.440 1.2833 0.8729 -12834.8 26.91 18.31 +HPC 83.68 5.336 0.8655 6281.403 1.6721 0.8918 -40554.0 24.35 24.47 +HPT 27.38 2.710 0.9148 155.093 1.2351 0.9049 40554.0 +LPT 72.31 4.578 0.9249 79.634 1.4087 0.9101 48618.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2890.11 1.342 0.9401 0.871 2.0313 0.5215 1.4369 0.9679 3943.9586 +LPC 170.39 1.354 0.8944 0.881 1.6702 0.9323 3.2631 0.9600 3662.6571 +HPC 198.95 21.045 0.8538 0.988 2.1215 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.026 0.9331 101.294 5.0257 1.4085 0.4249 0.9803 1.5311 +LPT 150.25 5.991 0.9237 98.179 5.9908 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5855.46 25065.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 999.05 240.75 75.462 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 999.05 240.75 75.462 +Duct1 0.0025 0.4104 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 999.05 240.75 75.462 +Duct2 0.0025 0.4299 365.99 +Duct3 0.0050 0.3000 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3486 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.3799 1346.99 329.11 246.251 +Duct5 0.0075 0.4625 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.5969 1346.99 329.11 246.251 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 627.75 150.15 21.514 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.7911 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7828.2 27208.7 40554.0 +LP_Shaft 3551.7 71894.9 48618.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2547.63 0.9940 0.0550 3.78070 0.01970 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.746 0.9975 1.0000 0.9975 2706.36 0.929 1051.3 39901.0 +Core_Nozz 1.511 0.9999 1.0000 0.9999 862.88 0.803 1377.6 9189.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 124 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 5000.0 27.00 1319.62 18018.8 0.5748 10356.82 6.2632 563.20 14.046 2357.4 2300.8 1833.0 + core size:20.55 Q: 308.21 Maximum Thrust: 30031.2 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1319.62 14.504 554.24 132.48 0.0000 1382.15 12.228 527.84 5396.2 0.5000 1.39982 +FS_2 Inlet.Fl_O 1319.62 14.432 554.24 132.48 0.0000 1389.10 12.618 533.37 5943.4 0.4423 1.39982 +FS_21 Fan.Fl_O 1319.62 20.071 614.19 146.89 0.0000 1051.45 17.569 591.31 4515.2 0.4404 1.39879 +FS_13 Splitter.Fl_O2 1137.93 20.071 614.19 146.89 0.0000 906.68 17.413 589.80 3795.6 0.4552 1.39879 +FS_22 Splitter.Fl_O1 181.68 20.071 614.19 146.89 0.0000 144.76 18.282 598.06 719.5 0.3677 1.39879 +FS_23 Duct1.Fl_O 181.68 20.021 614.19 146.89 0.0000 145.13 18.236 598.06 721.3 0.3677 1.39879 +FS_24 LPC.Fl_O 181.68 39.797 769.48 184.39 0.0000 81.72 35.299 743.83 366.0 0.4182 1.39342 +FS_25 Duct2.Fl_O 181.68 39.698 769.48 184.39 0.0000 81.92 35.211 743.83 366.9 0.4182 1.39342 +FS_3 HPC.Fl_O 181.68 203.732 1275.62 310.67 0.0000 20.55 190.926 1253.70 119.9 0.3098 1.36340 +FS_36 Bld3.Fl_O 165.33 203.732 1275.62 310.67 0.0000 18.70 190.926 1253.70 109.1 0.3098 1.36340 +FS_4 Burner.Fl_O 168.21 192.527 2357.38 618.26 0.0174 27.37 191.288 2353.82 483.4 0.0995 1.30528 +FS_45 HPT.Fl_O 184.56 70.470 1832.98 466.70 0.0158 72.35 66.395 1806.45 439.1 0.3010 1.32339 +FS_48 Duct3.Fl_O 184.56 70.118 1832.98 466.70 0.0158 72.72 66.063 1806.45 441.4 0.3010 1.32339 +FS_5 LPT.Fl_O 184.56 16.640 1320.23 326.81 0.0158 260.05 15.531 1296.82 1477.4 0.3209 1.34969 +FS_7 Duct4.Fl_O 184.56 16.474 1320.23 326.81 0.0158 262.68 15.896 1308.06 2018.9 0.2305 1.34969 +FS_9 Core_Nozz.Fl_O 184.56 16.474 1320.23 326.81 0.0158 262.68 12.227 1221.51 862.8 0.6761 1.34969 +FS_15 BypBld.Fl_O 1137.93 20.071 614.19 146.89 0.0000 906.68 17.413 589.80 3795.6 0.4552 1.39879 +FS_17 Duct5.Fl_O 1137.93 19.920 614.19 146.89 0.0000 913.53 17.282 589.80 3824.3 0.4552 1.39879 +FS_19 Byp_Nozz.Fl_O 1137.93 19.920 614.19 146.89 0.0000 913.53 12.228 534.30 2706.4 0.8650 1.39879 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1389.10 1.391 0.9127 3151.640 1.1082 0.9167 -26887.8 43.02 19.79 +LPC 145.13 1.988 0.8518 2993.887 1.2528 0.8652 -9641.6 25.87 15.68 +HPC 81.92 5.132 0.8654 6246.852 1.6578 0.8912 -32460.1 27.29 27.46 +HPT 27.37 2.732 0.9151 156.711 1.2415 0.9052 32460.1 +LPT 72.72 4.214 0.9212 76.096 1.3884 0.9066 36528.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2663.42 1.272 0.9430 0.799 2.0106 0.5215 1.4369 0.9679 3943.9586 +LPC 155.67 1.303 0.8873 0.817 1.6226 0.9323 3.2631 0.9600 3662.6571 +HPC 194.76 20.102 0.8538 0.983 2.1501 0.4206 0.2163 1.0137 6357.1603 +HPT 30.12 5.076 0.9334 102.350 5.0765 1.4085 0.4249 0.9803 1.5311 +LPT 151.10 5.483 0.9201 93.817 5.4832 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5396.17 23099.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 950.00 228.59 63.729 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 950.00 228.59 63.729 +Duct1 0.0025 0.3677 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 950.00 228.59 63.729 +Duct2 0.0025 0.4182 365.99 +Duct3 0.0050 0.3010 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3209 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.3589 1275.62 310.67 203.732 +Duct5 0.0075 0.4552 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.9926 1275.62 310.67 203.732 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 614.19 146.89 20.071 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.2632 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7608.7 22406.3 32460.1 +LP_Shaft 3257.9 58888.3 36528.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2357.38 0.9940 0.0550 2.87690 0.01740 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.629 0.9975 1.0000 0.9975 2706.36 0.865 977.7 34580.6 +Core_Nozz 1.347 0.9999 1.0000 0.9999 862.88 0.676 1139.7 6537.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 125 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 5000.0 27.00 1184.63 12012.5 0.6066 7286.68 6.8763 563.20 11.036 2131.9 2082.3 1648.6 + core size:20.91 Q: 308.21 Maximum Thrust: 30031.2 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1184.63 14.504 554.24 132.48 0.0000 1240.76 12.228 527.84 4844.2 0.5000 1.39982 +FS_2 Inlet.Fl_O 1184.63 14.432 554.24 132.48 0.0000 1247.01 13.018 538.16 5943.4 0.3865 1.39982 +FS_21 Fan.Fl_O 1184.63 18.510 599.00 143.23 0.0000 1010.75 16.407 578.74 4515.2 0.4188 1.39906 +FS_13 Splitter.Fl_O2 1034.22 18.510 599.00 143.23 0.0000 882.42 16.212 576.77 3795.6 0.4394 1.39906 +FS_22 Splitter.Fl_O1 150.40 18.510 599.00 143.23 0.0000 128.33 17.245 587.03 719.5 0.3197 1.39906 +FS_23 Duct1.Fl_O 150.40 18.464 599.00 143.23 0.0000 128.65 17.202 587.03 721.3 0.3197 1.39906 +FS_24 LPC.Fl_O 150.40 32.927 725.92 173.84 0.0000 79.42 29.443 703.28 366.0 0.4034 1.39516 +FS_25 Duct2.Fl_O 150.40 32.844 725.92 173.84 0.0000 79.62 29.370 703.28 366.9 0.4034 1.39516 +FS_3 HPC.Fl_O 150.40 160.071 1189.44 288.63 0.0000 20.91 149.630 1167.99 119.9 0.3152 1.36881 +FS_36 Bld3.Fl_O 136.87 160.071 1189.44 288.63 0.0000 19.03 149.630 1167.99 109.1 0.3152 1.36881 +FS_4 Burner.Fl_O 138.89 151.267 2131.94 551.03 0.0148 27.36 150.295 2128.66 483.4 0.0991 1.31327 +FS_45 HPT.Fl_O 152.43 54.832 1648.57 414.47 0.0135 72.84 51.617 1623.82 439.1 0.3020 1.33334 +FS_48 Duct3.Fl_O 152.43 54.557 1648.57 414.47 0.0135 73.20 51.359 1623.82 441.4 0.3020 1.33334 +FS_5 LPT.Fl_O 152.43 15.027 1223.30 300.73 0.0135 228.93 14.266 1206.66 1477.4 0.2776 1.35735 +FS_7 Duct4.Fl_O 152.43 14.877 1223.30 300.73 0.0135 231.25 14.476 1214.54 2018.9 0.2008 1.35735 +FS_9 Core_Nozz.Fl_O 152.43 14.877 1223.30 300.73 0.0135 231.25 12.228 1161.58 862.9 0.5434 1.35735 +FS_15 BypBld.Fl_O 1034.22 18.510 599.00 143.23 0.0000 882.42 16.212 576.77 3795.6 0.4394 1.39906 +FS_17 Duct5.Fl_O 1034.22 18.371 599.00 143.23 0.0000 889.09 16.090 576.77 3824.3 0.4394 1.39906 +FS_19 Byp_Nozz.Fl_O 1034.22 18.371 599.00 143.23 0.0000 889.09 12.228 533.25 2706.4 0.7854 1.39906 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1247.01 1.283 0.9120 2795.232 1.0808 0.9150 -18017.8 47.60 20.22 +LPC 128.65 1.783 0.8440 2688.772 1.2119 0.8561 -6512.0 26.36 13.23 +HPC 79.62 4.874 0.8643 6207.444 1.6385 0.8897 -24427.4 31.29 31.52 +HPT 27.36 2.759 0.9156 159.047 1.2501 0.9052 24427.5 +LPT 73.20 3.631 0.9159 71.166 1.3476 0.9016 24529.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2390.97 1.197 0.9422 0.709 2.0417 0.5215 1.4369 0.9679 3943.9586 +LPC 138.00 1.240 0.8791 0.734 1.5999 0.9323 3.2631 0.9600 3662.6571 +HPC 189.28 18.907 0.8526 0.976 2.1797 0.4206 0.2163 1.0137 6357.1603 +HPT 30.10 5.139 0.9339 103.876 5.1394 1.4085 0.4249 0.9803 1.5311 +LPT 152.11 4.670 0.9147 87.738 4.6696 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4844.17 20736.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 890.80 214.01 51.483 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 890.80 214.01 51.483 +Duct1 0.0025 0.3197 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 890.80 214.01 51.483 +Duct2 0.0025 0.4034 365.99 +Duct3 0.0050 0.3020 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2776 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.2642 1189.44 288.63 160.071 +Duct5 0.0075 0.4394 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.2722 1189.44 288.63 160.071 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 599.00 143.23 18.510 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.8763 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7343.7 17470.3 24427.5 +LP_Shaft 2889.5 44585.8 24529.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2131.94 0.9940 0.0550 2.02408 0.01479 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.502 0.9975 1.0000 0.9975 2706.36 0.785 886.9 28508.6 +Core_Nozz 1.217 0.9999 1.0000 0.9999 862.88 0.543 895.1 4240.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 126 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 5000.0 27.00 1013.14 6006.2 0.7228 4341.06 7.8052 563.20 7.811 1833.1 1792.6 1406.6 + core size:21.47 Q: 308.21 Maximum Thrust: 30031.2 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1013.14 14.504 554.24 132.48 0.0000 1061.15 12.228 527.84 4142.9 0.5000 1.39982 +FS_2 Inlet.Fl_O 1013.14 14.432 554.24 132.48 0.0000 1066.49 13.432 543.00 5943.4 0.3218 1.39982 +FS_21 Fan.Fl_O 1013.14 16.809 581.66 139.07 0.0000 938.02 15.199 565.18 4515.2 0.3820 1.39933 +FS_13 Splitter.Fl_O2 898.08 16.809 581.66 139.07 0.0000 831.49 14.992 562.97 3795.6 0.4076 1.39933 +FS_22 Splitter.Fl_O1 115.06 16.809 581.66 139.07 0.0000 106.53 16.037 573.91 719.5 0.2600 1.39933 +FS_23 Duct1.Fl_O 115.06 16.767 581.66 139.07 0.0000 106.80 15.997 573.91 721.3 0.2600 1.39933 +FS_24 LPC.Fl_O 115.06 25.319 668.51 159.97 0.0000 75.82 22.909 649.76 366.0 0.3810 1.39713 +FS_25 Duct2.Fl_O 115.06 25.255 668.51 159.97 0.0000 76.01 22.851 649.76 366.9 0.3810 1.39713 +FS_3 HPC.Fl_O 115.06 113.293 1073.11 259.24 0.0000 21.47 105.472 1052.30 119.9 0.3238 1.37614 +FS_36 Bld3.Fl_O 104.71 113.293 1073.11 259.24 0.0000 19.54 105.472 1052.30 109.1 0.3238 1.37614 +FS_4 Burner.Fl_O 105.91 107.062 1833.12 464.59 0.0115 27.33 106.375 1830.22 483.4 0.0985 1.32635 +FS_45 HPT.Fl_O 116.27 38.365 1406.56 348.05 0.0105 73.34 36.084 1384.44 439.1 0.3026 1.34810 +FS_48 Duct3.Fl_O 116.27 38.173 1406.56 348.05 0.0105 73.71 35.903 1384.44 441.4 0.3026 1.34810 +FS_5 LPT.Fl_O 116.27 13.740 1106.91 270.01 0.0105 181.66 13.312 1097.53 1477.4 0.2157 1.36678 +FS_7 Duct4.Fl_O 116.27 13.603 1106.91 270.01 0.0105 183.50 13.375 1101.90 2018.9 0.1574 1.36678 +FS_9 Core_Nozz.Fl_O 116.27 13.603 1106.91 270.01 0.0105 183.50 12.228 1075.59 862.9 0.3978 1.36678 +FS_15 BypBld.Fl_O 898.08 16.809 581.66 139.07 0.0000 831.49 14.992 562.97 3795.6 0.4076 1.39933 +FS_17 Duct5.Fl_O 898.08 16.683 581.66 139.07 0.0000 837.78 14.880 562.97 3824.3 0.4076 1.39933 +FS_19 Byp_Nozz.Fl_O 898.08 16.683 581.66 139.07 0.0000 837.78 12.228 532.25 2706.4 0.6813 1.39933 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1066.49 1.165 0.9000 2280.327 1.0495 0.9022 -9435.3 57.45 19.65 +LPC 106.80 1.510 0.8344 2225.944 1.1493 0.8438 -3402.1 31.96 11.20 +HPC 76.01 4.486 0.8624 6139.976 1.6052 0.8875 -16161.3 37.83 38.33 +HPT 27.33 2.791 0.9164 162.810 1.2630 0.9056 16161.4 +LPT 73.71 2.778 0.9030 62.853 1.2707 0.8904 12837.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2044.84 1.115 0.9298 0.578 2.1781 0.5215 1.4369 0.9679 3943.9586 +LPC 114.55 1.156 0.8691 0.608 1.6549 0.9323 3.2631 0.9600 3662.6571 +HPC 180.71 17.114 0.8508 0.966 2.2456 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.214 0.9348 106.334 5.2143 1.4085 0.4249 0.9803 1.5311 +LPT 153.16 3.480 0.9019 77.489 3.4805 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4142.92 17734.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 811.89 194.71 38.153 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 811.89 194.71 38.153 +Duct1 0.0025 0.2600 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 811.89 194.71 38.153 +Duct2 0.0025 0.3810 365.99 +Duct3 0.0050 0.3026 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2157 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.0271 1073.11 259.24 113.293 +Duct5 0.0075 0.4076 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.3283 1073.11 259.24 113.293 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 581.66 139.07 16.809 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8052 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6970.7 12176.9 16161.4 +LP_Shaft 2357.2 28602.8 12837.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1833.12 0.9940 0.0550 1.20585 0.01152 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.364 0.9975 1.0000 0.9975 2706.36 0.681 768.7 21456.4 +Core_Nozz 1.112 0.9999 1.0000 0.9999 862.88 0.398 632.2 2284.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 127 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 10000.0 27.00 1152.40 38694.7 0.3619 14002.25 4.9618 0.00 23.019 2697.7 2629.2 2116.4 + core size:19.84 Q: 0.00 Maximum Thrust: 38694.7 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1152.40 10.106 510.01 121.88 0.0000 1661.70 10.106 510.01 -----.- 0.0000 1.40066 +FS_2 Inlet.Fl_O 1152.40 10.025 510.01 121.88 0.0000 1675.10 8.003 478.16 5943.4 0.5764 1.40066 +FS_21 Fan.Fl_O 1152.40 16.712 601.62 143.86 0.0000 1091.40 14.435 577.00 4515.2 0.4623 1.39902 +FS_13 Splitter.Fl_O2 959.11 16.712 601.62 143.86 0.0000 908.33 14.490 577.62 3795.6 0.4562 1.39902 +FS_22 Splitter.Fl_O1 193.30 16.712 601.62 143.86 0.0000 183.06 14.131 573.50 719.5 0.4956 1.39902 +FS_23 Duct1.Fl_O 193.30 16.671 601.62 143.86 0.0000 183.52 14.095 573.50 721.3 0.4956 1.39902 +FS_24 LPC.Fl_O 193.30 41.203 804.25 192.85 0.0000 85.85 35.973 774.06 366.0 0.4456 1.39174 +FS_25 Duct2.Fl_O 193.30 41.100 804.25 192.85 0.0000 86.07 35.884 774.06 366.9 0.4456 1.39174 +FS_3 HPC.Fl_O 193.30 232.636 1368.75 334.76 0.0000 19.84 219.085 1347.25 119.9 0.2984 1.35774 +FS_36 Bld3.Fl_O 175.90 232.636 1368.75 334.76 0.0000 18.05 219.085 1347.25 109.1 0.2984 1.35774 +FS_4 Burner.Fl_O 179.79 219.841 2697.70 723.31 0.0221 27.41 218.423 2693.73 483.4 0.1000 1.29447 +FS_45 HPT.Fl_O 197.19 82.494 2116.44 549.91 0.0201 70.96 77.916 2087.99 439.1 0.2961 1.31012 +FS_48 Duct3.Fl_O 197.19 82.082 2116.44 549.91 0.0201 71.32 77.526 2087.99 441.4 0.2961 1.31012 +FS_5 LPT.Fl_O 197.19 17.127 1488.80 373.39 0.0201 286.66 15.712 1456.73 1477.4 0.3608 1.33704 +FS_7 Duct4.Fl_O 197.19 16.956 1488.80 373.39 0.0201 289.56 16.226 1472.37 2018.9 0.2571 1.33704 +FS_9 Core_Nozz.Fl_O 197.19 16.956 1488.80 373.39 0.0201 289.56 10.106 1304.77 862.9 0.9059 1.33704 +FS_15 BypBld.Fl_O 959.11 16.712 601.62 143.86 0.0000 908.33 14.490 577.62 3795.6 0.4562 1.39902 +FS_17 Duct5.Fl_O 959.11 16.587 601.62 143.86 0.0000 915.20 14.381 577.62 3824.3 0.4562 1.39902 +FS_19 Byp_Nozz.Fl_O 959.11 16.587 601.62 143.86 0.0000 915.20 10.106 522.22 2706.4 0.8720 1.39902 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.10 1.667 0.8752 3944.235 1.1796 0.8838 -35852.2 23.38 16.20 +LPC 183.52 2.472 0.8688 3631.522 1.3368 0.8843 -13396.8 29.03 23.83 +HPC 86.07 5.660 0.8643 6339.400 1.7019 0.8916 -38811.4 19.55 19.57 +HPT 27.41 2.665 0.9136 151.985 1.2270 0.9042 38812.3 +LPT 71.32 4.793 0.9330 85.016 1.4216 0.9194 49248.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.78 1.464 0.9042 1.000 2.2673 0.5215 1.4369 0.9679 3943.9586 +LPC 196.86 1.451 0.9050 0.991 1.7826 0.9323 3.2631 0.9600 3662.6571 +HPC 204.61 22.544 0.8527 0.997 2.0396 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.919 0.9319 99.264 4.9186 1.4085 0.4249 0.9803 1.5311 +LPT 148.19 6.291 0.9318 104.815 6.2905 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1006.17 242.52 69.160 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1006.17 242.52 69.160 +Duct1 0.0025 0.4956 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1006.17 242.52 69.160 +Duct2 0.0025 0.4456 365.99 +Duct3 0.0050 0.2961 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3608 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.7654 1368.75 334.76 232.636 +Duct5 0.0075 0.4562 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.6313 1368.75 334.76 232.636 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 601.62 143.86 16.712 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 4.9618 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7894.0 25823.0 38812.3 +LP_Shaft 3911.2 66132.8 49248.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2697.70 0.9940 0.0550 3.88951 0.02211 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.641 0.9975 1.0000 0.9975 2706.36 0.872 974.5 29050.6 +Core_Nozz 1.678 0.9999 1.0000 0.9999 862.88 0.906 1573.6 9644.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 128 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 10000.0 27.00 1102.85 34825.1 0.3448 12008.89 5.2476 0.00 20.551 2583.9 2518.6 2017.9 + core size:19.93 Q: 0.00 Maximum Thrust: 38694.7 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1102.85 10.106 510.01 121.88 0.0000 1590.24 10.106 510.01 -----.- 0.0000 1.40066 +FS_2 Inlet.Fl_O 1102.85 10.025 510.01 121.88 0.0000 1603.07 8.228 481.98 5943.4 0.5386 1.40066 +FS_21 Fan.Fl_O 1102.85 16.160 592.64 141.71 0.0000 1072.04 14.051 569.46 4515.2 0.4515 1.39916 +FS_13 Splitter.Fl_O2 926.32 16.160 592.64 141.71 0.0000 900.45 14.056 569.50 3795.6 0.4510 1.39916 +FS_22 Splitter.Fl_O1 176.52 16.160 592.64 141.71 0.0000 171.59 14.029 569.20 719.5 0.4541 1.39916 +FS_23 Duct1.Fl_O 176.52 16.120 592.64 141.71 0.0000 172.02 13.994 569.20 721.3 0.4541 1.39916 +FS_24 LPC.Fl_O 176.52 36.530 771.62 184.92 0.0000 86.62 31.796 741.94 366.0 0.4506 1.39332 +FS_25 Duct2.Fl_O 176.52 36.439 771.62 184.92 0.0000 86.83 31.716 741.94 366.9 0.4506 1.39332 +FS_3 HPC.Fl_O 176.52 207.695 1320.85 322.34 0.0000 19.93 195.473 1299.76 119.9 0.2996 1.36062 +FS_36 Bld3.Fl_O 160.64 207.695 1320.85 322.34 0.0000 18.14 195.473 1299.76 109.1 0.2996 1.36062 +FS_4 Burner.Fl_O 163.97 196.272 2583.86 687.97 0.0208 27.40 195.006 2580.03 483.4 0.0999 1.29772 +FS_45 HPT.Fl_O 179.86 72.672 2017.93 520.80 0.0189 71.74 68.544 1989.88 439.1 0.2993 1.31421 +FS_48 Duct3.Fl_O 179.86 72.309 2017.93 520.80 0.0189 72.10 68.201 1989.88 441.4 0.2993 1.31421 +FS_5 LPT.Fl_O 179.86 15.649 1429.02 356.80 0.0189 280.36 14.419 1399.52 1477.4 0.3510 1.34117 +FS_7 Duct4.Fl_O 179.86 15.492 1429.02 356.80 0.0189 283.20 14.856 1413.85 2018.9 0.2506 1.34117 +FS_9 Core_Nozz.Fl_O 179.86 15.492 1429.02 356.80 0.0189 283.20 10.106 1280.50 862.9 0.8179 1.34117 +FS_15 BypBld.Fl_O 926.32 16.160 592.64 141.71 0.0000 900.45 14.056 569.50 3795.6 0.4510 1.39916 +FS_17 Duct5.Fl_O 926.32 16.039 592.64 141.71 0.0000 907.25 13.950 569.50 3824.3 0.4510 1.39916 +FS_19 Byp_Nozz.Fl_O 926.32 16.039 592.64 141.71 0.0000 907.25 10.106 519.37 2706.4 0.8398 1.39916 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1603.07 1.612 0.9023 3682.416 1.1620 0.9086 -30942.6 27.40 16.17 +LPC 172.02 2.266 0.8662 3416.054 1.3020 0.8805 -10791.7 30.06 22.62 +HPC 86.83 5.700 0.8617 6365.268 1.7118 0.8896 -34321.4 19.67 19.64 +HPT 27.40 2.701 0.9142 152.735 1.2329 0.9043 34321.8 +LPT 72.10 4.621 0.9286 81.287 1.4121 0.9144 41733.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3073.56 1.426 0.9321 0.934 2.0192 0.5215 1.4369 0.9679 3943.9586 +LPC 184.51 1.388 0.9022 0.933 1.7735 0.9323 3.2631 0.9600 3662.6571 +HPC 206.44 22.726 0.8501 1.001 2.0756 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 5.003 0.9325 99.754 5.0029 1.4085 0.4249 0.9803 1.5311 +LPT 149.82 6.051 0.9274 100.217 6.0508 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 967.87 233.01 61.528 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 967.87 233.01 61.528 +Duct1 0.0025 0.4541 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 967.87 233.01 61.528 +Duct2 0.0025 0.4506 365.99 +Duct3 0.0050 0.2993 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3510 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.1783 1320.85 322.34 207.695 +Duct5 0.0075 0.4510 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.7088 1320.85 322.34 207.695 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 592.64 141.71 16.160 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.2476 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7763.8 23218.3 34321.8 +LP_Shaft 3651.5 60027.1 41733.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2583.86 0.9940 0.0550 3.33580 0.02077 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.587 0.9975 1.0000 0.9975 2706.36 0.840 936.1 26950.5 +Core_Nozz 1.533 0.9999 1.0000 0.9999 862.88 0.818 1408.7 7874.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 129 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 10000.0 27.00 1045.58 30955.9 0.3337 10328.56 5.4286 0.00 18.501 2472.3 2410.4 1926.2 + core size:20.08 Q: 0.00 Maximum Thrust: 38694.7 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1045.58 10.106 510.01 121.88 0.0000 1507.68 10.106 510.01 -----.- 0.0000 1.40066 +FS_2 Inlet.Fl_O 1045.58 10.025 510.01 121.88 0.0000 1519.83 8.457 485.78 5943.4 0.4988 1.40066 +FS_21 Fan.Fl_O 1045.58 15.517 584.66 139.79 0.0000 1051.33 13.584 562.86 4515.2 0.4402 1.39928 +FS_13 Splitter.Fl_O2 882.94 15.517 584.66 139.79 0.0000 887.79 13.563 562.62 3795.6 0.4428 1.39928 +FS_22 Splitter.Fl_O1 162.64 15.517 584.66 139.79 0.0000 163.54 13.691 564.12 719.5 0.4268 1.39928 +FS_23 Duct1.Fl_O 162.64 15.479 584.66 139.79 0.0000 163.95 13.657 564.12 721.3 0.4268 1.39928 +FS_24 LPC.Fl_O 162.64 33.516 751.03 179.92 0.0000 85.82 29.268 722.76 366.0 0.4450 1.39422 +FS_25 Duct2.Fl_O 162.64 33.433 751.03 179.92 0.0000 86.03 29.195 722.76 366.9 0.4450 1.39422 +FS_3 HPC.Fl_O 162.64 186.979 1279.49 311.67 0.0000 20.08 175.803 1258.63 119.9 0.3018 1.36316 +FS_36 Bld3.Fl_O 148.01 186.979 1279.49 311.67 0.0000 18.27 175.803 1258.63 109.1 0.3018 1.36316 +FS_4 Burner.Fl_O 150.88 176.695 2472.28 653.64 0.0194 27.40 175.556 2468.58 483.4 0.0997 1.30116 +FS_45 HPT.Fl_O 165.51 65.126 1926.19 493.93 0.0176 71.97 61.401 1898.95 439.1 0.2998 1.31842 +FS_48 Duct3.Fl_O 165.51 64.801 1926.19 493.93 0.0176 72.34 61.094 1898.95 441.4 0.2998 1.31842 +FS_5 LPT.Fl_O 165.51 14.584 1372.90 341.35 0.0176 271.35 13.518 1346.36 1477.4 0.3374 1.34529 +FS_7 Duct4.Fl_O 165.51 14.438 1372.90 341.35 0.0176 274.09 13.885 1359.18 2018.9 0.2416 1.34529 +FS_9 Core_Nozz.Fl_O 165.51 14.438 1372.90 341.35 0.0176 274.09 10.106 1251.82 862.9 0.7434 1.34529 +FS_15 BypBld.Fl_O 882.94 15.517 584.66 139.79 0.0000 887.79 13.563 562.62 3795.6 0.4428 1.39928 +FS_17 Duct5.Fl_O 882.94 15.401 584.66 139.79 0.0000 894.50 13.461 562.62 3824.3 0.4428 1.39928 +FS_19 Byp_Nozz.Fl_O 882.94 15.401 584.66 139.79 0.0000 894.50 10.106 518.34 2706.4 0.7997 1.39928 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1519.83 1.548 0.9086 3513.602 1.1464 0.9141 -26496.8 31.12 16.21 +LPC 163.95 2.165 0.8632 3281.642 1.2846 0.8770 -9234.8 29.55 20.82 +HPC 86.03 5.593 0.8635 6337.398 1.7037 0.8908 -30317.9 21.18 21.20 +HPT 27.40 2.713 0.9145 153.372 1.2365 0.9046 30317.5 +LPT 72.34 4.443 0.9262 79.386 1.4030 0.9119 35732.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2914.08 1.381 0.9387 0.891 1.9155 0.5215 1.4369 0.9679 3943.9586 +LPC 175.86 1.357 0.8991 0.896 1.7418 0.9323 3.2631 0.9600 3662.6571 +HPC 204.53 22.231 0.8518 0.997 2.0979 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.032 0.9329 100.170 5.0320 1.4085 0.4249 0.9803 1.5311 +LPT 150.31 5.803 0.9250 97.873 5.8032 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 939.63 226.03 55.927 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 939.63 226.03 55.927 +Duct1 0.0025 0.4268 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 939.63 226.03 55.927 +Duct2 0.0025 0.4450 365.99 +Duct3 0.0050 0.2998 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3374 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.6926 1279.49 311.67 186.979 +Duct5 0.0075 0.4428 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.9455 1279.49 311.67 186.979 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 584.66 139.79 15.517 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.4286 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7625.9 20880.2 30317.5 +LP_Shaft 3484.1 53863.7 35732.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2472.28 0.9940 0.0550 2.86904 0.01938 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.524 0.9975 1.0000 0.9975 2706.36 0.800 890.5 24436.6 +Core_Nozz 1.429 0.9999 1.0000 0.9999 862.88 0.743 1267.3 6519.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 130 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 10000.0 27.00 913.24 23216.6 0.3178 7377.64 5.7933 0.00 14.554 2249.3 2194.1 1742.2 + core size:20.37 Q: 0.00 Maximum Thrust: 38694.7 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 913.24 10.106 510.01 121.88 0.0000 1316.85 10.106 510.01 -----.- 0.0000 1.40066 +FS_2 Inlet.Fl_O 913.24 10.025 510.01 121.88 0.0000 1327.47 8.892 492.80 5943.4 0.4173 1.40066 +FS_21 Fan.Fl_O 913.24 14.185 568.85 135.99 0.0000 990.86 12.646 550.49 4515.2 0.4084 1.39955 +FS_13 Splitter.Fl_O2 778.81 14.185 568.85 135.99 0.0000 845.00 12.594 549.84 3795.6 0.4158 1.39955 +FS_22 Splitter.Fl_O1 134.43 14.185 568.85 135.99 0.0000 145.86 12.899 553.62 719.5 0.3709 1.39955 +FS_23 Duct1.Fl_O 134.43 14.149 568.85 135.99 0.0000 146.22 12.867 553.62 721.3 0.3709 1.39955 +FS_24 LPC.Fl_O 134.43 27.306 705.55 168.91 0.0000 84.38 23.981 680.02 366.0 0.4352 1.39582 +FS_25 Duct2.Fl_O 134.43 27.238 705.55 168.91 0.0000 84.60 23.921 680.02 366.9 0.4352 1.39582 +FS_3 HPC.Fl_O 134.43 147.085 1193.24 289.59 0.0000 20.37 138.016 1172.94 119.9 0.3061 1.36857 +FS_36 Bld3.Fl_O 122.33 147.085 1193.24 289.59 0.0000 18.54 138.016 1172.94 109.1 0.3061 1.36857 +FS_4 Burner.Fl_O 124.38 138.995 2249.29 586.25 0.0168 27.39 138.100 2245.87 483.4 0.0994 1.30863 +FS_45 HPT.Fl_O 136.48 50.659 1742.19 441.08 0.0152 72.56 47.711 1716.57 439.1 0.3015 1.32775 +FS_48 Duct3.Fl_O 136.48 50.405 1742.19 441.08 0.0152 72.93 47.473 1716.57 441.4 0.3015 1.32775 +FS_5 LPT.Fl_O 136.48 12.923 1273.08 314.21 0.0152 243.16 12.179 1253.49 1477.4 0.2972 1.35301 +FS_7 Duct4.Fl_O 136.48 12.794 1273.08 314.21 0.0152 245.61 12.404 1262.82 2018.9 0.2143 1.35301 +FS_9 Core_Nozz.Fl_O 136.48 12.794 1273.08 314.21 0.0152 245.61 10.106 1196.81 862.9 0.5983 1.35301 +FS_15 BypBld.Fl_O 778.81 14.185 568.85 135.99 0.0000 845.00 12.594 549.84 3795.6 0.4158 1.39955 +FS_17 Duct5.Fl_O 778.81 14.078 568.85 135.99 0.0000 851.39 12.499 549.84 3824.3 0.4158 1.39955 +FS_19 Byp_Nozz.Fl_O 778.81 14.078 568.85 135.99 0.0000 851.39 10.106 517.42 2706.4 0.7048 1.39955 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1327.47 1.415 0.9041 3125.319 1.1154 0.9087 -18237.4 35.72 15.31 +LPC 146.22 1.930 0.8567 2959.272 1.2403 0.8693 -6261.2 29.48 17.84 +HPC 84.60 5.400 0.8643 6301.025 1.6912 0.8911 -22954.6 24.04 24.13 +HPT 27.39 2.744 0.9148 154.956 1.2451 0.9047 22954.5 +LPT 72.93 3.900 0.9220 74.249 1.3685 0.9080 24498.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2545.24 1.289 0.9340 0.792 1.8069 0.5215 1.4369 0.9679 3943.9586 +LPC 156.85 1.285 0.8924 0.808 1.7060 0.9323 3.2631 0.9600 3662.6571 +HPC 201.12 21.340 0.8526 0.991 2.1420 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.104 0.9332 101.204 5.1041 1.4085 0.4249 0.9803 1.5311 +LPT 151.54 5.046 0.9208 91.539 5.0459 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 879.13 211.15 44.796 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 879.13 211.15 44.796 +Duct1 0.0025 0.3709 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 879.13 211.15 44.796 +Duct2 0.0025 0.4352 365.99 +Duct3 0.0050 0.3015 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2972 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.7052 1193.24 289.59 147.085 +Duct5 0.0075 0.4158 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.3938 1193.24 289.59 147.085 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 568.85 135.99 14.185 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.7933 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7349.0 16404.9 22954.5 +LP_Shaft 3099.1 41517.8 24498.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2249.29 0.9940 0.0550 2.04934 0.01675 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.393 0.9975 1.0000 0.9975 2706.36 0.705 784.1 18978.9 +Core_Nozz 1.266 0.9999 1.0000 0.9999 862.88 0.598 999.0 4237.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 131 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 10000.0 27.00 751.48 15477.9 0.3080 4767.43 6.1257 0.00 10.703 1985.8 1938.5 1527.2 + core size:20.76 Q: 0.00 Maximum Thrust: 38694.7 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 751.48 10.106 510.01 121.88 0.0000 1083.59 10.106 510.01 -----.- 0.0000 1.40066 +FS_2 Inlet.Fl_O 751.48 10.025 510.01 121.88 0.0000 1092.33 9.294 499.07 5943.4 0.3307 1.40066 +FS_21 Fan.Fl_O 751.48 12.828 551.54 131.84 0.0000 887.78 11.742 537.78 4515.2 0.3577 1.39988 +FS_13 Splitter.Fl_O2 646.02 12.828 551.54 131.84 0.0000 763.19 11.686 537.05 3795.6 0.3673 1.39988 +FS_22 Splitter.Fl_O1 105.46 12.828 551.54 131.84 0.0000 124.59 12.005 541.20 719.5 0.3091 1.39988 +FS_23 Duct1.Fl_O 105.46 12.796 551.54 131.84 0.0000 124.90 11.975 541.20 721.3 0.3091 1.39988 +FS_24 LPC.Fl_O 105.46 21.226 652.57 156.12 0.0000 81.90 18.816 630.55 366.0 0.4187 1.39773 +FS_25 Duct2.Fl_O 105.46 21.173 652.57 156.12 0.0000 82.10 18.769 630.55 366.9 0.4187 1.39773 +FS_3 HPC.Fl_O 105.46 108.167 1089.26 263.30 0.0000 20.76 101.221 1069.70 119.9 0.3120 1.37512 +FS_36 Bld3.Fl_O 95.97 108.167 1089.26 263.30 0.0000 18.90 101.221 1069.70 109.1 0.3120 1.37512 +FS_4 Burner.Fl_O 97.29 102.218 1985.83 508.73 0.0138 27.37 101.561 1982.74 483.4 0.0989 1.31882 +FS_45 HPT.Fl_O 106.79 36.823 1527.16 381.07 0.0126 73.13 34.646 1503.70 439.1 0.3026 1.34004 +FS_48 Duct3.Fl_O 106.79 36.639 1527.16 381.07 0.0126 73.50 34.473 1503.70 441.4 0.3026 1.34004 +FS_5 LPT.Fl_O 106.79 11.718 1171.22 287.00 0.0126 201.25 11.266 1159.04 1477.4 0.2410 1.36127 +FS_7 Duct4.Fl_O 106.79 11.601 1171.22 287.00 0.0126 203.28 11.361 1164.74 2018.9 0.1753 1.36127 +FS_9 Core_Nozz.Fl_O 106.79 11.601 1171.22 287.00 0.0126 203.28 10.106 1129.03 862.8 0.4537 1.36127 +FS_15 BypBld.Fl_O 646.02 12.828 551.54 131.84 0.0000 763.19 11.686 537.05 3795.6 0.3673 1.39988 +FS_17 Duct5.Fl_O 646.02 12.732 551.54 131.84 0.0000 768.96 11.598 537.05 3824.3 0.3673 1.39988 +FS_19 Byp_Nozz.Fl_O 646.02 12.732 551.54 131.84 0.0000 768.96 10.106 516.30 2706.4 0.5840 1.39988 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1092.33 1.280 0.8968 2638.831 1.0814 0.9003 -10589.9 34.61 12.90 +LPC 124.90 1.659 0.8479 2537.528 1.1832 0.8583 -3623.6 32.67 14.97 +HPC 82.10 5.109 0.8643 6249.861 1.6692 0.8909 -15991.8 28.28 28.45 +HPT 27.37 2.776 0.9153 157.313 1.2559 0.9049 15991.8 +LPT 73.50 3.127 0.9103 66.959 1.3039 0.8970 14212.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2094.39 1.195 0.9264 0.669 1.7152 0.5215 1.4369 0.9679 3943.9586 +LPC 133.98 1.202 0.8832 0.693 1.7168 0.9323 3.2631 0.9600 3662.6571 +HPC 195.19 19.993 0.8527 0.983 2.1814 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.180 0.9337 102.744 5.1798 1.4085 0.4249 0.9803 1.5311 +LPT 152.72 3.967 0.9091 82.553 3.9668 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 807.46 193.63 33.918 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 807.46 193.63 33.918 +Duct1 0.0025 0.3091 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 807.46 193.63 33.918 +Duct2 0.0025 0.4187 365.99 +Duct3 0.0050 0.3026 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2410 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.6911 1089.26 263.30 108.167 +Duct5 0.0075 0.3673 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.8003 1089.26 263.30 108.167 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 551.54 131.84 12.828 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.1257 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7010.3 11981.0 15991.8 +LP_Shaft 2616.7 28526.9 14212.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1985.83 0.9940 0.0550 1.32429 0.01380 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.260 0.9975 1.0000 0.9975 2706.36 0.584 649.0 13030.2 +Core_Nozz 1.148 0.9999 1.0000 0.9999 862.88 0.454 737.5 2447.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 132 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 8/ 18/ 1/ 6 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.000 10000.0 27.00 536.47 7738.9 0.3147 2435.38 6.2095 0.00 6.819 1627.2 1590.9 1239.6 + core size:21.47 Q: 0.00 Maximum Thrust: 38694.7 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 536.47 10.106 510.01 121.88 0.0000 773.56 10.106 510.01 -----.- 0.0000 1.40066 +FS_2 Inlet.Fl_O 536.47 10.025 510.01 121.88 0.0000 779.80 9.668 504.74 5943.4 0.2282 1.40066 +FS_21 Fan.Fl_O 536.47 11.477 532.56 127.28 0.0000 696.07 10.903 524.81 4515.2 0.2717 1.40026 +FS_13 Splitter.Fl_O2 462.06 11.477 532.56 127.28 0.0000 599.52 10.873 524.39 3795.6 0.2790 1.40026 +FS_22 Splitter.Fl_O1 74.41 11.477 532.56 127.28 0.0000 96.55 11.048 526.80 719.5 0.2338 1.40026 +FS_23 Duct1.Fl_O 74.41 11.448 532.56 127.28 0.0000 96.79 11.021 526.80 721.3 0.2338 1.40026 +FS_24 LPC.Fl_O 74.41 15.203 586.72 140.28 0.0000 76.51 13.726 569.86 366.0 0.3849 1.39925 +FS_25 Duct2.Fl_O 74.41 15.165 586.72 140.28 0.0000 76.70 13.692 569.86 366.9 0.3849 1.39925 +FS_3 HPC.Fl_O 74.41 68.914 949.55 228.48 0.0000 21.47 64.158 930.88 119.9 0.3229 1.38383 +FS_36 Bld3.Fl_O 67.71 68.914 949.55 228.48 0.0000 19.54 64.158 930.88 109.1 0.3229 1.38383 +FS_4 Burner.Fl_O 68.39 65.124 1627.19 407.18 0.0100 27.34 64.706 1624.55 483.4 0.0981 1.33676 +FS_45 HPT.Fl_O 75.09 23.196 1239.64 303.85 0.0091 73.55 21.809 1219.58 439.1 0.3023 1.35926 +FS_48 Duct3.Fl_O 75.09 23.080 1239.64 303.85 0.0091 73.92 21.700 1219.58 441.4 0.3023 1.35926 +FS_5 LPT.Fl_O 75.09 10.863 1038.42 252.33 0.0091 143.74 10.654 1032.96 1477.4 0.1685 1.37209 +FS_7 Duct4.Fl_O 75.09 10.754 1038.42 252.33 0.0091 145.19 10.642 1035.47 2018.9 0.1236 1.37209 +FS_9 Core_Nozz.Fl_O 75.09 10.754 1038.42 252.33 0.0091 145.19 10.106 1021.02 862.8 0.3023 1.37209 +FS_15 BypBld.Fl_O 462.06 11.477 532.56 127.28 0.0000 599.52 10.873 524.39 3795.6 0.2790 1.40026 +FS_17 Duct5.Fl_O 462.06 11.391 532.56 127.28 0.0000 604.05 10.791 524.39 3824.3 0.2790 1.40026 +FS_19 Byp_Nozz.Fl_O 462.06 11.391 532.56 127.28 0.0000 604.05 10.106 514.64 2706.4 0.4170 1.40026 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 779.80 1.145 0.8916 1940.747 1.0442 0.8938 -4104.5 35.83 7.50 +LPC 96.79 1.328 0.8300 1899.202 1.1017 0.8367 -1368.7 45.37 12.77 +HPC 76.70 4.544 0.8623 6152.944 1.6184 0.8876 -9285.4 37.05 37.49 +HPT 27.34 2.808 0.9164 162.231 1.2719 0.9053 9285.4 +LPT 73.92 2.125 0.8880 54.659 1.1938 0.8775 5473.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1495.16 1.101 0.9212 0.492 1.6384 0.5215 1.4369 0.9679 3943.9586 +LPC 103.82 1.100 0.8646 0.519 1.8716 0.9323 3.2631 0.9600 3662.6571 +HPC 182.34 17.385 0.8507 0.968 2.2406 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.254 0.9348 105.956 5.2542 1.4085 0.4249 0.9803 1.5311 +LPT 153.59 2.569 0.8868 67.388 2.5689 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9920 -----.-- 0.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 714.83 171.15 23.039 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 714.83 171.15 23.039 +Duct1 0.0025 0.2338 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 714.83 171.15 23.039 +Duct2 0.0025 0.3849 365.99 +Duct3 0.0050 0.3023 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1685 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.6044 949.55 228.48 68.914 +Duct5 0.0075 0.2790 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.0927 949.55 228.48 68.914 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 532.56 127.28 11.477 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.2095 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6544.2 7452.2 9285.4 +LP_Shaft 1924.5 14936.8 5473.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1627.19 0.9940 0.0550 0.67649 0.00999 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.127 0.9975 1.0000 0.9975 2706.36 0.417 462.7 6644.5 +Core_Nozz 1.064 0.9999 1.0000 0.9999 862.88 0.302 469.0 1094.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 133 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 2/ 12/ 1/ 0 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 10000.0 27.00 1160.50 35225.8 0.4001 14093.00 4.9695 110.73 23.002 2700.2 2631.7 2118.6 + core size:19.84 Q: 10.19 Maximum Thrust: 35225.8 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1160.50 10.177 511.03 122.12 0.0000 1663.37 10.106 510.01 28215.7 0.1000 1.40065 +FS_2 Inlet.Fl_O 1160.50 10.106 511.03 122.12 0.0000 1675.10 8.067 479.12 5943.4 0.5764 1.40065 +FS_21 Fan.Fl_O 1160.50 16.824 602.64 144.11 0.0000 1092.70 14.525 577.90 4515.2 0.4630 1.39900 +FS_13 Splitter.Fl_O2 966.09 16.824 602.64 144.11 0.0000 909.65 14.578 578.50 3795.6 0.4571 1.39900 +FS_22 Splitter.Fl_O1 194.40 16.824 602.64 144.11 0.0000 183.05 14.226 574.47 719.5 0.4955 1.39900 +FS_23 Duct1.Fl_O 194.40 16.782 602.64 144.11 0.0000 183.51 14.190 574.47 721.3 0.4955 1.39900 +FS_24 LPC.Fl_O 194.40 41.510 805.80 193.23 0.0000 85.79 36.251 775.61 366.0 0.4452 1.39167 +FS_25 Duct2.Fl_O 194.40 41.406 805.80 193.23 0.0000 86.00 36.161 775.61 366.9 0.4452 1.39167 +FS_3 HPC.Fl_O 194.40 234.102 1370.70 335.27 0.0000 19.84 220.461 1349.17 119.9 0.2984 1.35762 +FS_36 Bld3.Fl_O 176.91 234.102 1370.70 335.27 0.0000 18.05 220.461 1349.17 109.1 0.2984 1.35762 +FS_4 Burner.Fl_O 180.82 221.226 2700.23 724.09 0.0221 27.41 219.800 2696.26 483.4 0.1000 1.29441 +FS_45 HPT.Fl_O 198.32 83.027 2118.61 550.55 0.0201 70.95 78.421 2090.15 439.1 0.2961 1.31005 +FS_48 Duct3.Fl_O 198.32 82.612 2118.61 550.55 0.0201 71.30 78.028 2090.15 441.4 0.2961 1.31005 +FS_5 LPT.Fl_O 198.32 17.219 1490.06 373.74 0.0201 286.88 15.795 1457.91 1477.4 0.3611 1.33697 +FS_7 Duct4.Fl_O 198.32 17.047 1490.06 373.74 0.0201 289.78 16.312 1473.59 2018.9 0.2573 1.33697 +FS_9 Core_Nozz.Fl_O 198.32 17.047 1490.06 373.74 0.0201 289.78 10.106 1304.10 862.8 0.9109 1.33697 +FS_15 BypBld.Fl_O 966.09 16.824 602.64 144.11 0.0000 909.65 14.578 578.50 3795.6 0.4571 1.39900 +FS_17 Duct5.Fl_O 966.09 16.698 602.64 144.11 0.0000 916.52 14.469 578.50 3824.3 0.4571 1.39900 +FS_19 Byp_Nozz.Fl_O 966.09 16.698 602.64 144.11 0.0000 916.52 10.106 522.11 2706.4 0.8782 1.39900 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.10 1.665 0.8745 3944.235 1.1793 0.8832 -36102.0 23.51 16.32 +LPC 183.51 2.474 0.8688 3632.099 1.3371 0.8842 -13510.2 28.95 23.77 +HPC 86.00 5.654 0.8644 6337.682 1.7011 0.8916 -39069.6 19.62 19.64 +HPT 27.41 2.665 0.9136 152.019 1.2269 0.9042 39068.6 +LPT 71.30 4.798 0.9330 85.058 1.4218 0.9194 49612.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.78 1.463 0.9035 1.000 2.2780 0.5215 1.4369 0.9679 3943.9586 +LPC 196.84 1.452 0.9049 0.992 1.7807 0.9323 3.2631 0.9600 3662.6571 +HPC 204.47 22.513 0.8528 0.997 2.0400 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.918 0.9319 99.286 4.9176 1.4085 0.4249 0.9803 1.5311 +LPT 148.17 6.298 0.9318 104.866 6.2976 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 28215.72 3994.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1007.87 242.94 69.636 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1007.87 242.94 69.636 +Duct1 0.0025 0.4955 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1007.87 242.94 69.636 +Duct2 0.0025 0.4452 365.99 +Duct3 0.0050 0.2961 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3611 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.8042 1370.70 335.27 234.102 +Duct5 0.0075 0.4571 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.6923 1370.70 335.27 234.102 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 602.64 144.11 16.824 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 4.9695 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7899.5 25975.5 39068.6 +LP_Shaft 3915.1 66555.0 49612.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2700.23 0.9940 0.0550 3.91472 0.02213 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.652 0.9975 1.0000 0.9975 2706.36 0.878 981.4 29469.1 +Core_Nozz 1.687 0.9999 1.0000 0.9999 862.88 0.911 1581.9 9750.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 134 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 10000.0 27.00 1114.07 31703.0 0.3840 12175.06 5.2477 110.73 20.646 2591.2 2525.8 2024.2 + core size:19.93 Q: 10.19 Maximum Thrust: 35225.8 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1114.07 10.177 511.03 122.12 0.0000 1596.83 10.106 510.01 27086.9 0.1000 1.40065 +FS_2 Inlet.Fl_O 1114.07 10.106 511.03 122.12 0.0000 1608.09 8.279 482.69 5943.4 0.5411 1.40065 +FS_21 Fan.Fl_O 1114.07 16.303 594.05 142.05 0.0000 1074.75 14.163 570.66 4515.2 0.4530 1.39913 +FS_13 Splitter.Fl_O2 935.75 16.303 594.05 142.05 0.0000 902.72 14.167 570.71 3795.6 0.4525 1.39913 +FS_22 Splitter.Fl_O1 178.32 16.303 594.05 142.05 0.0000 172.02 14.140 570.40 719.5 0.4556 1.39913 +FS_23 Duct1.Fl_O 178.32 16.262 594.05 142.05 0.0000 172.45 14.105 570.40 721.3 0.4556 1.39913 +FS_24 LPC.Fl_O 178.32 36.985 774.30 185.56 0.0000 86.57 32.197 744.55 366.0 0.4503 1.39319 +FS_25 Duct2.Fl_O 178.32 36.892 774.30 185.56 0.0000 86.79 32.117 744.55 366.9 0.4503 1.39319 +FS_3 HPC.Fl_O 178.32 210.115 1324.64 323.32 0.0000 19.93 197.752 1303.50 119.9 0.2996 1.36039 +FS_36 Bld3.Fl_O 162.27 210.115 1324.64 323.32 0.0000 18.14 197.752 1303.50 109.1 0.2996 1.36039 +FS_4 Burner.Fl_O 165.65 198.559 2591.24 690.24 0.0208 27.40 197.279 2587.39 483.4 0.0999 1.29751 +FS_45 HPT.Fl_O 181.70 73.566 2024.21 522.64 0.0190 71.71 69.391 1996.11 439.1 0.2991 1.31395 +FS_48 Duct3.Fl_O 181.70 73.198 2024.21 522.64 0.0190 72.07 69.044 1996.11 441.4 0.2991 1.31395 +FS_5 LPT.Fl_O 181.70 15.781 1432.53 357.77 0.0190 281.19 14.533 1402.76 1477.4 0.3522 1.34093 +FS_7 Duct4.Fl_O 181.70 15.624 1432.53 357.77 0.0190 284.03 14.978 1417.23 2018.9 0.2514 1.34093 +FS_9 Core_Nozz.Fl_O 181.70 15.624 1432.53 357.77 0.0190 284.03 10.106 1280.91 862.9 0.8264 1.34093 +FS_15 BypBld.Fl_O 935.75 16.303 594.05 142.05 0.0000 902.72 14.167 570.71 3795.6 0.4525 1.39913 +FS_17 Duct5.Fl_O 935.75 16.181 594.05 142.05 0.0000 909.55 14.061 570.71 3824.3 0.4525 1.39913 +FS_19 Byp_Nozz.Fl_O 935.75 16.181 594.05 142.05 0.0000 909.55 10.106 519.30 2706.4 0.8483 1.39913 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1608.09 1.613 0.9014 3692.271 1.1625 0.9078 -31405.8 27.40 16.32 +LPC 172.45 2.274 0.8663 3424.553 1.3034 0.8806 -10979.4 29.99 22.65 +HPC 86.79 5.695 0.8620 6362.447 1.7108 0.8899 -34753.9 19.72 19.69 +HPT 27.40 2.699 0.9141 152.714 1.2326 0.9043 34754.1 +LPT 72.07 4.638 0.9287 81.460 1.4130 0.9145 42384.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3083.22 1.427 0.9312 0.936 2.0362 0.5215 1.4369 0.9679 3943.9586 +LPC 184.98 1.391 0.9023 0.935 1.7730 0.9323 3.2631 0.9600 3662.6571 +HPC 206.32 22.706 0.8504 1.001 2.0746 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.999 0.9325 99.740 4.9990 1.4085 0.4249 0.9803 1.5311 +LPT 149.75 6.075 0.9275 100.430 6.0752 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 27086.87 3834.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 970.96 233.78 62.270 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 970.96 233.78 62.270 +Duct1 0.0025 0.4556 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 970.96 233.78 62.270 +Duct2 0.0025 0.4503 365.99 +Duct3 0.0050 0.2991 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3522 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.2410 1324.64 323.32 210.115 +Duct5 0.0075 0.4525 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.8074 1324.64 323.32 210.115 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 594.05 142.05 16.303 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.2477 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7773.8 23480.5 34754.1 +LP_Shaft 3665.0 60739.8 42384.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2591.24 0.9940 0.0550 3.38196 0.02084 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.601 0.9975 1.0000 0.9975 2706.36 0.848 945.5 27498.5 +Core_Nozz 1.546 0.9999 1.0000 0.9999 862.88 0.826 1423.5 8038.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 135 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 10000.0 27.00 1060.14 28180.9 0.3741 10543.84 5.4259 110.73 18.682 2484.0 2421.8 1935.9 + core size:20.07 Q: 10.19 Maximum Thrust: 35225.8 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1060.14 10.177 511.03 122.12 0.0000 1519.53 10.106 510.01 25775.7 0.1000 1.40065 +FS_2 Inlet.Fl_O 1060.14 10.106 511.03 122.12 0.0000 1530.25 8.498 486.31 5943.4 0.5036 1.40065 +FS_21 Fan.Fl_O 1060.14 15.689 586.37 140.20 0.0000 1055.89 13.714 564.28 4515.2 0.4427 1.39925 +FS_13 Splitter.Fl_O2 895.17 15.689 586.37 140.20 0.0000 891.57 13.693 564.04 3795.6 0.4452 1.39925 +FS_22 Splitter.Fl_O1 164.98 15.689 586.37 140.20 0.0000 164.32 13.821 565.54 719.5 0.4294 1.39925 +FS_23 Duct1.Fl_O 164.98 15.649 586.37 140.20 0.0000 164.73 13.787 565.54 721.3 0.4294 1.39925 +FS_24 LPC.Fl_O 164.98 34.085 754.58 180.78 0.0000 85.80 29.767 726.20 366.0 0.4449 1.39407 +FS_25 Duct2.Fl_O 164.98 34.000 754.58 180.78 0.0000 86.01 29.693 726.20 366.9 0.4449 1.39407 +FS_3 HPC.Fl_O 164.98 190.134 1285.12 313.12 0.0000 20.07 178.778 1264.19 119.9 0.3017 1.36281 +FS_36 Bld3.Fl_O 150.13 190.134 1285.12 313.12 0.0000 18.27 178.778 1264.19 109.1 0.3017 1.36281 +FS_4 Burner.Fl_O 153.06 179.677 2483.99 657.21 0.0195 27.40 178.519 2480.28 483.4 0.0997 1.30081 +FS_45 HPT.Fl_O 167.91 66.264 1935.91 496.75 0.0178 71.94 62.478 1908.59 439.1 0.2997 1.31797 +FS_48 Duct3.Fl_O 167.91 65.933 1935.91 496.75 0.0178 72.30 62.165 1908.59 441.4 0.2997 1.31797 +FS_5 LPT.Fl_O 167.91 14.735 1377.95 342.73 0.0178 272.95 13.644 1350.98 1477.4 0.3397 1.34492 +FS_7 Duct4.Fl_O 167.91 14.588 1377.95 342.73 0.0178 275.71 14.022 1364.02 2018.9 0.2432 1.34492 +FS_9 Core_Nozz.Fl_O 167.91 14.588 1377.95 342.73 0.0178 275.71 10.106 1253.15 862.9 0.7546 1.34492 +FS_15 BypBld.Fl_O 895.17 15.689 586.37 140.20 0.0000 891.57 13.693 564.04 3795.6 0.4452 1.39925 +FS_17 Duct5.Fl_O 895.17 15.571 586.37 140.20 0.0000 898.31 13.590 564.04 3824.3 0.4452 1.39925 +FS_19 Byp_Nozz.Fl_O 895.17 15.571 586.37 140.20 0.0000 898.31 10.106 518.24 2706.4 0.8107 1.39925 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1530.25 1.552 0.9085 3531.142 1.1474 0.9140 -27117.9 31.05 16.41 +LPC 164.73 2.178 0.8634 3296.484 1.2869 0.8773 -9471.7 29.48 20.91 +HPC 86.01 5.592 0.8635 6336.900 1.7031 0.8908 -30890.3 21.16 21.19 +HPT 27.40 2.712 0.9145 153.359 1.2361 0.9046 30889.8 +LPT 72.30 4.475 0.9265 79.662 1.4049 0.9122 36590.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2934.05 1.384 0.9386 0.895 1.9334 0.5215 1.4369 0.9679 3943.9586 +LPC 176.69 1.361 0.8993 0.900 1.7421 0.9323 3.2631 0.9600 3662.6571 +HPC 204.48 22.229 0.8519 0.997 2.0967 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.028 0.9329 100.161 5.0283 1.4085 0.4249 0.9803 1.5311 +LPT 150.25 5.847 0.9253 98.213 5.8469 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 25775.75 3648.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 943.95 227.10 56.874 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 943.95 227.10 56.874 +Duct1 0.0025 0.4294 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 943.95 227.10 56.874 +Duct2 0.0025 0.4449 365.99 +Duct3 0.0050 0.2997 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3397 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.7743 1285.12 313.12 190.134 +Duct5 0.0075 0.4452 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.0738 1285.12 313.12 190.134 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 586.37 140.20 15.689 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.4259 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7643.3 21225.9 30889.8 +LP_Shaft 3505.0 54828.2 36590.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2483.99 0.9940 0.0550 2.92884 0.01951 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.541 0.9975 1.0000 0.9975 2706.36 0.811 902.6 25113.1 +Core_Nozz 1.443 0.9999 1.0000 0.9999 862.88 0.755 1287.0 6716.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 136 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 10000.0 27.00 935.17 21135.4 0.3623 7656.44 5.7911 110.73 14.875 2270.0 2214.2 1759.4 + core size:20.36 Q: 10.19 Maximum Thrust: 35225.8 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 935.17 10.177 511.03 122.12 0.0000 1340.41 10.106 510.01 22737.2 0.1000 1.40065 +FS_2 Inlet.Fl_O 935.17 10.106 511.03 122.12 0.0000 1349.86 8.918 493.08 5943.4 0.4262 1.40065 +FS_21 Fan.Fl_O 935.17 14.402 571.12 136.54 0.0000 1001.36 12.801 552.22 4515.2 0.4138 1.39951 +FS_13 Splitter.Fl_O2 797.47 14.402 571.12 136.54 0.0000 853.90 12.747 551.55 3795.6 0.4213 1.39951 +FS_22 Splitter.Fl_O1 137.71 14.402 571.12 136.54 0.0000 147.45 13.064 555.45 719.5 0.3758 1.39951 +FS_23 Duct1.Fl_O 137.71 14.366 571.12 136.54 0.0000 147.82 13.032 555.45 721.3 0.3758 1.39951 +FS_24 LPC.Fl_O 137.71 28.082 711.22 170.28 0.0000 84.39 24.662 685.49 366.0 0.4353 1.39563 +FS_25 Duct2.Fl_O 137.71 28.012 711.22 170.28 0.0000 84.60 24.600 685.49 366.9 0.4353 1.39563 +FS_3 HPC.Fl_O 137.71 151.386 1202.59 291.98 0.0000 20.36 142.070 1182.20 119.9 0.3059 1.36798 +FS_36 Bld3.Fl_O 125.31 151.386 1202.59 291.98 0.0000 18.52 142.070 1182.20 109.1 0.3059 1.36798 +FS_4 Burner.Fl_O 127.44 143.060 2269.99 592.43 0.0170 27.39 142.139 2266.54 483.4 0.0994 1.30792 +FS_45 HPT.Fl_O 139.83 52.209 1759.38 445.95 0.0154 72.49 49.177 1733.61 439.1 0.3012 1.32685 +FS_48 Duct3.Fl_O 139.83 51.947 1759.38 445.95 0.0154 72.86 48.931 1733.61 441.4 0.3012 1.32685 +FS_5 LPT.Fl_O 139.83 13.080 1280.86 316.31 0.0154 246.89 12.301 1260.51 1477.4 0.3023 1.35239 +FS_7 Duct4.Fl_O 139.83 12.949 1280.86 316.31 0.0154 249.38 12.542 1270.22 2018.9 0.2179 1.35239 +FS_9 Core_Nozz.Fl_O 139.83 12.949 1280.86 316.31 0.0154 249.38 10.106 1200.39 862.9 0.6140 1.35239 +FS_15 BypBld.Fl_O 797.47 14.402 571.12 136.54 0.0000 853.90 12.747 551.55 3795.6 0.4213 1.39951 +FS_17 Duct5.Fl_O 797.47 14.294 571.12 136.54 0.0000 860.36 12.651 551.55 3824.3 0.4213 1.39951 +FS_19 Byp_Nozz.Fl_O 797.47 14.294 571.12 136.54 0.0000 860.36 10.106 517.24 2706.4 0.7215 1.39951 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1349.86 1.425 0.9063 3163.714 1.1176 0.9109 -19073.8 36.07 15.73 +LPC 147.82 1.955 0.8571 2992.651 1.2453 0.8699 -6574.3 29.24 17.98 +HPC 84.60 5.404 0.8644 6301.138 1.6909 0.8912 -23710.3 23.92 24.02 +HPT 27.39 2.740 0.9148 154.869 1.2442 0.9047 23710.3 +LPT 72.86 3.971 0.9223 74.868 1.3736 0.9083 25647.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2588.16 1.296 0.9363 0.802 1.8285 0.5215 1.4369 0.9679 3943.9586 +LPC 158.56 1.293 0.8928 0.817 1.7030 0.9323 3.2631 0.9600 3662.6571 +HPC 201.12 21.360 0.8527 0.991 2.1386 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.096 0.9331 101.148 5.0957 1.4085 0.4249 0.9803 1.5311 +LPT 151.39 5.145 0.9212 92.303 5.1451 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 22737.23 3218.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 886.16 212.87 46.086 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 886.16 212.87 46.086 +Duct1 0.0025 0.3758 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 886.16 212.87 46.086 +Duct2 0.0025 0.4353 365.99 +Duct3 0.0050 0.3012 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3023 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.8197 1202.59 291.98 151.386 +Duct5 0.0075 0.4213 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.5738 1202.59 291.98 151.386 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 571.12 136.54 14.402 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.7911 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7378.6 16877.0 23710.3 +LP_Shaft 3140.3 42895.1 25647.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2269.99 0.9940 0.0550 2.12679 0.01697 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.414 0.9975 1.0000 0.9975 2706.36 0.722 802.6 19892.1 +Core_Nozz 1.281 0.9999 1.0000 0.9999 862.88 0.614 1026.7 4461.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 137 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 10000.0 27.00 782.18 14090.0 0.3600 5072.22 6.1483 110.73 11.123 2019.2 1971.0 1554.5 + core size:20.72 Q: 10.19 Maximum Thrust: 35225.8 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 782.18 10.177 511.03 122.12 0.0000 1121.12 10.106 510.01 19017.5 0.1000 1.40065 +FS_2 Inlet.Fl_O 782.18 10.106 511.03 122.12 0.0000 1129.03 9.313 499.22 5943.4 0.3435 1.40065 +FS_21 Fan.Fl_O 782.18 13.071 554.37 132.51 0.0000 909.19 11.904 539.75 4515.2 0.3679 1.39982 +FS_13 Splitter.Fl_O2 672.76 13.071 554.37 132.51 0.0000 782.00 11.842 538.95 3795.6 0.3781 1.39982 +FS_22 Splitter.Fl_O1 109.42 13.071 554.37 132.51 0.0000 127.19 12.195 543.49 719.5 0.3164 1.39982 +FS_23 Duct1.Fl_O 109.42 13.038 554.37 132.51 0.0000 127.51 12.164 543.49 721.3 0.3164 1.39982 +FS_24 LPC.Fl_O 109.42 22.100 660.41 158.01 0.0000 82.11 19.575 638.00 366.0 0.4201 1.39744 +FS_25 Duct2.Fl_O 109.42 22.044 660.41 158.01 0.0000 82.31 19.526 638.00 366.9 0.4201 1.39744 +FS_3 HPC.Fl_O 109.42 113.200 1103.48 266.87 0.0000 20.72 105.963 1083.78 119.9 0.3113 1.37423 +FS_36 Bld3.Fl_O 99.57 113.200 1103.48 266.87 0.0000 18.86 105.963 1083.78 109.1 0.3113 1.37423 +FS_4 Burner.Fl_O 100.98 106.974 2019.19 518.41 0.0141 27.37 106.286 2016.05 483.4 0.0990 1.31740 +FS_45 HPT.Fl_O 110.83 38.601 1554.48 388.58 0.0129 73.05 36.324 1530.73 439.1 0.3024 1.33841 +FS_48 Duct3.Fl_O 110.83 38.408 1554.48 388.58 0.0129 73.42 36.142 1530.73 441.4 0.3024 1.33841 +FS_5 LPT.Fl_O 110.83 11.853 1182.77 290.06 0.0129 207.52 11.365 1169.67 1477.4 0.2492 1.36032 +FS_7 Duct4.Fl_O 110.83 11.734 1182.77 290.06 0.0129 209.61 11.476 1175.82 2018.9 0.1811 1.36032 +FS_9 Core_Nozz.Fl_O 110.83 11.734 1182.77 290.06 0.0129 209.61 10.106 1136.80 863.0 0.4725 1.36032 +FS_15 BypBld.Fl_O 672.76 13.071 554.37 132.51 0.0000 782.00 11.842 538.95 3795.6 0.3781 1.39982 +FS_17 Duct5.Fl_O 672.76 12.973 554.37 132.51 0.0000 787.91 11.753 538.95 3824.3 0.3781 1.39982 +FS_19 Byp_Nozz.Fl_O 672.76 12.973 554.37 132.51 0.0000 787.91 10.106 516.17 2706.4 0.6081 1.39982 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1129.03 1.293 0.9001 2703.139 1.0848 0.9037 -11502.4 35.69 13.76 +LPC 127.51 1.695 0.8489 2595.328 1.1913 0.8597 -3947.3 31.73 15.19 +HPC 82.31 5.135 0.8644 6253.778 1.6709 0.8910 -16853.2 27.85 28.00 +HPT 27.37 2.771 0.9152 157.042 1.2544 0.9049 16853.2 +LPT 73.42 3.240 0.9116 68.054 1.3143 0.8981 15448.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2164.76 1.204 0.9299 0.685 1.7474 0.5215 1.4369 0.9679 3943.9586 +LPC 136.78 1.213 0.8842 0.709 1.7060 0.9323 3.2631 0.9600 3662.6571 +HPC 195.69 20.116 0.8528 0.984 2.1766 0.4206 0.2163 1.0137 6357.1603 +HPT 30.12 5.169 0.9336 102.567 5.1689 1.4085 0.4249 0.9803 1.5311 +LPT 152.55 4.125 0.9104 83.902 4.1254 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 19017.52 2692.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 817.63 196.11 35.399 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 817.63 196.11 35.399 +Duct1 0.0025 0.3164 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 817.63 196.11 35.399 +Duct2 0.0025 0.4201 365.99 +Duct3 0.0050 0.3024 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2492 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.8298 1103.48 266.87 113.200 +Duct5 0.0075 0.3781 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.0182 1103.48 266.87 113.200 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 554.37 132.51 13.071 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.1483 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7056.7 12543.4 16853.2 +LP_Shaft 2683.2 30239.4 15448.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2019.19 0.9940 0.0550 1.40895 0.01415 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.284 0.9975 1.0000 0.9975 2706.36 0.608 675.7 14127.7 +Core_Nozz 1.161 0.9999 1.0000 0.9999 862.88 0.473 770.6 2654.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 138 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.100 10000.0 27.00 579.28 7045.1 0.3825 2694.47 6.3779 110.73 7.252 1675.5 1637.7 1278.0 + core size:21.37 Q: 10.19 Maximum Thrust: 35225.8 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 579.28 10.177 511.03 122.12 0.0000 830.29 10.106 510.01 14084.2 0.1000 1.40065 +FS_2 Inlet.Fl_O 579.28 10.106 511.03 122.12 0.0000 836.15 9.689 504.91 5943.4 0.2459 1.40065 +FS_21 Fan.Fl_O 579.28 11.714 535.59 128.01 0.0000 738.49 11.050 526.73 4515.2 0.2900 1.40020 +FS_13 Splitter.Fl_O2 500.76 11.714 535.59 128.01 0.0000 638.39 11.009 526.17 3795.6 0.2991 1.40020 +FS_22 Splitter.Fl_O1 78.52 11.714 535.59 128.01 0.0000 100.10 11.242 529.33 719.5 0.2430 1.40020 +FS_23 Duct1.Fl_O 78.52 11.685 535.59 128.01 0.0000 100.35 11.214 529.33 721.3 0.2430 1.40020 +FS_24 LPC.Fl_O 78.52 16.011 596.12 142.54 0.0000 77.26 14.420 578.60 366.0 0.3895 1.39910 +FS_25 Duct2.Fl_O 78.52 15.971 596.12 142.54 0.0000 77.46 14.384 578.60 366.9 0.3895 1.39910 +FS_3 HPC.Fl_O 78.52 73.806 969.12 233.32 0.0000 21.37 68.763 950.30 119.9 0.3214 1.38263 +FS_36 Bld3.Fl_O 71.45 73.806 969.12 233.32 0.0000 19.45 68.763 950.30 109.1 0.3214 1.38263 +FS_4 Burner.Fl_O 72.20 69.746 1675.47 420.57 0.0105 27.34 69.299 1672.77 483.4 0.0983 1.33411 +FS_45 HPT.Fl_O 79.26 24.873 1278.03 313.95 0.0095 73.51 23.387 1257.48 439.1 0.3024 1.35654 +FS_48 Duct3.Fl_O 79.26 24.749 1278.03 313.95 0.0095 73.88 23.270 1257.48 441.4 0.3024 1.35654 +FS_5 LPT.Fl_O 79.26 10.950 1054.64 256.52 0.0095 151.70 10.714 1048.46 1477.4 0.1783 1.37076 +FS_7 Duct4.Fl_O 79.26 10.840 1054.64 256.52 0.0095 153.23 10.714 1051.32 2018.9 0.1307 1.37076 +FS_9 Core_Nozz.Fl_O 79.26 10.840 1054.64 256.52 0.0095 153.23 10.106 1034.78 862.8 0.3214 1.37076 +FS_15 BypBld.Fl_O 500.76 11.714 535.59 128.01 0.0000 638.39 11.009 526.17 3795.6 0.2991 1.40020 +FS_17 Duct5.Fl_O 500.76 11.626 535.59 128.01 0.0000 643.22 10.926 526.17 3824.3 0.2991 1.40020 +FS_19 Byp_Nozz.Fl_O 500.76 11.626 535.59 128.01 0.0000 643.22 10.106 514.55 2706.4 0.4519 1.40020 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 836.15 1.159 0.8976 2038.051 1.0481 0.8998 -4826.1 37.47 8.84 +LPC 100.35 1.370 0.8329 1990.772 1.1130 0.8402 -1614.5 42.54 12.85 +HPC 77.46 4.621 0.8626 6167.468 1.6257 0.8881 -10084.3 35.78 36.15 +HPT 27.34 2.804 0.9163 161.533 1.2697 0.9053 10084.7 +LPT 73.88 2.260 0.8941 56.588 1.2118 0.8833 6440.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1603.19 1.111 0.9273 0.517 1.6913 0.5215 1.4369 0.9679 3943.9586 +LPC 107.64 1.113 0.8676 0.544 1.8312 0.9323 3.2631 0.9600 3662.6571 +HPC 184.14 17.741 0.8510 0.970 2.2281 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.246 0.9347 105.500 5.2461 1.4085 0.4249 0.9803 1.5311 +LPT 153.52 2.758 0.8930 69.765 2.7580 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9930 14084.18 1993.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 727.90 174.32 24.443 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 727.90 174.32 24.443 +Duct1 0.0025 0.2430 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 727.90 174.32 24.443 +Duct2 0.0025 0.3895 365.99 +Duct3 0.0050 0.3024 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1783 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.7480 969.12 233.32 73.806 +Duct5 0.0075 0.2991 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.3184 969.12 233.32 73.806 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 535.59 128.01 11.714 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.3779 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6612.0 8010.6 10084.7 +LP_Shaft 2023.0 16720.4 6440.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1675.47 0.9940 0.0550 0.74846 0.01048 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.150 0.9975 1.0000 0.9975 2706.36 0.452 501.3 7802.8 +Core_Nozz 1.073 0.9999 1.0000 0.9999 862.88 0.321 501.7 1236.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 139 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 10000.0 27.00 1182.66 32557.3 0.4411 14361.50 4.9886 221.47 22.922 2709.1 2640.5 2126.1 + core size:19.85 Q: 40.77 Maximum Thrust: 32557.3 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1182.66 10.392 514.10 122.86 0.0000 1665.04 10.106 510.01 14377.3 0.2000 1.40060 +FS_2 Inlet.Fl_O 1182.66 10.330 514.10 122.86 0.0000 1675.10 8.246 481.99 5943.4 0.5764 1.40060 +FS_21 Fan.Fl_O 1182.66 17.139 605.78 144.86 0.0000 1095.92 14.781 580.73 4515.2 0.4649 1.39895 +FS_13 Splitter.Fl_O2 985.18 17.139 605.78 144.86 0.0000 912.92 14.832 581.30 3795.6 0.4593 1.39895 +FS_22 Splitter.Fl_O1 197.48 17.139 605.78 144.86 0.0000 183.00 14.494 577.49 719.5 0.4953 1.39895 +FS_23 Duct1.Fl_O 197.48 17.096 605.78 144.86 0.0000 183.46 14.458 577.49 721.3 0.4953 1.39895 +FS_24 LPC.Fl_O 197.48 42.367 810.45 194.36 0.0000 85.63 37.023 780.24 366.0 0.4442 1.39144 +FS_25 Duct2.Fl_O 197.48 42.262 810.45 194.36 0.0000 85.84 36.931 780.24 366.9 0.4442 1.39144 +FS_3 HPC.Fl_O 197.48 238.211 1376.75 336.84 0.0000 19.85 224.315 1355.11 119.9 0.2986 1.35726 +FS_36 Bld3.Fl_O 179.71 238.211 1376.75 336.84 0.0000 18.06 224.315 1355.11 109.1 0.2986 1.35726 +FS_4 Burner.Fl_O 183.70 225.109 2709.12 726.83 0.0222 27.41 223.657 2705.13 483.4 0.1000 1.29420 +FS_45 HPT.Fl_O 201.47 84.517 2126.11 552.77 0.0202 70.93 79.831 2097.59 439.1 0.2960 1.30977 +FS_48 Duct3.Fl_O 201.47 84.095 2126.11 552.77 0.0202 71.28 79.431 2097.59 441.4 0.2960 1.30977 +FS_5 LPT.Fl_O 201.47 17.484 1494.83 375.06 0.0202 287.49 16.031 1462.44 1477.4 0.3621 1.33667 +FS_7 Duct4.Fl_O 201.47 17.309 1494.83 375.06 0.0202 290.39 16.560 1478.24 2018.9 0.2580 1.33667 +FS_9 Core_Nozz.Fl_O 201.47 17.309 1494.83 375.06 0.0202 290.39 10.106 1303.24 862.9 0.9250 1.33667 +FS_15 BypBld.Fl_O 985.18 17.139 605.78 144.86 0.0000 912.92 14.832 581.30 3795.6 0.4593 1.39895 +FS_17 Duct5.Fl_O 985.18 17.011 605.78 144.86 0.0000 919.82 14.721 581.30 3824.3 0.4593 1.39895 +FS_19 Byp_Nozz.Fl_O 985.18 17.011 605.78 144.86 0.0000 919.82 10.106 522.06 2706.4 0.8955 1.39895 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.10 1.659 0.8727 3944.235 1.1783 0.8815 -36826.4 23.84 16.63 +LPC 183.46 2.478 0.8686 3633.513 1.3379 0.8841 -13829.8 28.77 23.62 +HPC 85.84 5.637 0.8647 6333.255 1.6988 0.8918 -39811.8 19.81 19.84 +HPT 27.41 2.663 0.9136 152.100 1.2267 0.9043 39811.8 +LPT 71.28 4.810 0.9331 85.162 1.4223 0.9195 50656.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.78 1.459 0.9016 1.000 2.3039 0.5215 1.4369 0.9679 3943.9586 +LPC 196.78 1.453 0.9048 0.992 1.7763 0.9323 3.2631 0.9600 3662.6571 +HPC 204.08 22.434 0.8531 0.996 2.0413 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.915 0.9320 99.339 4.9152 1.4085 0.4249 0.9803 1.5311 +LPT 148.12 6.314 0.9319 104.994 6.3145 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 14377.27 8140.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1013.04 244.23 70.968 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1013.04 244.23 70.968 +Duct1 0.0025 0.4953 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1013.04 244.23 70.968 +Duct2 0.0025 0.4442 365.99 +Duct3 0.0050 0.2960 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3621 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.9120 1376.75 336.84 238.211 +Duct5 0.0075 0.4593 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.8617 1376.75 336.84 238.211 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 605.78 144.86 17.139 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 4.9886 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7916.7 26412.1 39811.8 +LP_Shaft 3926.8 67752.9 50656.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2709.12 0.9940 0.0550 3.98930 0.02220 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.683 0.9975 1.0000 0.9975 2706.36 0.896 1000.7 30641.9 +Core_Nozz 1.713 0.9999 1.0000 0.9999 862.88 0.925 1605.9 10056.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 140 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 10000.0 27.00 1139.31 29301.7 0.4257 12472.81 5.2651 221.47 20.667 2602.6 2536.9 2033.9 + core size:19.94 Q: 40.77 Maximum Thrust: 32557.3 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1139.31 10.392 514.10 122.86 0.0000 1604.01 10.106 510.01 13850.3 0.2000 1.40060 +FS_2 Inlet.Fl_O 1139.31 10.330 514.10 122.86 0.0000 1613.71 8.445 485.31 5943.4 0.5440 1.40060 +FS_21 Fan.Fl_O 1139.31 16.642 597.49 142.87 0.0000 1079.83 14.432 573.68 4515.2 0.4558 1.39908 +FS_13 Splitter.Fl_O2 957.46 16.642 597.49 142.87 0.0000 907.47 14.434 573.70 3795.6 0.4557 1.39908 +FS_22 Splitter.Fl_O1 181.85 16.642 597.49 142.87 0.0000 172.36 14.424 573.59 719.5 0.4568 1.39908 +FS_23 Duct1.Fl_O 181.85 16.600 597.49 142.87 0.0000 172.79 14.387 573.59 721.3 0.4568 1.39908 +FS_24 LPC.Fl_O 181.85 37.923 779.82 186.91 0.0000 86.41 33.036 750.02 366.0 0.4492 1.39292 +FS_25 Duct2.Fl_O 181.85 37.828 779.82 186.91 0.0000 86.63 32.953 750.02 366.9 0.4492 1.39292 +FS_3 HPC.Fl_O 181.85 214.776 1331.87 325.19 0.0000 19.94 202.127 1310.62 119.9 0.2998 1.35995 +FS_36 Bld3.Fl_O 165.48 214.776 1331.87 325.19 0.0000 18.14 202.127 1310.62 109.1 0.2998 1.35995 +FS_4 Burner.Fl_O 168.95 202.963 2602.56 693.70 0.0209 27.40 201.655 2598.70 483.4 0.0999 1.29720 +FS_45 HPT.Fl_O 185.31 75.264 2033.87 525.46 0.0191 71.65 70.999 2005.72 439.1 0.2989 1.31355 +FS_48 Duct3.Fl_O 185.31 74.888 2033.87 525.46 0.0191 72.01 70.644 2005.72 441.4 0.2989 1.31355 +FS_5 LPT.Fl_O 185.31 16.042 1437.73 359.20 0.0191 282.65 14.758 1407.53 1477.4 0.3544 1.34057 +FS_7 Duct4.Fl_O 185.31 15.881 1437.73 359.20 0.0191 285.50 15.218 1422.22 2018.9 0.2529 1.34057 +FS_9 Core_Nozz.Fl_O 185.31 15.881 1437.73 359.20 0.0191 285.50 10.106 1280.25 862.9 0.8426 1.34057 +FS_15 BypBld.Fl_O 957.46 16.642 597.49 142.87 0.0000 907.47 14.434 573.70 3795.6 0.4557 1.39908 +FS_17 Duct5.Fl_O 957.46 16.517 597.49 142.87 0.0000 914.33 14.325 573.70 3824.3 0.4557 1.39908 +FS_19 Byp_Nozz.Fl_O 957.46 16.517 597.49 142.87 0.0000 914.33 10.106 519.24 2706.4 0.8680 1.39908 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1613.71 1.611 0.9000 3701.040 1.1622 0.9065 -32262.9 27.70 16.69 +LPC 172.79 2.284 0.8662 3433.062 1.3052 0.8807 -11330.4 29.79 22.57 +HPC 86.63 5.678 0.8627 6354.949 1.7079 0.8904 -35578.4 19.93 19.90 +HPT 27.40 2.697 0.9142 152.744 1.2322 0.9044 35578.2 +LPT 72.01 4.668 0.9287 81.703 1.4146 0.9144 43593.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3094.06 1.425 0.9298 0.938 2.0673 0.5215 1.4369 0.9679 3943.9586 +LPC 185.34 1.394 0.9023 0.937 1.7691 0.9323 3.2631 0.9600 3662.6571 +HPC 205.94 22.624 0.8511 1.000 2.0747 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.993 0.9325 99.760 4.9933 1.4085 0.4249 0.9803 1.5311 +LPT 149.64 6.117 0.9275 100.730 6.1172 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 13850.29 7842.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 977.13 235.31 63.751 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 977.13 235.31 63.751 +Duct1 0.0025 0.4568 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 977.13 235.31 63.751 +Duct2 0.0025 0.4492 365.99 +Duct3 0.0050 0.2989 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3544 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.3647 1331.87 325.19 214.776 +Duct5 0.0075 0.4557 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.0017 1331.87 325.19 214.776 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 597.49 142.87 16.642 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.2651 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7792.3 23980.2 35578.2 +LP_Shaft 3684.7 62137.5 43593.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2602.56 0.9940 0.0550 3.46467 0.02094 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.634 0.9975 1.0000 0.9975 2706.36 0.868 967.3 28786.1 +Core_Nozz 1.571 0.9999 1.0000 0.9999 862.88 0.843 1451.1 8357.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 141 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 10000.0 27.00 1088.59 26046.2 0.4168 10856.37 5.4481 221.47 18.778 2498.1 2435.6 1947.7 + core size:20.08 Q: 40.77 Maximum Thrust: 32557.3 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1088.59 10.392 514.10 122.86 0.0000 1532.60 10.106 510.01 13233.7 0.2000 1.40060 +FS_2 Inlet.Fl_O 1088.59 10.330 514.10 122.86 0.0000 1541.86 8.655 488.72 5943.4 0.5090 1.40060 +FS_21 Fan.Fl_O 1088.59 16.045 590.01 141.07 0.0000 1063.39 13.991 567.39 4515.2 0.4468 1.39920 +FS_13 Splitter.Fl_O2 919.77 16.045 590.01 141.07 0.0000 898.48 13.966 567.10 3795.6 0.4497 1.39920 +FS_22 Splitter.Fl_O1 168.82 16.045 590.01 141.07 0.0000 164.92 14.119 568.86 719.5 0.4314 1.39920 +FS_23 Duct1.Fl_O 168.82 16.005 590.01 141.07 0.0000 165.33 14.084 568.86 721.3 0.4314 1.39920 +FS_24 LPC.Fl_O 168.82 35.096 760.83 182.30 0.0000 85.62 30.671 732.38 366.0 0.4438 1.39380 +FS_25 Duct2.Fl_O 168.82 35.008 760.83 182.30 0.0000 85.83 30.594 732.38 366.9 0.4438 1.39380 +FS_3 HPC.Fl_O 168.82 195.143 1293.77 315.35 0.0000 20.08 183.476 1272.71 119.9 0.3019 1.36228 +FS_36 Bld3.Fl_O 153.63 195.143 1293.77 315.35 0.0000 18.27 183.476 1272.71 109.1 0.3019 1.36228 +FS_4 Burner.Fl_O 156.64 184.410 2498.08 661.48 0.0196 27.40 183.222 2494.35 483.4 0.0997 1.30042 +FS_45 HPT.Fl_O 171.84 68.059 1947.72 500.17 0.0179 71.90 64.174 1920.30 439.1 0.2996 1.31745 +FS_48 Duct3.Fl_O 171.84 67.718 1947.72 500.17 0.0179 72.27 63.853 1920.30 441.4 0.2996 1.31745 +FS_5 LPT.Fl_O 171.84 14.980 1383.55 344.26 0.0179 275.33 13.849 1355.95 1477.4 0.3432 1.34451 +FS_7 Duct4.Fl_O 171.84 14.830 1383.55 344.26 0.0179 278.11 14.244 1369.31 2018.9 0.2455 1.34451 +FS_9 Core_Nozz.Fl_O 171.84 14.830 1383.55 344.26 0.0179 278.11 10.106 1252.95 862.9 0.7722 1.34451 +FS_15 BypBld.Fl_O 919.77 16.045 590.01 141.07 0.0000 898.48 13.966 567.10 3795.6 0.4497 1.39920 +FS_17 Duct5.Fl_O 919.77 15.925 590.01 141.07 0.0000 905.27 13.862 567.10 3824.3 0.4497 1.39920 +FS_19 Byp_Nozz.Fl_O 919.77 15.925 590.01 141.07 0.0000 905.27 10.106 518.11 2706.4 0.8329 1.39920 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1541.86 1.553 0.9082 3546.521 1.1477 0.9138 -28059.1 31.39 16.88 +LPC 165.33 2.193 0.8634 3310.511 1.2895 0.8774 -9846.3 29.21 20.84 +HPC 85.83 5.574 0.8638 6332.102 1.7005 0.8910 -31780.3 21.36 21.39 +HPT 27.40 2.710 0.9145 153.442 1.2356 0.9046 31779.3 +LPT 72.27 4.521 0.9267 80.005 1.4078 0.9124 37905.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2956.09 1.385 0.9383 0.899 1.9656 0.5215 1.4369 0.9679 3943.9586 +LPC 177.33 1.366 0.8993 0.904 1.7373 0.9323 3.2631 0.9600 3662.6571 +HPC 204.06 22.146 0.8521 0.996 2.0970 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.024 0.9329 100.215 5.0236 1.4085 0.4249 0.9803 1.5311 +LPT 150.16 5.911 0.9255 98.636 5.9111 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 13233.68 7493.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 951.10 228.86 58.468 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 951.10 228.86 58.468 +Duct1 0.0025 0.4314 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 951.10 228.86 58.468 +Duct2 0.0025 0.4438 365.99 +Duct3 0.0050 0.2996 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3432 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.9088 1293.77 315.35 195.143 +Duct5 0.0075 0.4497 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.2853 1293.77 315.35 195.143 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 590.01 141.07 16.045 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.4481 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7669.1 21763.6 31779.3 +LP_Shaft 3530.8 56383.5 37905.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2498.08 0.9940 0.0550 3.01566 0.01963 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.576 0.9975 1.0000 0.9975 2706.36 0.833 927.2 26506.1 +Core_Nozz 1.467 0.9999 1.0000 0.9999 862.88 0.772 1316.8 7033.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 142 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 10000.0 27.00 970.65 19534.3 0.4083 7975.86 5.8335 221.47 15.093 2289.3 2233.1 1775.6 + core size:20.36 Q: 40.77 Maximum Thrust: 32557.3 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 970.65 10.392 514.10 122.86 0.0000 1366.55 10.106 510.01 11799.9 0.2000 1.40060 +FS_2 Inlet.Fl_O 970.65 10.330 514.10 122.86 0.0000 1374.81 9.063 495.20 5943.4 0.4363 1.40060 +FS_21 Fan.Fl_O 970.65 14.781 575.05 137.48 0.0000 1016.16 13.080 555.33 4515.2 0.4215 1.39944 +FS_13 Splitter.Fl_O2 828.60 14.781 575.05 137.48 0.0000 867.46 13.018 554.57 3795.6 0.4298 1.39944 +FS_22 Splitter.Fl_O1 142.04 14.781 575.05 137.48 0.0000 148.70 13.382 558.95 719.5 0.3796 1.39944 +FS_23 Duct1.Fl_O 142.04 14.744 575.05 137.48 0.0000 149.08 13.348 558.95 721.3 0.3796 1.39944 +FS_24 LPC.Fl_O 142.04 29.219 719.25 172.22 0.0000 84.13 25.685 693.44 366.0 0.4336 1.39537 +FS_25 Duct2.Fl_O 142.04 29.146 719.25 172.22 0.0000 84.34 25.621 693.44 366.9 0.4336 1.39537 +FS_3 HPC.Fl_O 142.04 156.847 1213.81 294.84 0.0000 20.36 147.189 1193.24 119.9 0.3060 1.36728 +FS_36 Bld3.Fl_O 129.26 156.847 1213.81 294.84 0.0000 18.53 147.189 1193.24 109.1 0.3060 1.36728 +FS_4 Burner.Fl_O 131.47 148.220 2289.29 598.16 0.0171 27.39 147.266 2285.81 483.4 0.0994 1.30729 +FS_45 HPT.Fl_O 144.26 54.169 1775.65 450.55 0.0156 72.41 51.031 1749.75 439.1 0.3010 1.32602 +FS_48 Duct3.Fl_O 144.26 53.898 1775.65 450.55 0.0156 72.78 50.776 1749.75 441.4 0.3010 1.32602 +FS_5 LPT.Fl_O 144.26 13.285 1286.91 317.95 0.0156 251.36 12.463 1265.66 1477.4 0.3085 1.35191 +FS_7 Duct4.Fl_O 144.26 13.152 1286.91 317.95 0.0156 253.90 12.723 1275.82 2018.9 0.2221 1.35191 +FS_9 Core_Nozz.Fl_O 144.26 13.152 1286.91 317.95 0.0156 253.90 10.106 1201.21 862.9 0.6337 1.35191 +FS_15 BypBld.Fl_O 828.60 14.781 575.05 137.48 0.0000 867.46 13.018 554.57 3795.6 0.4298 1.39944 +FS_17 Duct5.Fl_O 828.60 14.670 575.05 137.48 0.0000 874.01 12.921 554.57 3824.3 0.4298 1.39944 +FS_19 Byp_Nozz.Fl_O 828.60 14.670 575.05 137.48 0.0000 874.01 10.106 516.94 2706.4 0.7495 1.39944 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1374.81 1.431 0.9096 3198.129 1.1186 0.9141 -20083.4 37.17 16.54 +LPC 149.08 1.982 0.8570 3023.888 1.2508 0.8701 -6982.2 28.71 17.88 +HPC 84.34 5.381 0.8646 6295.358 1.6876 0.8913 -24641.8 24.14 24.25 +HPT 27.39 2.736 0.9148 154.941 1.2433 0.9047 24641.8 +LPT 72.78 4.057 0.9227 75.560 1.3798 0.9085 27065.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2636.00 1.300 0.9397 0.811 1.8683 0.5215 1.4369 0.9679 3943.9586 +LPC 159.91 1.301 0.8927 0.826 1.6930 0.9323 3.2631 0.9600 3662.6571 +HPC 200.51 21.254 0.8530 0.990 2.1367 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.087 0.9331 101.195 5.0865 1.4085 0.4249 0.9803 1.5311 +LPT 151.23 5.264 0.9215 93.156 5.2643 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 11799.86 6681.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 895.38 215.14 47.854 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 895.38 215.14 47.854 +Duct1 0.0025 0.3796 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 895.38 215.14 47.854 +Duct2 0.0025 0.4336 365.99 +Duct3 0.0050 0.3010 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3085 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.9715 1213.81 294.84 156.847 +Duct5 0.0075 0.4298 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.8124 1213.81 294.84 156.847 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 575.05 137.48 14.781 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.8335 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7413.4 17457.8 24641.8 +LP_Shaft 3184.0 44645.2 27065.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2289.29 0.9940 0.0550 2.21552 0.01714 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.452 0.9975 1.0000 0.9975 2706.36 0.749 833.4 21463.6 +Core_Nozz 1.301 0.9999 1.0000 0.9999 862.88 0.634 1059.9 4752.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 143 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 10000.0 27.00 826.09 13022.7 0.4128 5375.69 6.2498 221.47 11.423 2046.8 1997.9 1577.3 + core size:20.71 Q: 40.77 Maximum Thrust: 32557.3 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 826.09 10.392 514.10 122.86 0.0000 1163.04 10.106 510.01 10042.6 0.2000 1.40060 +FS_2 Inlet.Fl_O 826.09 10.330 514.10 122.86 0.0000 1170.07 9.453 501.21 5943.4 0.3582 1.40060 +FS_21 Fan.Fl_O 826.09 13.452 558.60 133.53 0.0000 936.57 12.168 542.82 4515.2 0.3812 1.39974 +FS_13 Splitter.Fl_O2 712.15 13.452 558.60 133.53 0.0000 807.38 12.093 541.86 3795.6 0.3930 1.39974 +FS_22 Splitter.Fl_O1 113.95 13.452 558.60 133.53 0.0000 129.18 12.519 547.25 719.5 0.3220 1.39974 +FS_23 Duct1.Fl_O 113.95 13.419 558.60 133.53 0.0000 129.51 12.488 547.25 721.3 0.3220 1.39974 +FS_24 LPC.Fl_O 113.95 23.212 669.82 160.28 0.0000 81.98 20.569 647.18 366.0 0.4194 1.39708 +FS_25 Duct2.Fl_O 113.95 23.153 669.82 160.28 0.0000 82.19 20.518 647.18 366.9 0.4194 1.39708 +FS_3 HPC.Fl_O 113.95 118.712 1117.97 270.52 0.0000 20.71 111.131 1098.07 119.9 0.3112 1.37331 +FS_36 Bld3.Fl_O 103.69 118.712 1117.97 270.52 0.0000 18.85 111.131 1098.07 109.1 0.3112 1.37331 +FS_4 Burner.Fl_O 105.18 112.183 2046.76 526.41 0.0144 27.37 111.462 2043.59 483.4 0.0990 1.31628 +FS_45 HPT.Fl_O 115.44 40.542 1577.28 394.86 0.0131 72.97 38.155 1553.30 439.1 0.3022 1.33709 +FS_48 Duct3.Fl_O 115.44 40.339 1577.28 394.86 0.0131 73.34 37.965 1553.30 441.4 0.3022 1.33709 +FS_5 LPT.Fl_O 115.44 12.006 1190.29 292.07 0.0131 214.05 11.479 1176.22 1477.4 0.2577 1.35969 +FS_7 Duct4.Fl_O 115.44 11.886 1190.29 292.07 0.0131 216.21 11.608 1182.84 2018.9 0.1871 1.35969 +FS_9 Core_Nozz.Fl_O 115.44 11.886 1190.29 292.07 0.0131 216.21 10.106 1140.17 863.0 0.4930 1.35969 +FS_15 BypBld.Fl_O 712.15 13.452 558.60 133.53 0.0000 807.38 12.093 541.86 3795.6 0.3930 1.39974 +FS_17 Duct5.Fl_O 712.15 13.351 558.60 133.53 0.0000 813.48 12.002 541.86 3824.3 0.3930 1.39974 +FS_19 Byp_Nozz.Fl_O 712.15 13.351 558.60 133.53 0.0000 813.48 10.106 515.85 2706.4 0.6435 1.39974 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1170.07 1.302 0.9060 2757.759 1.0866 0.9095 -12477.2 37.98 15.16 +LPC 129.51 1.730 0.8492 2645.615 1.1991 0.8604 -4312.4 30.57 15.16 +HPC 82.19 5.127 0.8646 6251.510 1.6691 0.8910 -17773.3 27.88 28.04 +HPT 27.37 2.767 0.9152 157.031 1.2531 0.9049 17773.3 +LPT 73.34 3.360 0.9130 69.132 1.3251 0.8993 16789.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2243.45 1.210 0.9360 0.699 1.8081 0.5215 1.4369 0.9679 3943.9586 +LPC 138.92 1.224 0.8846 0.722 1.6885 0.9323 3.2631 0.9600 3662.6571 +HPC 195.40 20.079 0.8529 0.983 2.1735 0.4206 0.2163 1.0137 6357.1603 +HPT 30.12 5.159 0.9336 102.559 5.1591 1.4085 0.4249 0.9803 1.5311 +LPT 152.39 4.292 0.9119 85.231 4.2918 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 10042.60 5686.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 828.92 198.86 37.153 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 828.92 198.86 37.153 +Duct1 0.0025 0.3220 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 828.92 198.86 37.153 +Duct2 0.0025 0.4194 365.99 +Duct3 0.0050 0.3022 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2577 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.9881 1117.97 270.52 118.712 +Duct5 0.0075 0.3930 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.2671 1117.97 270.52 118.712 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 558.60 133.53 13.452 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.2498 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7104.2 13139.7 17773.3 +LP_Shaft 2745.6 32116.6 16789.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2046.76 0.9940 0.0550 1.49325 0.01440 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.321 0.9975 1.0000 0.9975 2706.36 0.643 714.8 15820.8 +Core_Nozz 1.176 0.9999 1.0000 0.9999 862.88 0.493 805.0 2888.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:47 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 144 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.200 10000.0 27.00 635.39 6511.4 0.4522 2944.65 6.6700 221.47 7.585 1715.8 1676.9 1310.5 + core size:21.31 Q: 40.77 Maximum Thrust: 32557.3 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 635.39 10.392 514.10 122.86 0.0000 894.55 10.106 510.01 7724.2 0.2000 1.40060 +FS_2 Inlet.Fl_O 635.39 10.330 514.10 122.86 0.0000 899.96 9.833 506.89 5943.4 0.2663 1.40060 +FS_21 Fan.Fl_O 635.39 12.067 539.89 129.04 0.0000 789.49 11.277 529.54 4515.2 0.3125 1.40011 +FS_13 Splitter.Fl_O2 552.55 12.067 539.89 129.04 0.0000 686.56 11.216 528.73 3795.6 0.3247 1.40011 +FS_22 Splitter.Fl_O1 82.84 12.067 539.89 129.04 0.0000 102.93 11.552 533.19 719.5 0.2504 1.40011 +FS_23 Duct1.Fl_O 82.84 12.037 539.89 129.04 0.0000 103.19 11.523 533.19 721.3 0.2504 1.40011 +FS_24 LPC.Fl_O 82.84 16.976 606.68 145.08 0.0000 77.56 15.276 588.69 366.0 0.3914 1.39894 +FS_25 Duct2.Fl_O 82.84 16.934 606.68 145.08 0.0000 77.75 15.237 588.69 366.9 0.3914 1.39894 +FS_3 HPC.Fl_O 82.84 78.825 987.82 237.96 0.0000 21.31 73.470 968.79 119.9 0.3206 1.38147 +FS_36 Bld3.Fl_O 75.38 78.825 987.82 237.96 0.0000 19.40 73.470 968.79 109.1 0.3206 1.38147 +FS_4 Burner.Fl_O 76.20 74.490 1715.76 431.78 0.0109 27.34 74.011 1713.01 483.4 0.0984 1.33198 +FS_45 HPT.Fl_O 83.66 26.610 1310.53 322.54 0.0099 73.44 25.024 1289.59 439.1 0.3023 1.35429 +FS_48 Duct3.Fl_O 83.66 26.477 1310.53 322.54 0.0099 73.81 24.899 1289.59 441.4 0.3023 1.35429 +FS_5 LPT.Fl_O 83.66 11.044 1066.85 259.69 0.0099 159.65 10.781 1059.91 1477.4 0.1881 1.36975 +FS_7 Duct4.Fl_O 83.66 10.934 1066.85 259.69 0.0099 161.26 10.793 1063.12 2018.9 0.1377 1.36975 +FS_9 Core_Nozz.Fl_O 83.66 10.934 1066.85 259.69 0.0099 161.26 10.106 1044.35 862.9 0.3409 1.36975 +FS_15 BypBld.Fl_O 552.55 12.067 539.89 129.04 0.0000 686.56 11.216 528.73 3795.6 0.3247 1.40011 +FS_17 Duct5.Fl_O 552.55 11.976 539.89 129.04 0.0000 691.75 11.132 528.73 3824.3 0.3247 1.40011 +FS_19 Byp_Nozz.Fl_O 552.55 11.976 539.89 129.04 0.0000 691.75 10.106 514.30 2706.4 0.4985 1.40011 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 899.96 1.168 0.9060 2121.341 1.0502 0.9081 -5559.6 41.52 11.08 +LPC 103.19 1.410 0.8339 2070.049 1.1237 0.8418 -1880.1 39.85 12.73 +HPC 77.75 4.655 0.8629 6173.198 1.6282 0.8884 -10886.0 35.18 35.52 +HPT 27.34 2.799 0.9162 161.183 1.2676 0.9053 10886.2 +LPT 73.81 2.397 0.8964 58.340 1.2284 0.8851 7439.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1725.54 1.117 0.9360 0.538 1.7913 0.5215 1.4369 0.9679 3943.9586 +LPC 110.69 1.126 0.8687 0.565 1.7904 0.9323 3.2631 0.9600 3662.6571 +HPC 184.85 17.895 0.8512 0.971 2.2212 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.235 0.9346 105.271 5.2348 1.4085 0.4249 0.9803 1.5311 +LPT 153.37 2.949 0.8953 71.925 2.9492 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 7724.25 4373.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 741.42 177.59 26.001 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 741.42 177.59 26.001 +Duct1 0.0025 0.2504 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 741.42 177.59 26.001 +Duct2 0.0025 0.3914 365.99 +Duct3 0.0050 0.3023 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1881 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.8994 987.82 237.96 78.825 +Duct5 0.0075 0.3247 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.5562 987.82 237.96 78.825 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 539.89 129.04 12.067 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6700 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6676.5 8563.7 10886.2 +LP_Shaft 2112.0 18501.0 7439.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1715.76 0.9940 0.0550 0.81796 0.01085 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.185 0.9975 1.0000 0.9975 2706.36 0.498 552.9 9495.5 +Core_Nozz 1.082 0.9999 1.0000 0.9999 862.88 0.341 534.4 1389.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 145 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 10000.0 27.00 1198.57 31475.9 0.4628 14568.05 5.0005 276.83 22.859 2716.6 2647.9 2132.4 + core size:19.85 Q: 63.70 Maximum Thrust: 31475.9 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1198.57 10.556 516.39 123.41 0.0000 1665.05 10.106 510.01 11656.6 0.2500 1.40056 +FS_2 Inlet.Fl_O 1198.57 10.492 516.39 123.41 0.0000 1675.11 8.375 484.15 5943.4 0.5764 1.40056 +FS_21 Fan.Fl_O 1198.57 17.373 608.20 145.45 0.0000 1097.91 14.972 582.93 4515.2 0.4660 1.39891 +FS_13 Splitter.Fl_O2 998.83 17.373 608.20 145.45 0.0000 914.94 15.022 583.49 3795.6 0.4606 1.39891 +FS_22 Splitter.Fl_O1 199.74 17.373 608.20 145.45 0.0000 182.97 14.693 579.81 719.5 0.4952 1.39891 +FS_23 Duct1.Fl_O 199.74 17.330 608.20 145.45 0.0000 183.43 14.656 579.81 721.3 0.4952 1.39891 +FS_24 LPC.Fl_O 199.74 42.995 813.96 195.22 0.0000 85.53 37.586 783.72 366.0 0.4435 1.39128 +FS_25 Duct2.Fl_O 199.74 42.887 813.96 195.22 0.0000 85.74 37.493 783.72 366.9 0.4435 1.39128 +FS_3 HPC.Fl_O 199.74 241.291 1381.51 338.08 0.0000 19.85 227.208 1359.79 119.9 0.2987 1.35698 +FS_36 Bld3.Fl_O 181.77 241.291 1381.51 338.08 0.0000 18.07 227.208 1359.79 109.1 0.2987 1.35698 +FS_4 Burner.Fl_O 185.81 228.020 2716.61 729.15 0.0223 27.41 226.550 2712.62 483.4 0.1000 1.29402 +FS_45 HPT.Fl_O 203.79 85.632 2132.40 554.62 0.0203 70.91 80.885 2103.82 439.1 0.2960 1.30954 +FS_48 Duct3.Fl_O 203.79 85.204 2132.40 554.62 0.0203 71.27 80.481 2103.82 441.4 0.2960 1.30954 +FS_5 LPT.Fl_O 203.79 17.688 1499.02 376.22 0.0203 287.85 16.213 1466.47 1477.4 0.3627 1.33640 +FS_7 Duct4.Fl_O 203.79 17.511 1499.02 376.22 0.0203 290.76 16.751 1482.35 2018.9 0.2583 1.33640 +FS_9 Core_Nozz.Fl_O 203.79 17.511 1499.02 376.22 0.0203 290.76 10.106 1303.11 862.9 0.9356 1.33640 +FS_15 BypBld.Fl_O 998.83 17.373 608.20 145.45 0.0000 914.94 15.022 583.49 3795.6 0.4606 1.39891 +FS_17 Duct5.Fl_O 998.83 17.243 608.20 145.45 0.0000 921.85 14.909 583.49 3824.3 0.4606 1.39891 +FS_19 Byp_Nozz.Fl_O 998.83 17.243 608.20 145.45 0.0000 921.85 10.106 522.12 2706.4 0.9080 1.39891 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.656 0.8716 3944.235 1.1778 0.8804 -37374.4 24.04 16.82 +LPC 183.43 2.481 0.8686 3634.373 1.3383 0.8841 -14065.4 28.66 23.52 +HPC 85.74 5.626 0.8649 6330.600 1.6973 0.8919 -40375.8 19.92 19.96 +HPT 27.41 2.663 0.9137 152.155 1.2265 0.9043 40375.8 +LPT 71.27 4.817 0.9331 85.226 1.4225 0.9195 51439.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.456 0.9005 1.000 2.3196 0.5215 1.4369 0.9679 3943.9586 +LPC 196.75 1.454 0.9047 0.992 1.7735 0.9323 3.2631 0.9600 3662.6571 +HPC 203.84 22.386 0.8532 0.996 2.0421 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.914 0.9320 99.375 4.9136 1.4085 0.4249 0.9803 1.5311 +LPT 148.10 6.325 0.9319 105.073 6.3248 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 11656.57 10312.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1017.01 245.22 71.954 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1017.01 245.22 71.954 +Duct1 0.0025 0.4952 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1017.01 245.22 71.954 +Duct2 0.0025 0.4435 365.99 +Duct3 0.0050 0.2960 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3627 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.9911 1381.51 338.08 241.291 +Duct5 0.0075 0.4606 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.9860 1381.51 338.08 241.291 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 608.20 145.45 17.373 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0005 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7930.5 26739.6 40375.8 +LP_Shaft 3935.6 68647.6 51439.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2716.61 0.9940 0.0550 4.04668 0.02226 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.706 0.9975 1.0000 0.9975 2706.36 0.908 1014.7 31500.9 +Core_Nozz 1.733 0.9999 1.0000 0.9999 862.88 0.936 1624.2 10287.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 146 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 10000.0 27.00 1156.73 28327.5 0.4477 12681.80 5.2774 276.83 20.652 2610.9 2545.1 2041.0 + core size:19.95 Q: 63.70 Maximum Thrust: 31475.9 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1156.73 10.556 516.39 123.41 0.0000 1606.92 10.106 510.01 11249.7 0.2500 1.40056 +FS_2 Inlet.Fl_O 1156.73 10.492 516.39 123.41 0.0000 1616.63 8.569 487.33 5943.4 0.5455 1.40056 +FS_21 Fan.Fl_O 1156.73 16.885 600.04 143.48 0.0000 1082.85 14.628 575.96 4515.2 0.4575 1.39904 +FS_13 Splitter.Fl_O2 972.46 16.885 600.04 143.48 0.0000 910.35 14.627 575.96 3795.6 0.4576 1.39904 +FS_22 Splitter.Fl_O1 184.27 16.885 600.04 143.48 0.0000 172.50 14.630 575.98 719.5 0.4573 1.39904 +FS_23 Duct1.Fl_O 184.27 16.843 600.04 143.48 0.0000 172.93 14.593 575.98 721.3 0.4573 1.39904 +FS_24 LPC.Fl_O 184.27 38.582 783.80 187.87 0.0000 86.28 33.627 753.96 366.0 0.4484 1.39273 +FS_25 Duct2.Fl_O 184.27 38.485 783.80 187.87 0.0000 86.50 33.543 753.96 366.9 0.4484 1.39273 +FS_3 HPC.Fl_O 184.27 217.990 1337.16 326.56 0.0000 19.95 205.142 1315.82 119.9 0.3000 1.35963 +FS_36 Bld3.Fl_O 167.69 217.990 1337.16 326.56 0.0000 18.15 205.142 1315.82 109.1 0.3000 1.35963 +FS_4 Burner.Fl_O 171.21 206.000 2610.94 696.27 0.0210 27.40 204.672 2607.08 483.4 0.0999 1.29697 +FS_45 HPT.Fl_O 187.79 76.429 2040.96 527.54 0.0191 71.63 72.102 2012.75 439.1 0.2989 1.31327 +FS_48 Duct3.Fl_O 187.79 76.047 2040.96 527.54 0.0191 71.99 71.741 2012.75 441.4 0.2989 1.31327 +FS_5 LPT.Fl_O 187.79 16.225 1441.80 360.32 0.0191 283.59 14.917 1411.30 1477.4 0.3558 1.34030 +FS_7 Duct4.Fl_O 187.79 16.063 1441.80 360.32 0.0191 286.45 15.387 1426.14 2018.9 0.2538 1.34030 +FS_9 Core_Nozz.Fl_O 187.79 16.063 1441.80 360.32 0.0191 286.45 10.106 1280.18 862.9 0.8538 1.34030 +FS_15 BypBld.Fl_O 972.46 16.885 600.04 143.48 0.0000 910.35 14.627 575.96 3795.6 0.4576 1.39904 +FS_17 Duct5.Fl_O 972.46 16.758 600.04 143.48 0.0000 917.23 14.518 575.96 3824.3 0.4576 1.39904 +FS_19 Byp_Nozz.Fl_O 972.46 16.758 600.04 143.48 0.0000 917.23 10.106 519.31 2706.4 0.8816 1.39904 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1616.63 1.609 0.8990 3705.603 1.1620 0.9056 -32857.1 27.90 16.92 +LPC 172.93 2.291 0.8662 3437.645 1.3063 0.8806 -11573.2 29.64 22.48 +HPC 86.50 5.664 0.8630 6351.027 1.7060 0.8906 -36157.6 20.07 20.06 +HPT 27.40 2.695 0.9142 152.792 1.2319 0.9045 36158.4 +LPT 71.99 4.687 0.9287 81.844 1.4156 0.9144 44429.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3099.75 1.424 0.9288 0.940 2.0862 0.5215 1.4369 0.9679 3943.9586 +LPC 185.50 1.396 0.9022 0.939 1.7660 0.9323 3.2631 0.9600 3662.6571 +HPC 205.63 22.562 0.8514 0.999 2.0750 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.990 0.9325 99.791 4.9901 1.4085 0.4249 0.9803 1.5311 +LPT 149.58 6.143 0.9275 100.903 6.1432 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 11249.65 9952.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 981.59 236.41 64.783 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 981.59 236.41 64.783 +Duct1 0.0025 0.4573 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 981.59 236.41 64.783 +Duct2 0.0025 0.4484 365.99 +Duct3 0.0050 0.2989 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3558 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.4494 1337.16 326.56 217.990 +Duct5 0.0075 0.4576 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.1348 1337.16 326.56 217.990 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 600.04 143.48 16.885 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.2774 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7807.3 24324.4 36158.4 +LP_Shaft 3697.5 63110.8 44429.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2610.94 0.9940 0.0550 3.52272 0.02101 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.658 0.9975 1.0000 0.9975 2706.36 0.882 982.6 29698.7 +Core_Nozz 1.589 0.9999 1.0000 0.9999 862.88 0.854 1470.3 8581.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 147 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 10000.0 27.00 1107.58 25180.6 0.4393 11061.21 5.4645 276.83 18.797 2507.3 2444.7 1955.4 + core size:20.09 Q: 63.70 Maximum Thrust: 31475.9 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1107.58 10.556 516.39 123.41 0.0000 1538.64 10.106 510.01 10771.7 0.2500 1.40056 +FS_2 Inlet.Fl_O 1107.58 10.492 516.39 123.41 0.0000 1547.94 8.774 490.63 5943.4 0.5119 1.40056 +FS_21 Fan.Fl_O 1107.58 16.295 592.64 141.70 0.0000 1067.77 14.188 569.68 4515.2 0.4492 1.39916 +FS_13 Splitter.Fl_O2 936.25 16.295 592.64 141.70 0.0000 902.59 14.160 569.36 3795.6 0.4524 1.39916 +FS_22 Splitter.Fl_O1 171.33 16.295 592.64 141.70 0.0000 165.17 14.331 571.31 719.5 0.4323 1.39916 +FS_23 Duct1.Fl_O 171.33 16.254 592.64 141.70 0.0000 165.59 14.295 571.31 721.3 0.4323 1.39916 +FS_24 LPC.Fl_O 171.33 35.765 765.04 183.32 0.0000 85.50 31.271 736.53 366.0 0.4430 1.39362 +FS_25 Duct2.Fl_O 171.33 35.676 765.04 183.32 0.0000 85.72 31.192 736.53 366.9 0.4430 1.39362 +FS_3 HPC.Fl_O 171.33 198.417 1299.55 316.84 0.0000 20.09 186.546 1278.39 119.9 0.3021 1.36192 +FS_36 Bld3.Fl_O 155.91 198.417 1299.55 316.84 0.0000 18.28 186.546 1278.39 109.1 0.3021 1.36192 +FS_4 Burner.Fl_O 158.99 187.505 2507.30 664.28 0.0197 27.40 186.296 2503.56 483.4 0.0997 1.30016 +FS_45 HPT.Fl_O 174.41 69.229 1955.42 502.40 0.0179 71.89 65.279 1927.92 439.1 0.2996 1.31712 +FS_48 Duct3.Fl_O 174.41 68.883 1955.42 502.40 0.0179 72.25 64.953 1927.92 441.4 0.2996 1.31712 +FS_5 LPT.Fl_O 174.41 15.145 1387.40 345.31 0.0179 276.79 13.988 1359.41 1477.4 0.3454 1.34423 +FS_7 Duct4.Fl_O 174.41 14.993 1387.40 345.31 0.0179 279.59 14.394 1372.98 2018.9 0.2469 1.34423 +FS_9 Core_Nozz.Fl_O 174.41 14.993 1387.40 345.31 0.0179 279.59 10.106 1252.94 862.9 0.7837 1.34423 +FS_15 BypBld.Fl_O 936.25 16.295 592.64 141.70 0.0000 902.59 14.160 569.36 3795.6 0.4524 1.39916 +FS_17 Duct5.Fl_O 936.25 16.172 592.64 141.70 0.0000 909.41 14.054 569.36 3824.3 0.4524 1.39916 +FS_19 Byp_Nozz.Fl_O 936.25 16.172 592.64 141.70 0.0000 909.41 10.106 518.13 2706.3 0.8478 1.39916 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1547.94 1.553 0.9079 3553.740 1.1476 0.9135 -28674.5 31.62 17.17 +LPC 165.59 2.200 0.8633 3317.280 1.2909 0.8774 -10087.0 29.05 20.78 +HPC 85.72 5.562 0.8640 6328.889 1.6987 0.8911 -32366.7 21.49 21.54 +HPT 27.40 2.708 0.9145 153.504 1.2354 0.9046 32366.6 +LPT 72.25 4.548 0.9268 80.188 1.4094 0.9124 38761.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2967.83 1.385 0.9380 0.901 1.9858 0.5215 1.4369 0.9679 3943.9586 +LPC 177.61 1.368 0.8993 0.906 1.7341 0.9323 3.2631 0.9600 3662.6571 +HPC 203.77 22.088 0.8523 0.996 2.0975 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.021 0.9329 100.256 5.0211 1.4085 0.4249 0.9803 1.5311 +LPT 150.12 5.950 0.9256 98.862 5.9498 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 10771.67 9529.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 955.89 230.05 59.517 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 955.89 230.05 59.517 +Duct1 0.0025 0.4323 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 955.89 230.05 59.517 +Duct2 0.0025 0.4430 365.99 +Duct3 0.0050 0.2996 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3454 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.9967 1299.55 316.84 198.417 +Duct5 0.0075 0.4524 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.4233 1299.55 316.84 198.417 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 592.64 141.70 16.295 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.4645 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7686.4 22116.1 32366.6 +LP_Shaft 3545.9 57412.1 38761.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2507.30 0.9940 0.0550 3.07256 0.01971 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.600 0.9975 1.0000 0.9975 2706.36 0.848 943.9 27466.1 +Core_Nozz 1.484 0.9999 1.0000 0.9999 862.88 0.784 1336.4 7244.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 148 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 10000.0 27.00 993.08 18885.4 0.4324 8166.25 5.8633 276.83 15.174 2300.2 2243.8 1784.9 + core size:20.37 Q: 63.70 Maximum Thrust: 31475.9 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 993.08 10.556 516.39 123.41 0.0000 1379.57 10.106 510.01 9658.0 0.2500 1.40056 +FS_2 Inlet.Fl_O 993.08 10.492 516.39 123.41 0.0000 1387.91 9.176 496.97 5943.4 0.4416 1.40056 +FS_21 Fan.Fl_O 993.08 15.034 577.77 138.13 0.0000 1024.54 13.271 557.55 4515.2 0.4259 1.39940 +FS_13 Splitter.Fl_O2 848.38 15.034 577.77 138.13 0.0000 875.27 13.203 556.74 3795.6 0.4348 1.39940 +FS_22 Splitter.Fl_O1 144.69 15.034 577.77 138.13 0.0000 149.28 13.599 561.45 719.5 0.3814 1.39940 +FS_23 Duct1.Fl_O 144.69 14.997 577.77 138.13 0.0000 149.65 13.565 561.45 721.3 0.3814 1.39940 +FS_24 LPC.Fl_O 144.69 29.936 724.34 173.45 0.0000 83.94 26.334 698.49 366.0 0.4324 1.39521 +FS_25 Duct2.Fl_O 144.69 29.861 724.34 173.45 0.0000 84.15 26.269 698.49 366.9 0.4324 1.39521 +FS_3 HPC.Fl_O 144.69 160.171 1220.69 296.59 0.0000 20.37 150.301 1200.00 119.9 0.3062 1.36684 +FS_36 Bld3.Fl_O 131.67 160.171 1220.69 296.59 0.0000 18.53 150.301 1200.00 109.1 0.3062 1.36684 +FS_4 Burner.Fl_O 133.94 151.361 2300.22 601.42 0.0172 27.39 150.387 2296.73 483.4 0.0994 1.30693 +FS_45 HPT.Fl_O 146.96 55.359 1784.88 453.17 0.0157 72.37 52.156 1758.91 439.1 0.3008 1.32556 +FS_48 Duct3.Fl_O 146.96 55.082 1784.88 453.17 0.0157 72.74 51.895 1758.91 441.4 0.3008 1.32556 +FS_5 LPT.Fl_O 146.96 13.414 1290.37 318.88 0.0157 253.96 12.565 1268.59 1477.4 0.3121 1.35164 +FS_7 Duct4.Fl_O 146.96 13.280 1290.37 318.88 0.0157 256.52 12.836 1279.02 2018.9 0.2246 1.35164 +FS_9 Core_Nozz.Fl_O 146.96 13.280 1290.37 318.88 0.0157 256.52 10.106 1201.44 862.9 0.6456 1.35164 +FS_15 BypBld.Fl_O 848.38 15.034 577.77 138.13 0.0000 875.27 13.203 556.74 3795.6 0.4348 1.39940 +FS_17 Duct5.Fl_O 848.38 14.921 577.77 138.13 0.0000 881.88 13.104 556.74 3824.3 0.4348 1.39940 +FS_19 Byp_Nozz.Fl_O 848.38 14.921 577.77 138.13 0.0000 881.88 10.106 516.88 2706.4 0.7673 1.39940 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1387.91 1.433 0.9111 3215.050 1.1189 0.9155 -20691.2 37.82 17.03 +LPC 149.65 1.996 0.8569 3039.496 1.2537 0.8700 -7230.6 28.38 17.78 +HPC 84.15 5.364 0.8648 6291.233 1.6853 0.8913 -25209.0 24.33 24.43 +HPT 27.39 2.734 0.9148 155.016 1.2428 0.9048 25208.9 +LPT 72.74 4.106 0.9227 75.932 1.3832 0.9085 27921.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2661.12 1.301 0.9412 0.815 1.8924 0.5215 1.4369 0.9679 3943.9586 +LPC 160.52 1.305 0.8926 0.830 1.6865 0.9323 3.2631 0.9600 3662.6571 +HPC 200.06 21.173 0.8531 0.990 2.1361 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.082 0.9332 101.243 5.0816 1.4085 0.4249 0.9803 1.5311 +LPT 151.14 5.333 0.9215 93.615 5.3333 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 9658.03 8544.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 901.13 216.55 48.951 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 901.13 216.55 48.951 +Duct1 0.0025 0.3814 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 901.13 216.55 48.951 +Duct2 0.0025 0.4324 365.99 +Duct3 0.0050 0.3008 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3121 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.0642 1220.69 296.59 160.171 +Duct5 0.0075 0.4348 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.9581 1220.69 296.59 160.171 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 577.77 138.13 15.034 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.8633 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7434.6 17808.5 25208.9 +LP_Shaft 3208.0 45712.9 27921.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2300.22 0.9940 0.0550 2.26840 0.01723 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.476 0.9975 1.0000 0.9975 2706.36 0.767 853.2 22497.6 +Core_Nozz 1.314 0.9999 1.0000 0.9999 862.88 0.646 1079.9 4932.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 149 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 10000.0 27.00 852.71 12590.3 0.4401 5541.28 6.3156 276.83 11.544 2060.4 2011.3 1588.7 + core size:20.71 Q: 63.70 Maximum Thrust: 31475.9 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 852.71 10.556 516.39 123.41 0.0000 1184.57 10.106 510.01 8292.9 0.2500 1.40056 +FS_2 Inlet.Fl_O 852.71 10.492 516.39 123.41 0.0000 1191.73 9.564 502.90 5943.4 0.3660 1.40056 +FS_21 Fan.Fl_O 852.71 13.700 561.42 134.21 0.0000 951.65 12.344 544.95 4515.2 0.3887 1.39969 +FS_13 Splitter.Fl_O2 736.15 13.700 561.42 134.21 0.0000 821.56 12.260 543.88 3795.6 0.4015 1.39969 +FS_22 Splitter.Fl_O1 116.56 13.700 561.42 134.21 0.0000 130.08 12.735 549.83 719.5 0.3246 1.39969 +FS_23 Duct1.Fl_O 116.56 13.666 561.42 134.21 0.0000 130.41 12.704 549.83 721.3 0.3246 1.39969 +FS_24 LPC.Fl_O 116.56 23.890 675.51 161.65 0.0000 81.83 21.183 652.79 366.0 0.4184 1.39687 +FS_25 Duct2.Fl_O 116.56 23.831 675.51 161.65 0.0000 82.03 21.130 652.79 366.9 0.4184 1.39687 +FS_3 HPC.Fl_O 116.56 121.856 1126.14 272.58 0.0000 20.71 114.071 1106.10 119.9 0.3114 1.37280 +FS_36 Bld3.Fl_O 106.07 121.856 1126.14 272.58 0.0000 18.85 114.071 1106.10 109.1 0.3114 1.37280 +FS_4 Burner.Fl_O 107.61 115.154 2060.44 530.38 0.0145 27.37 114.413 2057.25 483.4 0.0991 1.31575 +FS_45 HPT.Fl_O 118.10 41.647 1588.65 397.99 0.0132 72.93 39.199 1564.57 439.1 0.3021 1.33645 +FS_48 Duct3.Fl_O 118.10 41.439 1588.65 397.99 0.0132 73.30 39.003 1564.57 441.4 0.3021 1.33645 +FS_5 LPT.Fl_O 118.10 12.097 1193.54 292.93 0.0132 217.63 11.547 1178.92 1477.4 0.2624 1.35941 +FS_7 Duct4.Fl_O 118.10 11.976 1193.54 292.93 0.0132 219.83 11.686 1185.81 2018.9 0.1903 1.35941 +FS_9 Core_Nozz.Fl_O 118.10 11.976 1193.54 292.93 0.0132 219.83 10.106 1141.02 862.9 0.5046 1.35941 +FS_15 BypBld.Fl_O 736.15 13.700 561.42 134.21 0.0000 821.56 12.260 543.88 3795.6 0.4015 1.39969 +FS_17 Duct5.Fl_O 736.15 13.597 561.42 134.21 0.0000 827.77 12.168 543.88 3824.3 0.4015 1.39969 +FS_19 Byp_Nozz.Fl_O 736.15 13.597 561.42 134.21 0.0000 827.77 10.106 515.75 2706.4 0.6651 1.39969 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1191.73 1.306 0.9090 2784.378 1.0872 0.9124 -13029.4 39.49 15.97 +LPC 130.41 1.748 0.8492 2670.401 1.2032 0.8606 -4526.2 29.91 15.08 +HPC 82.03 5.113 0.8646 6248.618 1.6671 0.8910 -18294.2 28.02 28.18 +HPT 27.37 2.765 0.9152 157.099 1.2525 0.9049 18294.3 +LPT 73.30 3.425 0.9139 69.704 1.3310 0.9000 17555.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2284.98 1.213 0.9391 0.706 1.8438 0.5215 1.4369 0.9679 3943.9586 +LPC 139.89 1.229 0.8845 0.729 1.6776 0.9323 3.2631 0.9600 3662.6571 +HPC 195.02 20.016 0.8530 0.983 2.1724 0.4206 0.2163 1.0137 6357.1603 +HPT 30.12 5.154 0.9336 102.604 5.1540 1.4085 0.4249 0.9803 1.5311 +LPT 152.31 4.383 0.9127 85.936 4.3835 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 8292.89 7336.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 835.52 200.48 38.191 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 835.52 200.48 38.191 +Duct1 0.0025 0.3246 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 835.52 200.48 38.191 +Duct2 0.0025 0.4184 365.99 +Duct3 0.0050 0.3021 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2624 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.0796 1126.14 272.58 121.856 +Duct5 0.0075 0.4015 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.4108 1126.14 272.58 121.856 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 561.42 134.21 13.700 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.3156 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7131.0 13474.0 18294.3 +LP_Shaft 2778.3 33186.6 17555.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2060.44 0.9940 0.0550 1.53924 0.01451 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.345 0.9975 1.0000 0.9975 2706.36 0.665 738.7 16902.0 +Core_Nozz 1.185 0.9999 1.0000 0.9999 862.88 0.505 824.2 3025.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 150 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.250 10000.0 27.00 668.19 6295.1 0.4887 3076.31 6.8351 276.83 7.731 1734.7 1695.4 1325.9 + core size:21.30 Q: 63.70 Maximum Thrust: 31475.9 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 668.19 10.556 516.39 123.41 0.0000 928.24 10.106 510.01 6498.4 0.2500 1.40056 +FS_2 Inlet.Fl_O 668.19 10.492 516.39 123.41 0.0000 933.85 9.946 508.56 5943.4 0.2774 1.40056 +FS_21 Fan.Fl_O 668.19 12.294 542.72 129.72 0.0000 817.05 11.427 531.49 4515.2 0.3249 1.40005 +FS_13 Splitter.Fl_O2 582.91 12.294 542.72 129.72 0.0000 712.77 11.354 530.51 3795.6 0.3390 1.40005 +FS_22 Splitter.Fl_O1 85.28 12.294 542.72 129.72 0.0000 104.28 11.754 535.80 719.5 0.2540 1.40005 +FS_23 Duct1.Fl_O 85.28 12.263 542.72 129.72 0.0000 104.54 11.725 535.80 721.3 0.2540 1.40005 +FS_24 LPC.Fl_O 85.28 17.559 612.86 146.57 0.0000 77.59 15.799 594.67 366.0 0.3916 1.39882 +FS_25 Duct2.Fl_O 85.28 17.515 612.86 146.57 0.0000 77.78 15.759 594.67 366.9 0.3916 1.39882 +FS_3 HPC.Fl_O 85.28 81.607 997.81 240.44 0.0000 21.30 76.070 978.64 119.9 0.3204 1.38085 +FS_36 Bld3.Fl_O 77.61 81.607 997.81 240.44 0.0000 19.38 76.070 978.64 109.1 0.3204 1.38085 +FS_4 Burner.Fl_O 78.46 77.118 1734.73 437.08 0.0110 27.34 76.623 1731.95 483.4 0.0984 1.33100 +FS_45 HPT.Fl_O 86.14 27.570 1325.90 326.61 0.0100 73.41 25.927 1304.78 439.1 0.3023 1.35325 +FS_48 Duct3.Fl_O 86.14 27.432 1325.90 326.61 0.0100 73.78 25.798 1304.78 441.4 0.3023 1.35325 +FS_5 LPT.Fl_O 86.14 11.099 1071.77 260.96 0.0100 163.94 10.819 1064.41 1477.4 0.1934 1.36934 +FS_7 Duct4.Fl_O 86.14 10.988 1071.77 260.96 0.0100 165.60 10.839 1067.82 2018.9 0.1415 1.36934 +FS_9 Core_Nozz.Fl_O 86.14 10.988 1071.77 260.96 0.0100 165.60 10.106 1047.78 862.9 0.3516 1.36934 +FS_15 BypBld.Fl_O 582.91 12.294 542.72 129.72 0.0000 712.77 11.354 530.51 3795.6 0.3390 1.40005 +FS_17 Duct5.Fl_O 582.91 12.202 542.72 129.72 0.0000 718.15 11.268 530.51 3824.3 0.3390 1.40005 +FS_19 Byp_Nozz.Fl_O 582.91 12.202 542.72 129.72 0.0000 718.15 10.106 514.25 2706.4 0.5259 1.40005 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 933.85 1.172 0.9095 2162.497 1.0510 0.9116 -5967.8 43.92 12.45 +LPC 104.54 1.432 0.8351 2109.399 1.1292 0.8432 -2032.8 38.46 12.62 +HPC 77.78 4.659 0.8629 6173.733 1.6281 0.8885 -11327.0 35.08 35.42 +HPT 27.34 2.797 0.9161 161.127 1.2667 0.9053 11327.2 +LPT 73.78 2.472 0.8976 59.258 1.2371 0.8859 8000.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1790.52 1.120 0.9396 0.548 1.8503 0.5215 1.4369 0.9679 3943.9586 +LPC 112.14 1.132 0.8698 0.576 1.7689 0.9323 3.2631 0.9600 3662.6571 +HPC 184.91 17.916 0.8513 0.971 2.2197 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.230 0.9345 105.235 5.2300 1.4085 0.4249 0.9803 1.5311 +LPT 153.31 3.053 0.8964 73.058 3.0527 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 6498.37 5749.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 748.99 179.42 26.905 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 748.99 179.42 26.905 +Duct1 0.0025 0.2540 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 748.99 179.42 26.905 +Duct2 0.0025 0.3916 365.99 +Duct3 0.0050 0.3023 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1934 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.9848 997.81 240.44 81.607 +Duct5 0.0075 0.3390 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.6905 997.81 240.44 81.607 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 542.72 129.72 12.294 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.8351 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6710.9 8864.9 11327.2 +LP_Shaft 2157.7 19473.7 8000.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1734.73 0.9940 0.0550 0.85453 0.01101 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.207 0.9975 1.0000 0.9975 2706.36 0.526 583.2 10566.5 +Core_Nozz 1.087 0.9999 1.0000 0.9999 862.88 0.352 552.0 1477.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 151 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 10000.0 27.00 1218.21 30580.9 0.4851 14835.13 5.0130 332.20 22.794 2726.5 2657.5 2140.6 + core size:19.86 Q: 91.73 Maximum Thrust: 30580.9 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1218.21 10.758 519.20 124.08 0.0000 1665.05 10.106 510.01 9873.0 0.3000 1.40051 +FS_2 Inlet.Fl_O 1218.21 10.693 519.20 124.08 0.0000 1675.11 8.536 486.79 5943.4 0.5764 1.40051 +FS_21 Fan.Fl_O 1218.21 17.668 611.21 146.17 0.0000 1099.98 15.215 585.70 4515.2 0.4672 1.39885 +FS_13 Splitter.Fl_O2 1015.61 17.668 611.21 146.17 0.0000 917.05 15.263 586.23 3795.6 0.4621 1.39885 +FS_22 Splitter.Fl_O1 202.60 17.668 611.21 146.17 0.0000 182.94 14.944 582.70 719.5 0.4951 1.39885 +FS_23 Duct1.Fl_O 202.60 17.624 611.21 146.17 0.0000 183.39 14.906 582.70 721.3 0.4951 1.39885 +FS_24 LPC.Fl_O 202.60 43.777 818.26 196.26 0.0000 85.43 38.286 787.96 366.0 0.4429 1.39107 +FS_25 Duct2.Fl_O 202.60 43.668 818.26 196.26 0.0000 85.64 38.190 787.96 366.9 0.4429 1.39107 +FS_3 HPC.Fl_O 202.60 245.209 1387.48 339.64 0.0000 19.86 230.889 1365.68 119.9 0.2989 1.35663 +FS_36 Bld3.Fl_O 184.36 245.209 1387.48 339.64 0.0000 18.07 230.889 1365.68 109.1 0.2989 1.35663 +FS_4 Burner.Fl_O 188.49 231.722 2726.45 732.20 0.0224 27.41 230.228 2722.45 483.4 0.1000 1.29377 +FS_45 HPT.Fl_O 206.72 87.046 2140.62 557.06 0.0203 70.90 82.224 2111.96 439.1 0.2960 1.30923 +FS_48 Duct3.Fl_O 206.72 86.611 2140.62 557.06 0.0203 71.26 81.812 2111.96 441.4 0.2960 1.30923 +FS_5 LPT.Fl_O 206.72 17.952 1504.66 377.79 0.0203 288.23 16.451 1471.91 1477.4 0.3633 1.33605 +FS_7 Duct4.Fl_O 206.72 17.772 1504.66 377.79 0.0203 291.14 16.999 1487.90 2018.9 0.2587 1.33605 +FS_9 Core_Nozz.Fl_O 206.72 17.772 1504.66 377.79 0.0203 291.14 10.106 1303.16 862.9 0.9491 1.33605 +FS_15 BypBld.Fl_O 1015.61 17.668 611.21 146.17 0.0000 917.05 15.263 586.23 3795.6 0.4621 1.39885 +FS_17 Duct5.Fl_O 1015.61 17.535 611.21 146.17 0.0000 923.98 15.149 586.23 3824.3 0.4621 1.39885 +FS_19 Byp_Nozz.Fl_O 1015.61 17.535 611.21 146.17 0.0000 923.98 10.106 522.20 2706.4 0.9233 1.39885 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.652 0.8704 3944.235 1.1772 0.8792 -38073.2 24.25 17.02 +LPC 183.39 2.484 0.8685 3635.262 1.3388 0.8840 -14359.6 28.54 23.43 +HPC 85.64 5.615 0.8650 6327.872 1.6957 0.8919 -41098.6 20.04 20.09 +HPT 27.41 2.662 0.9137 152.215 1.2262 0.9043 41098.6 +LPT 71.26 4.825 0.9331 85.294 1.4227 0.9195 52432.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.454 0.8992 1.000 2.3357 0.5215 1.4369 0.9679 3943.9586 +LPC 196.71 1.455 0.9046 0.993 1.7706 0.9323 3.2631 0.9600 3662.6571 +HPC 203.60 22.336 0.8533 0.995 2.0428 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.912 0.9321 99.415 4.9118 1.4085 0.4249 0.9803 1.5311 +LPT 148.07 6.335 0.9319 105.156 6.3352 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 9872.98 12578.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1021.94 246.45 73.193 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1021.94 246.45 73.193 +Duct1 0.0025 0.4951 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1021.94 246.45 73.193 +Duct2 0.0025 0.4429 365.99 +Duct3 0.0050 0.2960 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3633 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.0909 1387.48 339.64 245.209 +Duct5 0.0075 0.4621 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.1429 1387.48 339.64 245.209 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 611.21 146.17 17.668 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0130 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7948.0 27158.3 41098.6 +LP_Shaft 3946.3 69783.2 52432.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2726.45 0.9940 0.0550 4.12087 0.02235 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.735 0.9975 1.0000 0.9975 2706.36 0.923 1031.9 32573.1 +Core_Nozz 1.759 0.9999 1.0000 0.9999 862.88 0.949 1647.6 10585.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 152 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 10000.0 27.00 1177.84 27522.7 0.4702 12942.39 5.2905 332.20 20.635 2621.5 2555.5 2049.8 + core size:19.95 Q: 91.73 Maximum Thrust: 30580.9 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1177.84 10.758 519.20 124.08 0.0000 1609.86 10.106 510.01 9545.8 0.3000 1.40051 +FS_2 Inlet.Fl_O 1177.84 10.693 519.20 124.08 0.0000 1619.59 8.724 489.83 5943.4 0.5470 1.40051 +FS_21 Fan.Fl_O 1177.84 17.188 603.17 144.24 0.0000 1086.02 14.874 578.79 4515.2 0.4593 1.39900 +FS_13 Splitter.Fl_O2 990.60 17.188 603.17 144.24 0.0000 913.38 14.871 578.76 3795.6 0.4596 1.39900 +FS_22 Splitter.Fl_O1 187.24 17.188 603.17 144.24 0.0000 172.64 14.887 578.94 719.5 0.4578 1.39900 +FS_23 Duct1.Fl_O 187.24 17.145 603.17 144.24 0.0000 173.08 14.850 578.94 721.3 0.4578 1.39900 +FS_24 LPC.Fl_O 187.24 39.389 788.59 189.04 0.0000 86.14 34.350 758.70 366.0 0.4474 1.39250 +FS_25 Duct2.Fl_O 187.24 39.290 788.59 189.04 0.0000 86.36 34.264 758.70 366.9 0.4474 1.39250 +FS_3 HPC.Fl_O 187.24 221.987 1343.68 328.25 0.0000 19.95 208.896 1322.24 119.9 0.3001 1.35924 +FS_36 Bld3.Fl_O 170.39 221.987 1343.68 328.25 0.0000 18.16 208.896 1322.24 109.1 0.3001 1.35924 +FS_4 Burner.Fl_O 173.98 209.778 2621.47 699.51 0.0211 27.40 208.426 2617.60 483.4 0.0999 1.29668 +FS_45 HPT.Fl_O 190.83 77.875 2049.83 530.14 0.0192 71.59 73.470 2021.55 439.1 0.2987 1.31291 +FS_48 Duct3.Fl_O 190.83 77.485 2049.83 530.14 0.0192 71.95 73.102 2021.55 441.4 0.2987 1.31291 +FS_5 LPT.Fl_O 190.83 16.460 1447.10 361.78 0.0192 284.60 15.122 1416.26 1477.4 0.3573 1.33995 +FS_7 Duct4.Fl_O 190.83 16.295 1447.10 361.78 0.0192 287.47 15.605 1431.27 2018.9 0.2548 1.33995 +FS_9 Core_Nozz.Fl_O 190.83 16.295 1447.10 361.78 0.0192 287.47 10.106 1280.24 862.9 0.8677 1.33995 +FS_15 BypBld.Fl_O 990.60 17.188 603.17 144.24 0.0000 913.38 14.871 578.76 3795.6 0.4596 1.39900 +FS_17 Duct5.Fl_O 990.60 17.059 603.17 144.24 0.0000 920.28 14.760 578.76 3824.3 0.4596 1.39900 +FS_19 Byp_Nozz.Fl_O 990.60 17.059 603.17 144.24 0.0000 920.28 10.106 519.38 2706.4 0.8981 1.39900 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1619.59 1.607 0.8979 3710.343 1.1617 0.9045 -33588.8 28.11 17.16 +LPC 173.08 2.297 0.8661 3442.421 1.3074 0.8806 -11868.8 29.46 22.38 +HPC 86.36 5.650 0.8633 6346.911 1.7039 0.8908 -36879.5 20.22 20.22 +HPT 27.40 2.694 0.9142 152.851 1.2316 0.9046 36879.5 +LPT 71.95 4.708 0.9287 81.993 1.4165 0.9143 45457.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3105.38 1.423 0.9277 0.941 2.1060 0.5215 1.4369 0.9679 3943.9586 +LPC 185.65 1.398 0.9022 0.940 1.7623 0.9323 3.2631 0.9600 3662.6571 +HPC 205.30 22.496 0.8516 0.998 2.0752 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.987 0.9326 99.830 4.9865 1.4085 0.4249 0.9803 1.5311 +LPT 149.51 6.172 0.9275 101.087 6.1719 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 9545.75 12161.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 987.02 237.76 66.055 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 987.02 237.76 66.055 +Duct1 0.0025 0.4578 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 987.02 237.76 66.055 +Duct2 0.0025 0.4474 365.99 +Duct3 0.0050 0.2987 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3573 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.5534 1343.68 328.25 221.987 +Duct5 0.0075 0.4596 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.2982 1343.68 328.25 221.987 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 603.17 144.24 17.188 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.2905 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7826.0 24750.2 36879.5 +LP_Shaft 3712.2 64313.8 45457.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2621.47 0.9940 0.0550 3.59511 0.02110 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.688 0.9975 1.0000 0.9975 2706.36 0.898 1001.1 30821.1 +Core_Nozz 1.612 0.9999 1.0000 0.9999 862.88 0.868 1494.3 8862.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 153 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 10000.0 27.00 1130.22 24464.7 0.4622 11308.19 5.4827 332.20 18.812 2518.3 2455.5 1964.6 + core size:20.09 Q: 91.73 Maximum Thrust: 30580.9 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1130.22 10.758 519.20 124.08 0.0000 1544.78 10.106 510.01 9159.8 0.3000 1.40051 +FS_2 Inlet.Fl_O 1130.22 10.693 519.20 124.08 0.0000 1554.11 8.924 493.02 5943.4 0.5148 1.40051 +FS_21 Fan.Fl_O 1130.22 16.601 595.83 142.47 0.0000 1072.37 14.433 572.51 4515.2 0.4517 1.39911 +FS_13 Splitter.Fl_O2 955.88 16.601 595.83 142.47 0.0000 906.95 14.401 572.15 3795.6 0.4553 1.39911 +FS_22 Splitter.Fl_O1 174.34 16.601 595.83 142.47 0.0000 165.42 14.594 574.32 719.5 0.4331 1.39911 +FS_23 Duct1.Fl_O 174.34 16.560 595.83 142.47 0.0000 165.83 14.557 574.32 721.3 0.4331 1.39911 +FS_24 LPC.Fl_O 174.34 36.569 770.01 184.52 0.0000 85.37 31.991 741.45 366.0 0.4421 1.39339 +FS_25 Duct2.Fl_O 174.34 36.478 770.01 184.52 0.0000 85.58 31.911 741.45 366.9 0.4421 1.39339 +FS_3 HPC.Fl_O 174.34 202.371 1306.45 318.62 0.0000 20.09 190.254 1285.18 119.9 0.3022 1.36150 +FS_36 Bld3.Fl_O 158.65 202.371 1306.45 318.62 0.0000 18.29 190.254 1285.18 109.1 0.3022 1.36150 +FS_4 Burner.Fl_O 161.79 191.241 2518.30 667.62 0.0198 27.40 190.008 2514.54 483.4 0.0998 1.29985 +FS_45 HPT.Fl_O 177.48 70.638 1964.57 505.05 0.0180 71.86 66.611 1937.00 439.1 0.2995 1.31672 +FS_48 Duct3.Fl_O 177.48 70.285 1964.57 505.05 0.0180 72.22 66.278 1937.00 441.4 0.2995 1.31672 +FS_5 LPT.Fl_O 177.48 15.349 1392.16 346.62 0.0180 278.41 14.161 1363.72 1477.4 0.3478 1.34389 +FS_7 Duct4.Fl_O 177.48 15.195 1392.16 346.62 0.0180 281.22 14.580 1377.52 2018.9 0.2485 1.34389 +FS_9 Core_Nozz.Fl_O 177.48 15.195 1392.16 346.62 0.0180 281.22 10.106 1252.96 862.9 0.7976 1.34389 +FS_15 BypBld.Fl_O 955.88 16.601 595.83 142.47 0.0000 906.95 14.401 572.15 3795.6 0.4553 1.39911 +FS_17 Duct5.Fl_O 955.88 16.477 595.83 142.47 0.0000 913.80 14.293 572.15 3824.3 0.4553 1.39911 +FS_19 Byp_Nozz.Fl_O 955.88 16.477 595.83 142.47 0.0000 913.80 10.106 518.17 2706.3 0.8656 1.39911 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1554.11 1.553 0.9074 3560.933 1.1476 0.9129 -29412.6 31.86 17.47 +LPC 165.83 2.208 0.8633 3324.067 1.2923 0.8774 -10372.7 28.86 20.70 +HPC 85.58 5.548 0.8641 6325.414 1.6967 0.8912 -33076.3 21.65 21.71 +HPT 27.40 2.707 0.9145 153.582 1.2351 0.9046 33076.2 +LPT 72.22 4.579 0.9269 80.381 1.4112 0.9125 39785.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2979.77 1.385 0.9374 0.903 2.0077 0.5215 1.4369 0.9679 3943.9586 +LPC 177.88 1.370 0.8992 0.908 1.7304 0.9323 3.2631 0.9600 3662.6571 +HPC 203.45 22.023 0.8525 0.995 2.0981 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.018 0.9329 100.307 5.0184 1.4085 0.4249 0.9803 1.5311 +LPT 150.07 5.993 0.9257 99.100 5.9929 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 9159.84 11669.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 961.59 231.46 60.781 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 961.59 231.46 60.781 +Duct1 0.0025 0.4331 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 961.59 231.46 60.781 +Duct2 0.0025 0.4421 365.99 +Duct3 0.0050 0.2995 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3478 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.1020 1306.45 318.62 202.371 +Duct5 0.0075 0.4553 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.5888 1306.45 318.62 202.371 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 595.83 142.47 16.601 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.4827 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7707.1 22540.2 33076.2 +LP_Shaft 3562.8 58650.5 39785.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2518.30 0.9940 0.0550 3.14116 0.01980 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.630 0.9975 1.0000 0.9975 2706.36 0.866 963.7 28631.6 +Core_Nozz 1.504 0.9999 1.0000 0.9999 862.88 0.798 1360.1 7502.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 154 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 10000.0 27.00 1019.01 18348.4 0.4570 8384.54 5.8967 332.20 15.246 2312.3 2255.8 1795.1 + core size:20.38 Q: 91.73 Maximum Thrust: 30580.9 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1019.01 10.758 519.20 124.08 0.0000 1392.78 10.106 510.01 8258.6 0.3000 1.40051 +FS_2 Inlet.Fl_O 1019.01 10.693 519.20 124.08 0.0000 1401.20 9.321 499.20 5943.4 0.4471 1.40051 +FS_21 Fan.Fl_O 1019.01 15.339 581.03 138.92 0.0000 1033.33 13.504 560.27 4515.2 0.4306 1.39934 +FS_13 Splitter.Fl_O2 871.26 15.339 581.03 138.92 0.0000 883.50 13.429 559.39 3795.6 0.4400 1.39934 +FS_22 Splitter.Fl_O1 147.75 15.339 581.03 138.92 0.0000 149.83 13.862 564.48 719.5 0.3831 1.39934 +FS_23 Duct1.Fl_O 147.75 15.300 581.03 138.92 0.0000 150.20 13.827 564.48 721.3 0.3831 1.39934 +FS_24 LPC.Fl_O 147.75 30.774 730.20 174.87 0.0000 83.72 27.095 704.33 366.0 0.4310 1.39501 +FS_25 Duct2.Fl_O 147.75 30.697 730.20 174.87 0.0000 83.93 27.027 704.33 366.9 0.4310 1.39501 +FS_3 HPC.Fl_O 147.75 164.009 1228.54 298.60 0.0000 20.38 153.893 1207.72 119.9 0.3064 1.36635 +FS_36 Bld3.Fl_O 134.46 164.009 1228.54 298.60 0.0000 18.54 153.893 1207.72 109.1 0.3064 1.36635 +FS_4 Burner.Fl_O 136.78 154.989 2312.35 605.03 0.0173 27.39 153.991 2308.84 483.4 0.0995 1.30654 +FS_45 HPT.Fl_O 150.08 56.732 1795.13 456.07 0.0158 72.33 53.454 1769.08 439.1 0.3007 1.32506 +FS_48 Duct3.Fl_O 150.08 56.448 1795.13 456.07 0.0158 72.69 53.187 1769.08 441.4 0.3007 1.32506 +FS_5 LPT.Fl_O 150.08 13.566 1294.29 319.94 0.0158 256.82 12.687 1271.90 1477.4 0.3161 1.35134 +FS_7 Duct4.Fl_O 150.08 13.431 1294.29 319.94 0.0158 259.42 12.972 1282.63 2018.9 0.2273 1.35134 +FS_9 Core_Nozz.Fl_O 150.08 13.431 1294.29 319.94 0.0158 259.42 10.106 1201.56 862.9 0.6593 1.35134 +FS_15 BypBld.Fl_O 871.26 15.339 581.03 138.92 0.0000 883.50 13.429 559.39 3795.6 0.4400 1.39934 +FS_17 Duct5.Fl_O 871.26 15.224 581.03 138.92 0.0000 890.18 13.328 559.39 3824.3 0.4400 1.39934 +FS_19 Byp_Nozz.Fl_O 871.26 15.224 581.03 138.92 0.0000 890.18 10.106 516.82 2706.4 0.7880 1.39934 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1401.20 1.434 0.9121 3232.104 1.1191 0.9165 -21390.3 38.49 17.56 +LPC 150.20 2.011 0.8567 3055.308 1.2567 0.8700 -7516.7 28.00 17.65 +HPC 83.93 5.343 0.8650 6286.410 1.6825 0.8914 -25864.7 24.55 24.67 +HPT 27.39 2.732 0.9148 155.115 1.2423 0.9048 25864.7 +LPT 72.69 4.161 0.9228 76.324 1.3870 0.9084 28906.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2686.60 1.302 0.9423 0.820 1.9183 0.5215 1.4369 0.9679 3943.9586 +LPC 161.12 1.310 0.8924 0.834 1.6789 0.9323 3.2631 0.9600 3662.6571 +HPC 199.53 21.076 0.8533 0.989 2.1356 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.076 0.9332 101.308 5.0763 1.4085 0.4249 0.9803 1.5311 +LPT 151.05 5.409 0.9216 94.098 5.4093 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 8258.58 10521.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 907.74 218.18 50.228 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 907.74 218.18 50.228 +Duct1 0.0025 0.3831 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 907.74 218.18 50.228 +Duct2 0.0025 0.4310 365.99 +Duct3 0.0050 0.3007 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3161 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.1714 1228.54 298.60 164.009 +Duct5 0.0075 0.4400 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.1264 1228.54 298.60 164.009 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 581.03 138.92 15.339 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.8967 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7459.0 18212.2 25864.7 +LP_Shaft 3233.8 46948.6 28906.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2312.35 0.9940 0.0550 2.32904 0.01732 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.506 0.9975 1.0000 0.9975 2706.36 0.788 876.1 23725.1 +Core_Nozz 1.329 0.9999 1.0000 0.9999 862.88 0.659 1102.9 5144.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 155 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 10000.0 27.00 882.72 12232.3 0.4678 5721.86 6.3872 332.20 11.653 2074.5 2025.0 1600.4 + core size:20.72 Q: 91.73 Maximum Thrust: 30580.9 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 882.72 10.758 519.20 124.08 0.0000 1206.49 10.106 510.01 7154.0 0.3000 1.40051 +FS_2 Inlet.Fl_O 882.72 10.693 519.20 124.08 0.0000 1213.78 9.708 505.04 5943.4 0.3741 1.40051 +FS_21 Fan.Fl_O 882.72 13.993 564.74 135.00 0.0000 967.32 12.556 547.53 4515.2 0.3965 1.39963 +FS_13 Splitter.Fl_O2 763.22 13.993 564.74 135.00 0.0000 836.38 12.461 546.33 3795.6 0.4105 1.39963 +FS_22 Splitter.Fl_O1 119.49 13.993 564.74 135.00 0.0000 130.94 12.994 552.91 719.5 0.3271 1.39963 +FS_23 Duct1.Fl_O 119.49 13.958 564.74 135.00 0.0000 131.27 12.962 552.91 721.3 0.3271 1.39963 +FS_24 LPC.Fl_O 119.49 24.672 681.95 163.21 0.0000 81.61 21.893 659.18 366.0 0.4171 1.39664 +FS_25 Duct2.Fl_O 119.49 24.610 681.95 163.21 0.0000 81.82 21.838 659.18 366.9 0.4171 1.39664 +FS_3 HPC.Fl_O 119.49 125.363 1135.10 274.85 0.0000 20.72 117.346 1114.91 119.9 0.3116 1.37223 +FS_36 Bld3.Fl_O 108.74 125.363 1135.10 274.85 0.0000 18.86 117.346 1114.91 109.1 0.3116 1.37223 +FS_4 Burner.Fl_O 110.33 118.468 2074.47 534.45 0.0146 27.37 117.706 2071.26 483.4 0.0991 1.31521 +FS_45 HPT.Fl_O 121.08 42.880 1600.36 401.22 0.0133 72.89 40.362 1576.16 439.1 0.3020 1.33580 +FS_48 Duct3.Fl_O 121.08 42.666 1600.36 401.22 0.0133 73.26 40.160 1576.16 441.4 0.3020 1.33580 +FS_5 LPT.Fl_O 121.08 12.201 1196.60 293.75 0.0133 221.51 11.625 1181.39 1477.4 0.2675 1.35915 +FS_7 Duct4.Fl_O 121.08 12.079 1196.60 293.75 0.0133 223.75 11.775 1188.57 2018.9 0.1939 1.35915 +FS_9 Core_Nozz.Fl_O 121.08 12.079 1196.60 293.75 0.0133 223.75 10.106 1141.38 862.9 0.5174 1.35915 +FS_15 BypBld.Fl_O 763.22 13.993 564.74 135.00 0.0000 836.38 12.461 546.33 3795.6 0.4105 1.39963 +FS_17 Duct5.Fl_O 763.22 13.889 564.74 135.00 0.0000 842.70 12.367 546.33 3824.3 0.4105 1.39963 +FS_19 Byp_Nozz.Fl_O 763.22 13.889 564.74 135.00 0.0000 842.70 10.106 515.68 2706.4 0.6895 1.39963 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1213.78 1.309 0.9114 2811.120 1.0877 0.9147 -13643.4 41.07 16.83 +LPC 131.27 1.768 0.8490 2695.405 1.2075 0.8607 -4768.0 29.20 14.95 +HPC 81.82 5.094 0.8647 6244.731 1.6645 0.8910 -18874.1 28.25 28.41 +HPT 27.37 2.763 0.9153 157.214 1.2518 0.9049 18874.2 +LPT 73.26 3.497 0.9148 70.306 1.3374 0.9008 18411.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2327.26 1.215 0.9416 0.713 1.8817 0.5215 1.4369 0.9679 3943.9586 +LPC 140.81 1.235 0.8843 0.736 1.6652 0.9323 3.2631 0.9600 3662.6571 +HPC 194.51 19.925 0.8530 0.982 2.1717 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.149 0.9336 102.679 5.1489 1.4085 0.4249 0.9803 1.5311 +LPT 152.23 4.483 0.9136 86.679 4.4830 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 7153.95 9114.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 842.90 202.28 39.371 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 842.90 202.28 39.371 +Duct1 0.0025 0.3271 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 842.90 202.28 39.371 +Duct2 0.0025 0.4171 365.99 +Duct3 0.0050 0.3020 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2675 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.1822 1135.10 274.85 125.363 +Duct5 0.0075 0.4105 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.5720 1135.10 274.85 125.363 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 564.74 135.00 13.993 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.3872 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7160.5 13843.9 18874.2 +LP_Shaft 2812.6 34380.2 18411.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2074.47 0.9940 0.0550 1.58941 0.01462 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.374 0.9975 1.0000 0.9975 2706.36 0.689 765.8 18165.4 +Core_Nozz 1.195 0.9999 1.0000 0.9999 862.88 0.517 845.3 3181.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 156 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 10000.0 27.00 704.25 6116.1 0.5257 3215.39 7.0058 332.20 7.868 1753.4 1713.6 1341.0 + core size:21.30 Q: 91.73 Maximum Thrust: 30580.9 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 704.25 10.758 519.20 124.08 0.0000 962.57 10.106 510.01 5707.6 0.3000 1.40051 +FS_2 Inlet.Fl_O 704.25 10.693 519.20 124.08 0.0000 968.38 10.092 510.68 5943.4 0.2887 1.40051 +FS_21 Fan.Fl_O 704.25 12.562 546.05 130.52 0.0000 845.38 11.607 533.85 4515.2 0.3379 1.39998 +FS_13 Splitter.Fl_O2 616.28 12.562 546.05 130.52 0.0000 739.79 11.518 532.69 3795.6 0.3540 1.39998 +FS_22 Splitter.Fl_O1 87.97 12.562 546.05 130.52 0.0000 105.60 11.995 538.90 719.5 0.2575 1.39998 +FS_23 Duct1.Fl_O 87.97 12.530 546.05 130.52 0.0000 105.86 11.965 538.90 721.3 0.2575 1.39998 +FS_24 LPC.Fl_O 87.97 18.224 619.76 148.23 0.0000 77.54 16.399 601.39 366.0 0.3913 1.39867 +FS_25 Duct2.Fl_O 87.97 18.178 619.76 148.23 0.0000 77.74 16.358 601.39 366.9 0.3913 1.39867 +FS_3 HPC.Fl_O 87.97 84.641 1008.48 243.09 0.0000 21.30 78.901 989.13 119.9 0.3204 1.38018 +FS_36 Bld3.Fl_O 80.05 84.641 1008.48 243.09 0.0000 19.38 78.901 989.13 109.1 0.3204 1.38018 +FS_4 Burner.Fl_O 80.94 79.986 1753.35 442.29 0.0112 27.34 79.473 1750.55 483.4 0.0984 1.33005 +FS_45 HPT.Fl_O 88.86 28.612 1341.01 330.62 0.0102 73.39 26.909 1319.71 439.1 0.3024 1.35224 +FS_48 Duct3.Fl_O 88.86 28.469 1341.01 330.62 0.0102 73.76 26.774 1319.71 441.4 0.3024 1.35224 +FS_5 LPT.Fl_O 88.86 11.161 1076.02 262.07 0.0102 168.53 10.863 1068.20 1477.4 0.1991 1.36898 +FS_7 Duct4.Fl_O 88.86 11.049 1076.02 262.07 0.0102 170.23 10.890 1071.83 2018.9 0.1456 1.36898 +FS_9 Core_Nozz.Fl_O 88.86 11.049 1076.02 262.07 0.0102 170.23 10.106 1050.38 862.9 0.3632 1.36898 +FS_15 BypBld.Fl_O 616.28 12.562 546.05 130.52 0.0000 739.79 11.518 532.69 3795.6 0.3540 1.39998 +FS_17 Duct5.Fl_O 616.28 12.467 546.05 130.52 0.0000 745.38 11.432 532.69 3824.3 0.3540 1.39998 +FS_19 Byp_Nozz.Fl_O 616.28 12.467 546.05 130.52 0.0000 745.38 10.106 514.22 2706.4 0.5560 1.39998 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 968.38 1.175 0.9115 2203.958 1.0517 0.9136 -6414.7 46.41 13.93 +LPC 105.86 1.454 0.8360 2149.101 1.1350 0.8444 -2204.0 37.03 12.48 +HPC 77.74 4.656 0.8630 6172.941 1.6272 0.8885 -11807.4 35.10 35.45 +HPT 27.34 2.796 0.9161 161.148 1.2659 0.9053 11807.6 +LPT 73.76 2.551 0.8988 60.216 1.2463 0.8869 8618.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1856.74 1.122 0.9417 0.559 1.9128 0.5215 1.4369 0.9679 3943.9586 +LPC 113.55 1.139 0.8708 0.587 1.7463 0.9323 3.2631 0.9600 3662.6571 +HPC 184.81 17.902 0.8513 0.971 2.2195 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.226 0.9345 105.249 5.2260 1.4085 0.4249 0.9803 1.5311 +LPT 153.26 3.163 0.8977 74.239 3.1633 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 5707.60 7271.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 757.26 181.43 27.915 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 757.26 181.43 27.915 +Duct1 0.0025 0.2575 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 757.26 181.43 27.915 +Duct2 0.0025 0.3913 365.99 +Duct3 0.0050 0.3024 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1991 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.0789 1008.48 243.09 84.641 +Duct5 0.0075 0.3540 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.8382 1008.48 243.09 84.641 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 546.05 130.52 12.562 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.0058 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6747.8 9190.4 11807.6 +LP_Shaft 2205.1 20527.7 8618.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1753.35 0.9940 0.0550 0.89316 0.01116 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.234 0.9975 1.0000 0.9975 2706.36 0.556 616.6 11810.8 +Core_Nozz 1.093 0.9999 1.0000 0.9999 862.88 0.363 570.9 1576.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 157 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 10000.0 27.00 1262.26 28738.7 0.5264 15128.27 5.1046 442.93 22.192 2730.0 2661.1 2142.5 + core size:19.88 Q: 163.07 Maximum Thrust: 28738.7 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1262.26 11.285 526.35 125.79 0.0000 1655.98 10.106 510.01 7672.5 0.4000 1.40038 +FS_2 Inlet.Fl_O 1262.26 11.228 526.35 125.79 0.0000 1664.32 9.003 494.12 5943.4 0.5705 1.40038 +FS_21 Fan.Fl_O 1262.26 18.385 617.23 147.62 0.0000 1100.70 15.828 591.42 4515.2 0.4676 1.39873 +FS_13 Splitter.Fl_O2 1055.49 18.385 617.23 147.62 0.0000 920.39 15.860 591.77 3795.6 0.4643 1.39873 +FS_22 Splitter.Fl_O1 206.77 18.385 617.23 147.62 0.0000 180.31 15.650 589.52 719.5 0.4854 1.39873 +FS_23 Duct1.Fl_O 206.77 18.339 617.23 147.62 0.0000 180.76 15.610 589.52 721.3 0.4854 1.39873 +FS_24 LPC.Fl_O 206.77 44.748 821.77 197.12 0.0000 85.48 39.127 791.31 366.0 0.4433 1.39091 +FS_25 Duct2.Fl_O 206.77 44.636 821.77 197.12 0.0000 85.69 39.029 791.31 366.9 0.4433 1.39091 +FS_3 HPC.Fl_O 206.77 250.429 1392.85 341.04 0.0000 19.88 235.765 1370.91 119.9 0.2993 1.35631 +FS_36 Bld3.Fl_O 188.16 250.429 1392.85 341.04 0.0000 18.09 235.765 1370.91 109.1 0.2993 1.35631 +FS_4 Burner.Fl_O 192.37 236.656 2729.99 733.25 0.0223 27.41 235.130 2725.98 483.4 0.1000 1.29372 +FS_45 HPT.Fl_O 210.98 88.684 2142.52 557.60 0.0203 71.06 83.747 2113.71 439.1 0.2967 1.30919 +FS_48 Duct3.Fl_O 210.98 88.240 2142.52 557.60 0.0203 71.41 83.328 2113.71 441.4 0.2967 1.30919 +FS_5 LPT.Fl_O 210.98 18.313 1507.38 378.52 0.0203 288.63 16.777 1474.48 1477.4 0.3639 1.33592 +FS_7 Duct4.Fl_O 210.98 18.130 1507.38 378.52 0.0203 291.54 17.338 1490.54 2018.9 0.2591 1.33592 +FS_9 Core_Nozz.Fl_O 210.98 18.130 1507.38 378.52 0.0203 291.54 10.106 1298.87 862.9 0.9669 1.33592 +FS_15 BypBld.Fl_O 1055.49 18.385 617.23 147.62 0.0000 920.39 15.860 591.77 3795.6 0.4643 1.39873 +FS_17 Duct5.Fl_O 1055.49 18.247 617.23 147.62 0.0000 927.34 15.741 591.77 3824.3 0.4643 1.39873 +FS_19 Byp_Nozz.Fl_O 1055.49 18.247 617.23 147.62 0.0000 927.34 10.106 521.39 2706.4 0.9588 1.39873 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1664.32 1.637 0.8759 3885.818 1.1727 0.8841 -38972.4 25.49 17.39 +LPC 180.76 2.440 0.8678 3588.378 1.3314 0.8831 -14483.0 28.58 23.04 +HPC 85.69 5.610 0.8648 6328.940 1.6949 0.8917 -42104.0 20.23 20.27 +HPT 27.41 2.669 0.9139 152.469 1.2269 0.9045 42104.8 +LPT 71.41 4.818 0.9319 84.569 1.4214 0.9181 53455.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3191.11 1.444 0.9049 0.985 2.2961 0.5215 1.4369 0.9679 3943.9586 +LPC 193.89 1.441 0.9039 0.980 1.7635 0.9323 3.2631 0.9600 3662.6571 +HPC 203.71 22.313 0.8532 0.996 2.0514 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.927 0.9323 99.580 4.9271 1.4085 0.4249 0.9803 1.5311 +LPT 148.38 6.327 0.9307 104.263 6.3266 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 7672.46 17377.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1026.14 247.49 74.785 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1026.14 247.49 74.785 +Duct1 0.0025 0.4854 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1026.14 247.49 74.785 +Duct2 0.0025 0.4433 365.99 +Duct3 0.0050 0.2967 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3639 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.2371 1392.85 341.04 250.429 +Duct5 0.0075 0.4643 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.3725 1392.85 341.04 250.429 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 617.23 147.62 18.385 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.1046 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7966.4 27759.0 42104.8 +LP_Shaft 3914.5 71721.6 53455.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2729.99 0.9940 0.0550 4.20230 0.02233 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.805 0.9975 1.0000 0.9975 2706.36 0.959 1070.8 35126.6 +Core_Nozz 1.794 0.9999 1.0000 0.9999 862.88 0.967 1675.9 10989.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 158 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 10000.0 27.00 1223.76 25864.5 0.5140 13294.06 5.3579 442.93 20.250 2628.3 2562.4 2055.5 + core size:19.99 Q: 163.07 Maximum Thrust: 28738.7 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1223.76 11.285 526.35 125.79 0.0000 1605.47 10.106 510.01 7438.4 0.4000 1.40038 +FS_2 Inlet.Fl_O 1223.76 11.228 526.35 125.79 0.0000 1613.55 9.180 496.89 5943.4 0.5439 1.40038 +FS_21 Fan.Fl_O 1223.76 17.893 609.78 145.83 0.0000 1089.79 15.464 584.92 4515.2 0.4614 1.39888 +FS_13 Splitter.Fl_O2 1031.28 17.893 609.78 145.83 0.0000 918.39 15.450 584.77 3795.6 0.4629 1.39888 +FS_22 Splitter.Fl_O1 192.48 17.893 609.78 145.83 0.0000 171.41 15.539 585.73 719.5 0.4535 1.39888 +FS_23 Duct1.Fl_O 192.48 17.849 609.78 145.83 0.0000 171.84 15.500 585.73 721.3 0.4535 1.39888 +FS_24 LPC.Fl_O 192.48 40.875 796.47 190.96 0.0000 85.76 35.701 766.65 366.0 0.4449 1.39211 +FS_25 Duct2.Fl_O 192.48 40.772 796.47 190.96 0.0000 85.97 35.612 766.65 366.9 0.4449 1.39211 +FS_3 HPC.Fl_O 192.48 228.509 1352.77 330.61 0.0000 19.99 214.974 1331.11 119.9 0.3008 1.35869 +FS_36 Bld3.Fl_O 175.15 228.509 1352.77 330.61 0.0000 18.19 214.974 1331.11 109.1 0.3008 1.35869 +FS_4 Burner.Fl_O 178.85 215.941 2628.29 701.54 0.0211 27.40 214.549 2624.40 483.4 0.0999 1.29655 +FS_45 HPT.Fl_O 196.17 80.147 2055.51 531.76 0.0192 71.61 75.611 2027.15 439.1 0.2988 1.31273 +FS_48 Duct3.Fl_O 196.17 79.746 2055.51 531.76 0.0192 71.97 75.233 2027.15 441.4 0.2988 1.31273 +FS_5 LPT.Fl_O 196.17 16.850 1449.88 362.52 0.0192 286.06 15.465 1418.62 1477.4 0.3595 1.33980 +FS_7 Duct4.Fl_O 196.17 16.681 1449.88 362.52 0.0192 288.95 15.967 1433.85 2018.9 0.2563 1.33980 +FS_9 Core_Nozz.Fl_O 196.17 16.681 1449.88 362.52 0.0192 288.95 10.106 1274.99 862.9 0.8900 1.33980 +FS_15 BypBld.Fl_O 1031.28 17.893 609.78 145.83 0.0000 918.39 15.450 584.77 3795.6 0.4629 1.39888 +FS_17 Duct5.Fl_O 1031.28 17.759 609.78 145.83 0.0000 925.33 15.334 584.77 3824.3 0.4629 1.39888 +FS_19 Byp_Nozz.Fl_O 1031.28 17.759 609.78 145.83 0.0000 925.33 10.106 519.08 2706.4 0.9347 1.39888 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1613.55 1.594 0.8982 3687.662 1.1585 0.9047 -34682.7 29.20 17.68 +LPC 171.84 2.290 0.8654 3426.125 1.3062 0.8800 -12290.6 29.04 21.87 +HPC 85.97 5.605 0.8639 6335.938 1.6984 0.8911 -38030.5 20.79 20.81 +HPT 27.40 2.694 0.9144 153.149 1.2316 0.9048 38029.9 +LPT 71.97 4.733 0.9283 81.938 1.4177 0.9138 46972.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3093.47 1.413 0.9280 0.935 2.1201 0.5215 1.4369 0.9679 3943.9586 +LPC 184.31 1.395 0.9014 0.935 1.7493 0.9323 3.2631 0.9600 3662.6571 +HPC 204.38 22.286 0.8522 0.997 2.0817 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 4.988 0.9328 100.024 4.9878 1.4085 0.4249 0.9803 1.5311 +LPT 149.54 6.207 0.9271 101.019 6.2071 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 7438.43 16847.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 995.37 239.83 68.276 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 995.37 239.83 68.276 +Duct1 0.0025 0.4535 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 995.37 239.83 68.276 +Duct2 0.0025 0.4449 365.99 +Duct3 0.0050 0.2988 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3595 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.7367 1352.77 330.61 228.509 +Duct5 0.0075 0.4629 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.5862 1352.77 330.61 228.509 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 609.78 145.83 17.893 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3579 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7851.5 25439.5 38029.9 +LP_Shaft 3714.9 66410.1 46972.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2628.29 0.9940 0.0550 3.69279 0.02108 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.757 0.9975 1.0000 0.9975 2706.36 0.935 1041.6 33385.1 +Core_Nozz 1.651 0.9999 1.0000 0.9999 862.88 0.890 1529.7 9326.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 159 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 10000.0 27.00 1178.97 22991.1 0.5076 11669.91 5.5524 442.93 18.544 2527.5 2464.7 1972.5 + core size:20.14 Q: 163.07 Maximum Thrust: 28738.7 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1178.97 11.285 526.35 125.79 0.0000 1546.72 10.106 510.01 7166.2 0.4000 1.40038 +FS_2 Inlet.Fl_O 1178.97 11.228 526.35 125.79 0.0000 1554.50 9.369 499.79 5943.4 0.5150 1.40038 +FS_21 Fan.Fl_O 1178.97 17.308 602.72 144.13 0.0000 1079.12 15.013 578.75 4515.2 0.4555 1.39900 +FS_13 Splitter.Fl_O2 999.04 17.308 602.72 144.13 0.0000 914.43 14.969 578.26 3795.6 0.4603 1.39900 +FS_22 Splitter.Fl_O1 179.93 17.308 602.72 144.13 0.0000 164.69 15.237 581.20 719.5 0.4307 1.39900 +FS_23 Duct1.Fl_O 179.93 17.265 602.72 144.13 0.0000 165.10 15.198 581.20 721.3 0.4307 1.39900 +FS_24 LPC.Fl_O 179.93 38.217 779.57 186.85 0.0000 84.83 33.503 751.12 366.0 0.4386 1.39294 +FS_25 Duct2.Fl_O 179.93 38.121 779.57 186.85 0.0000 85.04 33.419 751.12 366.9 0.4386 1.39294 +FS_3 HPC.Fl_O 179.93 209.255 1317.29 321.42 0.0000 20.14 196.666 1295.76 119.9 0.3031 1.36084 +FS_36 Bld3.Fl_O 163.74 209.255 1317.29 321.42 0.0000 18.33 196.666 1295.76 109.1 0.3031 1.36084 +FS_4 Burner.Fl_O 166.98 197.746 2527.47 670.35 0.0198 27.39 196.472 2523.70 483.4 0.0998 1.29965 +FS_45 HPT.Fl_O 183.17 73.073 1972.51 507.31 0.0180 71.84 68.909 1944.86 439.1 0.2995 1.31643 +FS_48 Duct3.Fl_O 183.17 72.707 1972.51 507.31 0.0180 72.20 68.565 1944.86 441.4 0.2995 1.31643 +FS_5 LPT.Fl_O 183.17 15.713 1394.88 347.34 0.0180 280.95 14.472 1365.79 1477.4 0.3515 1.34373 +FS_7 Duct4.Fl_O 183.17 15.556 1394.88 347.34 0.0180 283.79 14.914 1379.92 2018.9 0.2509 1.34373 +FS_9 Core_Nozz.Fl_O 183.17 15.556 1394.88 347.34 0.0180 283.79 10.106 1247.80 862.9 0.8214 1.34373 +FS_15 BypBld.Fl_O 999.04 17.308 602.72 144.13 0.0000 914.43 14.969 578.26 3795.6 0.4603 1.39900 +FS_17 Duct5.Fl_O 999.04 17.178 602.72 144.13 0.0000 921.34 14.856 578.26 3824.3 0.4603 1.39900 +FS_19 Byp_Nozz.Fl_O 999.04 17.178 602.72 144.13 0.0000 921.34 10.106 517.96 2706.3 0.9045 1.39900 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1554.50 1.541 0.9069 3552.751 1.1451 0.9124 -30583.8 33.00 18.14 +LPC 165.10 2.214 0.8624 3320.049 1.2934 0.8767 -10874.9 28.23 20.15 +HPC 85.04 5.489 0.8647 6311.898 1.6898 0.8916 -34257.8 22.35 22.43 +HPT 27.39 2.706 0.9146 153.922 1.2348 0.9047 34257.8 +LPT 72.20 4.627 0.9268 80.584 1.4141 0.9122 41458.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2980.46 1.377 0.9369 0.901 2.0383 0.5215 1.4369 0.9679 3943.9586 +LPC 177.09 1.372 0.8983 0.906 1.7142 0.9323 3.2631 0.9600 3662.6571 +HPC 202.17 21.753 0.8531 0.993 2.1029 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.016 0.9329 100.529 5.0156 1.4085 0.4249 0.9803 1.5311 +LPT 150.03 6.060 0.9256 99.350 6.0599 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 7166.20 16230.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 971.64 233.95 63.192 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 971.64 233.95 63.192 +Duct1 0.0025 0.4307 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 971.64 233.95 63.192 +Duct2 0.0025 0.4386 365.99 +Duct3 0.0050 0.2995 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3515 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.2976 1317.29 321.42 209.255 +Duct5 0.0075 0.4603 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.8962 1317.29 321.42 209.255 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 602.72 144.13 17.308 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5524 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7738.3 23251.4 34257.8 +LP_Shaft 3579.0 60840.2 41458.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2527.47 0.9940 0.0550 3.24164 0.01980 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.700 0.9975 1.0000 0.9975 2706.36 0.905 1006.8 31263.3 +Core_Nozz 1.539 0.9999 1.0000 0.9999 862.88 0.821 1397.9 7958.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 160 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 10000.0 27.00 1074.54 17243.5 0.5064 8732.64 5.9998 442.93 15.148 2326.2 2269.6 1807.1 + core size:20.42 Q: 163.07 Maximum Thrust: 28738.7 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1074.54 11.285 526.35 125.79 0.0000 1409.71 10.106 510.01 6531.4 0.4000 1.40038 +FS_2 Inlet.Fl_O 1074.54 11.228 526.35 125.79 0.0000 1416.80 9.749 505.51 5943.4 0.4537 1.40038 +FS_21 Fan.Fl_O 1074.54 16.044 588.25 140.65 0.0000 1048.20 14.059 566.49 4515.2 0.4385 1.39922 +FS_13 Splitter.Fl_O2 921.03 16.044 588.25 140.65 0.0000 898.45 13.965 565.41 3795.6 0.4497 1.39922 +FS_22 Splitter.Fl_O1 153.51 16.044 588.25 140.65 0.0000 149.75 14.501 571.52 719.5 0.3828 1.39922 +FS_23 Duct1.Fl_O 153.51 16.004 588.25 140.65 0.0000 150.12 14.465 571.52 721.3 0.3828 1.39922 +FS_24 LPC.Fl_O 153.51 32.473 741.50 177.61 0.0000 83.06 28.661 715.73 366.0 0.4268 1.39460 +FS_25 Duct2.Fl_O 153.51 32.392 741.50 177.61 0.0000 83.27 28.590 715.73 366.9 0.4268 1.39460 +FS_3 HPC.Fl_O 153.51 170.941 1241.84 302.00 0.0000 20.42 160.346 1220.72 119.9 0.3073 1.36552 +FS_36 Bld3.Fl_O 139.69 170.941 1241.84 302.00 0.0000 18.58 160.346 1220.72 109.1 0.3073 1.36552 +FS_4 Burner.Fl_O 142.12 161.539 2326.22 609.11 0.0174 27.38 160.499 2322.71 483.4 0.0995 1.30614 +FS_45 HPT.Fl_O 155.94 59.191 1807.14 459.44 0.0158 72.27 55.777 1780.99 439.1 0.3005 1.32451 +FS_48 Duct3.Fl_O 155.94 58.895 1807.14 459.44 0.0158 72.63 55.498 1780.99 441.4 0.3005 1.32451 +FS_5 LPT.Fl_O 155.94 13.852 1297.11 320.69 0.0158 261.62 12.917 1273.73 1477.4 0.3229 1.35114 +FS_7 Duct4.Fl_O 155.94 13.713 1297.11 320.69 0.0158 264.26 13.226 1284.96 2018.9 0.2318 1.35114 +FS_9 Core_Nozz.Fl_O 155.94 13.713 1297.11 320.69 0.0158 264.26 10.106 1197.63 862.8 0.6839 1.35114 +FS_15 BypBld.Fl_O 921.03 16.044 588.25 140.65 0.0000 898.45 13.965 565.41 3795.6 0.4497 1.39922 +FS_17 Duct5.Fl_O 921.03 15.924 588.25 140.65 0.0000 905.24 13.860 565.41 3824.3 0.4497 1.39922 +FS_19 Byp_Nozz.Fl_O 921.03 15.924 588.25 140.65 0.0000 905.24 10.106 516.58 2706.4 0.8328 1.39922 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1416.80 1.429 0.9130 3242.597 1.1176 0.9173 -22587.0 40.11 18.66 +LPC 150.12 2.029 0.8556 3067.260 1.2605 0.8690 -8026.7 27.11 17.13 +HPC 83.27 5.277 0.8653 6272.825 1.6748 0.8915 -27017.3 25.33 25.46 +HPT 27.38 2.729 0.9149 155.506 1.2418 0.9049 27017.2 +LPT 72.63 4.252 0.9225 76.841 1.3932 0.9079 30612.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2716.59 1.299 0.9432 0.822 1.9689 0.5215 1.4369 0.9679 3943.9586 +LPC 161.03 1.315 0.8912 0.837 1.6586 0.9323 3.2631 0.9600 3662.6571 +HPC 197.97 20.773 0.8537 0.987 2.1375 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.070 0.9332 101.563 5.0697 1.4085 0.4249 0.9803 1.5311 +LPT 150.92 5.536 0.9213 94.735 5.5361 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6531.41 14792.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 919.82 221.14 52.690 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 919.82 221.14 52.690 +Duct1 0.0025 0.3828 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 919.82 221.14 52.690 +Duct2 0.0025 0.4268 365.99 +Duct3 0.0050 0.3005 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3229 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.3728 1241.84 302.00 170.941 +Duct5 0.0075 0.4497 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.4430 1241.84 302.00 170.941 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 588.25 140.65 16.044 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9998 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7500.2 18919.1 27017.2 +LP_Shaft 3266.5 49220.2 30612.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2326.22 0.9940 0.0550 2.42573 0.01736 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.576 0.9975 1.0000 0.9975 2706.36 0.833 925.7 26500.2 +Core_Nozz 1.357 0.9999 1.0000 0.9999 862.88 0.684 1142.3 5536.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 161 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 10000.0 27.00 947.04 11495.5 0.5239 6022.76 6.5647 442.93 11.692 2092.4 2042.9 1615.6 + core size:20.77 Q: 163.07 Maximum Thrust: 28738.7 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 947.04 11.285 526.35 125.79 0.0000 1242.45 10.106 510.01 5756.5 0.4000 1.40038 +FS_2 Inlet.Fl_O 947.04 11.228 526.35 125.79 0.0000 1248.70 10.125 511.02 5943.4 0.3871 1.40038 +FS_21 Fan.Fl_O 947.04 14.681 572.24 136.81 0.0000 995.75 13.070 553.56 4515.2 0.4109 1.39949 +FS_13 Splitter.Fl_O2 821.85 14.681 572.24 136.81 0.0000 864.12 12.946 552.06 3795.6 0.4277 1.39949 +FS_22 Splitter.Fl_O1 125.19 14.681 572.24 136.81 0.0000 131.63 13.621 560.12 719.5 0.3291 1.39949 +FS_23 Duct1.Fl_O 125.19 14.644 572.24 136.81 0.0000 131.96 13.587 560.12 721.3 0.3291 1.39949 +FS_24 LPC.Fl_O 125.19 26.325 694.94 166.35 0.0000 80.90 23.419 672.24 366.0 0.4126 1.39618 +FS_25 Duct2.Fl_O 125.19 26.259 694.94 166.35 0.0000 81.10 23.361 672.24 366.9 0.4126 1.39618 +FS_3 HPC.Fl_O 125.19 131.935 1151.06 278.88 0.0000 20.77 123.452 1130.51 119.9 0.3126 1.37123 +FS_36 Bld3.Fl_O 113.92 131.935 1151.06 278.88 0.0000 18.90 123.452 1130.51 109.1 0.3126 1.37123 +FS_4 Burner.Fl_O 115.60 124.679 2092.39 539.62 0.0147 27.37 123.877 2089.16 483.4 0.0991 1.31458 +FS_45 HPT.Fl_O 126.86 45.184 1615.63 405.41 0.0134 72.83 42.535 1591.29 439.1 0.3018 1.33501 +FS_48 Duct3.Fl_O 126.86 44.958 1615.63 405.41 0.0134 73.19 42.323 1591.29 441.4 0.3018 1.33501 +FS_5 LPT.Fl_O 126.86 12.403 1197.76 294.06 0.0134 228.44 11.777 1181.49 1477.4 0.2767 1.35904 +FS_7 Duct4.Fl_O 126.86 12.279 1197.76 294.06 0.0134 230.74 11.949 1189.19 2018.9 0.2003 1.35904 +FS_9 Core_Nozz.Fl_O 126.86 12.279 1197.76 294.06 0.0134 230.74 10.106 1137.53 862.9 0.5412 1.35904 +FS_15 BypBld.Fl_O 821.85 14.681 572.24 136.81 0.0000 864.12 12.946 552.06 3795.6 0.4277 1.39949 +FS_17 Duct5.Fl_O 821.85 14.571 572.24 136.81 0.0000 870.65 12.849 552.06 3824.3 0.4277 1.39949 +FS_19 Byp_Nozz.Fl_O 821.85 14.571 572.24 136.81 0.0000 870.65 10.106 515.41 2706.4 0.7423 1.39949 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1248.70 1.308 0.9136 2844.758 1.0872 0.9169 -14754.4 44.22 18.58 +LPC 131.96 1.798 0.8478 2728.314 1.2144 0.8598 -5232.3 27.71 14.44 +HPC 81.10 5.024 0.8647 6232.055 1.6563 0.8907 -19933.7 29.14 29.32 +HPT 27.37 2.759 0.9153 157.703 1.2511 0.9050 19933.7 +LPT 73.19 3.625 0.9164 71.296 1.3489 0.9022 19986.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2394.21 1.214 0.9439 0.721 1.9598 0.5215 1.4369 0.9679 3943.9586 +LPC 141.55 1.244 0.8831 0.745 1.6361 0.9323 3.2631 0.9600 3662.6571 +HPC 192.81 19.604 0.8531 0.980 2.1724 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.141 0.9337 102.998 5.1409 1.4085 0.4249 0.9803 1.5311 +LPT 152.09 4.662 0.9152 87.900 4.6616 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5756.46 13037.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 857.02 205.73 41.741 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 857.02 205.73 41.741 +Duct1 0.0025 0.3291 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 857.02 205.73 41.741 +Duct2 0.0025 0.4126 365.99 +Duct3 0.0050 0.3018 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2767 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.3817 1151.06 278.88 131.935 +Duct5 0.0075 0.4277 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.8855 1151.06 278.88 131.935 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 572.24 136.81 14.681 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.5647 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7213.7 14513.2 19933.7 +LP_Shaft 2865.7 36629.3 19986.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2092.39 0.9940 0.0550 1.67299 0.01469 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.442 0.9975 1.0000 0.9975 2706.36 0.742 824.2 21052.7 +Core_Nozz 1.215 0.9999 1.0000 0.9999 862.88 0.541 882.7 3480.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 162 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 10000.0 27.00 781.77 5747.6 0.6023 3461.86 7.3675 442.93 8.030 1780.7 1740.6 1363.4 + core size:21.34 Q: 163.07 Maximum Thrust: 28738.7 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 781.77 11.285 526.35 125.79 0.0000 1025.62 10.106 510.01 4751.9 0.4000 1.40038 +FS_2 Inlet.Fl_O 781.77 11.228 526.35 125.79 0.0000 1030.79 10.506 516.44 5943.4 0.3096 1.40038 +FS_21 Fan.Fl_O 781.77 13.206 553.81 132.38 0.0000 898.96 12.056 539.58 4515.2 0.3630 1.39983 +FS_13 Splitter.Fl_O2 688.34 13.206 553.81 132.38 0.0000 791.52 11.930 537.96 3795.6 0.3837 1.39983 +FS_22 Splitter.Fl_O1 93.43 13.206 553.81 132.38 0.0000 107.43 12.589 546.29 719.5 0.2624 1.39983 +FS_23 Duct1.Fl_O 93.43 13.173 553.81 132.38 0.0000 107.70 12.557 546.29 721.3 0.2624 1.39983 +FS_24 LPC.Fl_O 93.43 19.698 634.34 151.73 0.0000 77.09 17.751 615.81 366.0 0.3886 1.39830 +FS_25 Duct2.Fl_O 93.43 19.648 634.34 151.73 0.0000 77.28 17.707 615.81 366.9 0.3886 1.39830 +FS_3 HPC.Fl_O 93.43 90.617 1028.47 248.07 0.0000 21.34 84.446 1008.70 119.9 0.3212 1.37893 +FS_36 Bld3.Fl_O 85.02 90.617 1028.47 248.07 0.0000 19.42 84.446 1008.70 109.1 0.3212 1.37893 +FS_4 Burner.Fl_O 85.98 85.633 1780.66 449.91 0.0113 27.34 85.083 1777.82 483.4 0.0985 1.32874 +FS_45 HPT.Fl_O 94.39 30.659 1363.41 336.57 0.0103 73.36 28.835 1341.83 439.1 0.3024 1.35079 +FS_48 Duct3.Fl_O 94.39 30.505 1363.41 336.57 0.0103 73.73 28.691 1341.83 441.4 0.3024 1.35079 +FS_5 LPT.Fl_O 94.39 11.287 1079.05 262.87 0.0103 177.26 10.953 1070.33 1477.4 0.2100 1.36869 +FS_7 Duct4.Fl_O 94.39 11.174 1079.05 262.87 0.0103 179.05 10.996 1074.38 2018.9 0.1534 1.36869 +FS_9 Core_Nozz.Fl_O 94.39 11.174 1079.05 262.87 0.0103 179.05 10.106 1050.14 862.9 0.3858 1.36869 +FS_15 BypBld.Fl_O 688.34 13.206 553.81 132.38 0.0000 791.52 11.930 537.96 3795.6 0.3837 1.39983 +FS_17 Duct5.Fl_O 688.34 13.107 553.81 132.38 0.0000 797.51 11.841 537.96 3824.3 0.3837 1.39983 +FS_19 Byp_Nozz.Fl_O 688.34 13.107 553.81 132.38 0.0000 797.51 10.106 514.13 2706.4 0.6209 1.39983 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1030.79 1.176 0.9103 2272.022 1.0522 0.9124 -7284.2 51.58 16.97 +LPC 107.70 1.495 0.8365 2214.993 1.1454 0.8455 -2558.3 34.20 12.01 +HPC 77.28 4.612 0.8629 6164.136 1.6213 0.8883 -12735.3 35.77 36.16 +HPT 27.34 2.793 0.9162 161.547 1.2648 0.9054 12735.6 +LPT 73.73 2.703 0.9015 61.986 1.2635 0.8890 9842.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1976.39 1.123 0.9405 0.576 2.0429 0.5215 1.4369 0.9679 3943.9586 +LPC 115.53 1.152 0.8713 0.605 1.6990 0.9323 3.2631 0.9600 3662.6571 +HPC 183.72 17.697 0.8513 0.970 2.2252 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.220 0.9346 105.509 5.2203 1.4085 0.4249 0.9803 1.5311 +LPT 153.19 3.375 0.9003 76.421 3.3751 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4751.88 10762.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 773.84 185.45 30.045 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 773.84 185.45 30.045 +Duct1 0.0025 0.2624 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 773.84 185.45 30.045 +Duct2 0.0025 0.3886 365.99 +Duct3 0.0050 0.3024 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2100 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.2700 1028.47 248.07 90.617 +Duct5 0.0075 0.3837 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.1386 1028.47 248.07 90.617 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 553.81 132.38 13.206 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.3675 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6816.9 9812.2 12735.6 +LP_Shaft 2288.8 22585.3 9842.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1780.66 0.9940 0.0550 0.96163 0.01131 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.297 0.9975 1.0000 0.9975 2706.36 0.621 688.6 14731.4 +Core_Nozz 1.106 0.9999 1.0000 0.9999 862.88 0.386 606.3 1778.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 163 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 4/ 14/ 1/ 2 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 10000.0 27.00 1315.60 27158.0 0.5675 15410.99 5.2238 553.67 21.357 2730.0 2661.4 2141.0 + core size:19.92 Q: 254.80 Maximum Thrust: 27158.0 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1315.60 11.989 535.54 128.00 0.0000 1638.72 10.106 510.01 6397.4 0.5000 1.40020 +FS_2 Inlet.Fl_O 1315.60 11.929 535.54 128.00 0.0000 1646.97 9.631 503.75 5943.4 0.5613 1.40020 +FS_21 Fan.Fl_O 1315.60 19.324 624.81 149.44 0.0000 1098.12 16.652 598.85 4515.2 0.4662 1.39856 +FS_13 Splitter.Fl_O2 1104.22 19.324 624.81 149.44 0.0000 921.68 16.662 598.96 3795.6 0.4652 1.39856 +FS_22 Splitter.Fl_O1 211.38 19.324 624.81 149.44 0.0000 176.44 16.598 598.30 719.5 0.4713 1.39856 +FS_23 Duct1.Fl_O 211.38 19.276 624.81 149.44 0.0000 176.88 16.556 598.30 721.3 0.4713 1.39856 +FS_24 LPC.Fl_O 211.38 45.778 824.94 197.89 0.0000 85.58 40.011 794.28 366.0 0.4440 1.39076 +FS_25 Duct2.Fl_O 211.38 45.664 824.94 197.89 0.0000 85.80 39.911 794.28 366.9 0.4440 1.39076 +FS_3 HPC.Fl_O 211.38 256.040 1397.88 342.35 0.0000 19.92 240.992 1375.80 119.9 0.2999 1.35602 +FS_36 Bld3.Fl_O 192.36 256.040 1397.88 342.35 0.0000 18.13 240.992 1375.80 109.1 0.2999 1.35602 +FS_4 Burner.Fl_O 196.64 241.958 2730.00 733.18 0.0223 27.40 240.399 2725.99 483.4 0.1000 1.29378 +FS_45 HPT.Fl_O 215.66 90.331 2141.00 557.12 0.0203 71.29 85.268 2112.00 439.1 0.2977 1.30928 +FS_48 Duct3.Fl_O 215.66 89.880 2141.00 557.12 0.0203 71.64 84.841 2112.00 441.4 0.2977 1.30928 +FS_5 LPT.Fl_O 215.66 18.714 1508.56 378.82 0.0203 288.84 17.142 1475.58 1477.4 0.3642 1.33590 +FS_7 Duct4.Fl_O 215.66 18.527 1508.56 378.82 0.0203 291.75 17.716 1491.68 2018.9 0.2593 1.33590 +FS_9 Core_Nozz.Fl_O 215.66 18.527 1508.56 378.82 0.0203 291.75 10.106 1292.65 862.9 0.9859 1.33590 +FS_15 BypBld.Fl_O 1104.22 19.324 624.81 149.44 0.0000 921.68 16.662 598.96 3795.6 0.4652 1.39856 +FS_17 Duct5.Fl_O 1104.22 19.179 624.81 149.44 0.0000 928.65 16.537 598.96 3824.3 0.4652 1.39856 +FS_19 Byp_Nozz.Fl_O 1104.22 19.179 624.81 149.44 0.0000 928.65 10.131 520.72 2706.4 1.0000 1.39856 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1646.97 1.620 0.8858 3800.499 1.1667 0.8933 -39913.4 27.09 17.62 +LPC 176.88 2.375 0.8667 3518.538 1.3203 0.8818 -14491.5 28.73 22.51 +HPC 85.80 5.607 0.8644 6331.607 1.6945 0.8914 -43204.4 20.47 20.51 +HPT 27.40 2.679 0.9142 152.827 1.2280 0.9048 43204.5 +LPT 71.64 4.803 0.9301 83.461 1.4192 0.9160 54404.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3157.84 1.431 0.9151 0.964 2.2218 0.5215 1.4369 0.9679 3943.9586 +LPC 189.73 1.421 0.9028 0.961 1.7557 0.9323 3.2631 0.9600 3662.6571 +HPC 203.97 22.298 0.8528 0.996 2.0640 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.951 0.9325 99.814 4.9507 1.4085 0.4249 0.9803 1.5311 +LPT 148.87 6.305 0.9289 102.897 6.3049 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6397.37 22639.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1030.00 248.46 76.484 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1030.00 248.46 76.484 +Duct1 0.0025 0.4713 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1030.00 248.46 76.484 +Duct2 0.0025 0.4440 365.99 +Duct3 0.0050 0.2977 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3642 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.3984 1397.88 342.35 256.040 +Duct5 0.0075 0.4652 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.6261 1397.88 342.35 256.040 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 624.81 149.44 19.324 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.2238 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7985.1 28417.3 43204.5 +LP_Shaft 3861.8 73991.0 54404.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2730.00 0.9940 0.0550 4.28083 0.02225 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.898 0.9975 1.0000 0.9975 2706.36 1.000 1116.0 38368.7 +Core_Nozz 1.833 0.9999 1.0000 0.9999 862.88 0.986 1705.0 11428.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 164 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 10000.0 27.00 1278.27 24442.3 0.5589 13660.97 5.4408 553.67 19.671 2632.8 2567.1 2059.3 + core size:20.05 Q: 254.80 Maximum Thrust: 27158.0 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1278.27 11.989 535.54 128.00 0.0000 1592.23 10.106 510.01 6215.9 0.5000 1.40020 +FS_2 Inlet.Fl_O 1278.27 11.929 535.54 128.00 0.0000 1600.24 9.800 506.27 5943.4 0.5373 1.40020 +FS_21 Fan.Fl_O 1278.27 18.802 618.09 147.82 0.0000 1090.70 16.244 592.85 4515.2 0.4620 1.39871 +FS_13 Splitter.Fl_O2 1079.81 18.802 618.09 147.82 0.0000 921.35 16.214 592.53 3795.6 0.4650 1.39871 +FS_22 Splitter.Fl_O1 198.47 18.802 618.09 147.82 0.0000 169.34 16.399 594.45 719.5 0.4465 1.39871 +FS_23 Duct1.Fl_O 198.47 18.755 618.09 147.82 0.0000 169.77 16.358 594.45 721.3 0.4465 1.39871 +FS_24 LPC.Fl_O 198.47 42.648 805.65 193.19 0.0000 85.23 37.327 775.96 366.0 0.4415 1.39167 +FS_25 Duct2.Fl_O 198.47 42.541 805.65 193.19 0.0000 85.45 37.234 775.96 366.9 0.4415 1.39167 +FS_3 HPC.Fl_O 198.47 235.830 1362.69 333.19 0.0000 20.05 221.779 1340.77 119.9 0.3018 1.35810 +FS_36 Bld3.Fl_O 180.60 235.830 1362.69 333.19 0.0000 18.24 221.779 1340.77 109.1 0.3018 1.35810 +FS_4 Burner.Fl_O 184.40 222.859 2632.79 702.82 0.0210 27.40 221.423 2628.90 483.4 0.0999 1.29650 +FS_45 HPT.Fl_O 202.26 82.661 2059.30 532.81 0.0191 71.65 77.977 2030.86 439.1 0.2990 1.31265 +FS_48 Duct3.Fl_O 202.26 82.248 2059.30 532.81 0.0191 72.01 77.587 2030.86 441.4 0.2990 1.31265 +FS_5 LPT.Fl_O 202.26 17.306 1451.72 363.00 0.0191 287.35 15.869 1420.10 1477.4 0.3614 1.33974 +FS_7 Duct4.Fl_O 202.26 17.133 1451.72 363.00 0.0191 290.25 16.392 1435.52 2018.9 0.2575 1.33974 +FS_9 Core_Nozz.Fl_O 202.26 17.133 1451.72 363.00 0.0191 290.25 10.106 1267.81 862.9 0.9149 1.33974 +FS_15 BypBld.Fl_O 1079.81 18.802 618.09 147.82 0.0000 921.35 16.214 592.53 3795.6 0.4650 1.39871 +FS_17 Duct5.Fl_O 1079.81 18.661 618.09 147.82 0.0000 928.32 16.092 592.53 3824.3 0.4650 1.39871 +FS_19 Byp_Nozz.Fl_O 1079.81 18.661 618.09 147.82 0.0000 928.32 10.106 518.78 2706.3 0.9785 1.39871 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1600.24 1.576 0.9000 3649.932 1.1541 0.9062 -35857.4 30.56 18.12 +LPC 169.77 2.274 0.8642 3397.464 1.3034 0.8789 -12739.2 28.50 21.14 +HPC 85.45 5.544 0.8645 6322.141 1.6914 0.8914 -39310.4 21.56 21.63 +HPT 27.40 2.696 0.9145 153.562 1.2318 0.9049 39310.1 +LPT 72.01 4.753 0.9276 81.729 1.4185 0.9130 48595.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3068.30 1.401 0.9298 0.925 2.1147 0.5215 1.4369 0.9679 3943.9586 +LPC 182.10 1.390 0.9002 0.928 1.7314 0.9323 3.2631 0.9600 3662.6571 +HPC 203.14 22.004 0.8528 0.994 2.0903 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 4.992 0.9329 100.294 4.9919 1.4085 0.4249 0.9803 1.5311 +LPT 149.63 6.235 0.9264 100.762 6.2347 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6215.85 21997.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1004.84 242.19 70.858 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1004.84 242.19 70.858 +Duct1 0.0025 0.4465 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1004.84 242.19 70.858 +Duct2 0.0025 0.4415 365.99 +Duct3 0.0050 0.2990 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3614 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.9463 1362.69 333.19 235.830 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.9156 1362.69 333.19 235.830 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 618.09 147.82 18.802 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.4408 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7879.4 26202.7 39310.1 +LP_Shaft 3708.8 68817.2 48595.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2632.79 0.9940 0.0550 3.79472 0.02101 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.846 0.9975 1.0000 0.9975 2706.36 0.978 1090.0 36580.7 +Core_Nozz 1.695 0.9999 1.0000 0.9999 862.88 0.915 1568.3 9858.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 165 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 4/ 14/ 1/ 2 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 10000.0 27.00 1236.11 21726.8 0.5548 12053.16 5.6377 553.67 18.094 2535.3 2472.8 1979.4 + core size:20.20 Q: 254.80 Maximum Thrust: 27158.0 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1236.11 11.989 535.54 128.00 0.0000 1539.71 10.106 510.01 6010.8 0.5000 1.40020 +FS_2 Inlet.Fl_O 1236.11 11.929 535.54 128.00 0.0000 1547.46 9.976 508.86 5943.4 0.5117 1.40020 +FS_21 Fan.Fl_O 1236.11 18.212 611.38 146.21 0.0000 1082.95 15.777 586.85 4515.2 0.4576 1.39885 +FS_13 Splitter.Fl_O2 1049.88 18.212 611.38 146.21 0.0000 919.80 15.715 586.20 3795.6 0.4639 1.39885 +FS_22 Splitter.Fl_O1 186.23 18.212 611.38 146.21 0.0000 163.15 16.080 590.05 719.5 0.4256 1.39885 +FS_23 Duct1.Fl_O 186.23 18.166 611.38 146.21 0.0000 163.56 16.040 590.05 721.3 0.4256 1.39885 +FS_24 LPC.Fl_O 186.23 40.134 790.42 189.48 0.0000 84.18 35.271 762.14 366.0 0.4344 1.39241 +FS_25 Duct2.Fl_O 186.23 40.033 790.42 189.48 0.0000 84.39 35.183 762.14 366.9 0.4344 1.39241 +FS_3 HPC.Fl_O 186.23 216.919 1329.20 324.50 0.0000 20.20 203.786 1307.37 119.9 0.3041 1.36011 +FS_36 Bld3.Fl_O 169.47 216.919 1329.20 324.50 0.0000 18.38 203.786 1307.37 109.1 0.3041 1.36011 +FS_4 Burner.Fl_O 172.81 204.989 2535.35 672.66 0.0198 27.39 203.668 2531.57 483.4 0.0998 1.29950 +FS_45 HPT.Fl_O 189.58 75.757 1979.36 509.25 0.0180 71.84 71.441 1951.63 439.1 0.2995 1.31620 +FS_48 Duct3.Fl_O 189.58 75.378 1979.36 509.25 0.0180 72.20 71.084 1951.63 441.4 0.2995 1.31620 +FS_5 LPT.Fl_O 189.58 16.137 1397.32 347.99 0.0180 283.37 14.839 1367.61 1477.4 0.3550 1.34362 +FS_7 Duct4.Fl_O 189.58 15.976 1397.32 347.99 0.0180 286.24 15.305 1382.06 2018.9 0.2533 1.34362 +FS_9 Core_Nozz.Fl_O 189.58 15.976 1397.32 347.99 0.0180 286.24 10.106 1241.37 863.0 0.8477 1.34362 +FS_15 BypBld.Fl_O 1049.88 18.212 611.38 146.21 0.0000 919.80 15.715 586.20 3795.6 0.4639 1.39885 +FS_17 Duct5.Fl_O 1049.88 18.075 611.38 146.21 0.0000 926.75 15.598 586.20 3824.3 0.4639 1.39885 +FS_19 Byp_Nozz.Fl_O 1049.88 18.075 611.38 146.21 0.0000 926.75 10.106 517.83 2706.3 0.9505 1.39885 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1547.46 1.527 0.9070 3529.343 1.1416 0.9123 -31851.7 34.31 18.71 +LPC 163.56 2.209 0.8611 3303.203 1.2928 0.8755 -11402.1 27.52 19.42 +HPC 84.39 5.418 0.8653 6296.745 1.6816 0.8918 -35573.6 23.22 23.32 +HPT 27.39 2.706 0.9146 154.377 1.2347 0.9048 35574.6 +LPT 72.20 4.671 0.9263 80.609 1.4165 0.9115 43253.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2966.85 1.367 0.9370 0.895 2.0549 0.5215 1.4369 0.9679 3943.9586 +LPC 175.44 1.371 0.8969 0.902 1.6942 0.9323 3.2631 0.9600 3662.6571 +HPC 200.62 21.426 0.8536 0.990 2.1094 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.015 0.9330 100.826 5.0149 1.4085 0.4249 0.9803 1.5311 +LPT 150.02 6.121 0.9251 99.381 6.1211 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6010.82 21271.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 982.90 236.74 65.947 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 982.90 236.74 65.947 +Duct1 0.0025 0.4256 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 982.90 236.74 65.947 +Duct2 0.0025 0.4344 365.99 +Duct3 0.0050 0.2995 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3550 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.5179 1329.20 324.50 216.919 +Duct5 0.0075 0.4639 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.2425 1329.20 324.50 216.919 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 611.38 146.21 18.212 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.6377 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7773.2 24036.6 35574.6 +LP_Shaft 3586.3 63344.4 43253.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2535.35 0.9940 0.0550 3.34810 0.01976 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.789 0.9975 1.0000 0.9975 2706.36 0.950 1057.8 34518.3 +Core_Nozz 1.581 0.9999 1.0000 0.9999 862.88 0.848 1439.2 8480.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 166 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 10000.0 27.00 1138.29 16294.6 0.5588 9104.84 6.1137 553.67 14.906 2339.3 2282.7 1818.5 + core size:20.48 Q: 254.80 Maximum Thrust: 27158.0 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1138.29 11.989 535.54 128.00 0.0000 1417.87 10.106 510.01 5535.2 0.5000 1.40020 +FS_2 Inlet.Fl_O 1138.29 11.929 535.54 128.00 0.0000 1425.00 10.335 514.03 5943.4 0.4572 1.40020 +FS_21 Fan.Fl_O 1138.29 16.937 597.36 142.84 0.0000 1059.93 14.786 574.65 4515.2 0.4449 1.39908 +FS_13 Splitter.Fl_O2 978.28 16.937 597.36 142.84 0.0000 910.94 14.669 573.35 3795.6 0.4579 1.39908 +FS_22 Splitter.Fl_O1 160.01 16.937 597.36 142.84 0.0000 149.00 15.327 580.57 719.5 0.3806 1.39908 +FS_23 Duct1.Fl_O 160.01 16.895 597.36 142.84 0.0000 149.37 15.289 580.57 721.3 0.3806 1.39908 +FS_24 LPC.Fl_O 160.01 34.474 754.54 180.77 0.0000 82.27 30.516 728.95 366.0 0.4217 1.39407 +FS_25 Duct2.Fl_O 160.01 34.388 754.54 180.77 0.0000 82.48 30.440 728.95 366.9 0.4217 1.39407 +FS_3 HPC.Fl_O 160.01 178.702 1256.71 305.81 0.0000 20.48 167.552 1235.24 119.9 0.3084 1.36458 +FS_36 Bld3.Fl_O 145.61 178.702 1256.71 305.81 0.0000 18.64 167.552 1235.24 109.1 0.3084 1.36458 +FS_4 Burner.Fl_O 148.14 168.873 2339.27 612.93 0.0174 27.38 167.787 2335.74 483.4 0.0995 1.30578 +FS_45 HPT.Fl_O 162.54 61.928 1818.49 462.62 0.0158 72.23 58.360 1792.24 439.1 0.3003 1.32403 +FS_48 Duct3.Fl_O 162.54 61.618 1818.49 462.62 0.0158 72.59 58.068 1792.24 441.4 0.3003 1.32403 +FS_5 LPT.Fl_O 162.54 14.186 1299.58 321.35 0.0158 266.53 13.189 1275.17 1477.4 0.3298 1.35098 +FS_7 Duct4.Fl_O 162.54 14.045 1299.58 321.35 0.0158 269.22 13.526 1286.93 2018.9 0.2365 1.35098 +FS_9 Core_Nozz.Fl_O 162.54 14.045 1299.58 321.35 0.0158 269.22 10.106 1192.44 862.9 0.7112 1.35098 +FS_15 BypBld.Fl_O 978.28 16.937 597.36 142.84 0.0000 910.94 14.669 573.35 3795.6 0.4579 1.39908 +FS_17 Duct5.Fl_O 978.28 16.810 597.36 142.84 0.0000 917.82 14.559 573.35 3824.3 0.4579 1.39908 +FS_19 Byp_Nozz.Fl_O 978.28 16.810 597.36 142.84 0.0000 917.82 10.106 516.53 2706.4 0.8845 1.39908 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1425.00 1.420 0.9125 3241.180 1.1154 0.9167 -23903.3 41.65 19.62 +LPC 149.37 2.040 0.8538 3068.898 1.2631 0.8676 -8587.2 26.10 16.42 +HPC 82.48 5.197 0.8656 6257.262 1.6655 0.8914 -28309.3 26.33 26.48 +HPT 27.38 2.727 0.9150 156.041 1.2413 0.9050 28309.3 +LPT 72.59 4.343 0.9221 77.232 1.3993 0.9071 32490.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2732.26 1.292 0.9427 0.822 2.0116 0.5215 1.4369 0.9679 3943.9586 +LPC 160.22 1.319 0.8894 0.838 1.6343 0.9323 3.2631 0.9600 3662.6571 +HPC 196.08 20.400 0.8539 0.984 2.1411 0.4206 0.2163 1.0137 6357.1603 +HPT 30.12 5.065 0.9333 101.913 5.0645 1.4085 0.4249 0.9803 1.5311 +LPT 150.83 5.664 0.9209 95.218 5.6640 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5535.17 19588.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 933.57 224.53 55.530 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 933.57 224.53 55.530 +Duct1 0.0025 0.3806 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 933.57 224.53 55.530 +Duct2 0.0025 0.4217 365.99 +Duct3 0.0050 0.3003 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3298 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.6005 1256.71 305.81 178.702 +Duct5 0.0075 0.4579 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.8008 1256.71 305.81 178.702 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 597.36 142.84 16.937 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.1137 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7547.1 19700.8 28309.3 +LP_Shaft 3293.5 51812.2 32490.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2339.27 0.9940 0.0550 2.52912 0.01737 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.663 0.9975 1.0000 0.9975 2706.36 0.885 983.2 29894.2 +Core_Nozz 1.390 0.9999 1.0000 0.9999 862.88 0.711 1185.4 5988.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 167 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 10000.0 27.00 1019.66 10863.3 0.5842 6346.26 6.7424 553.67 11.627 2109.5 2060.0 1630.4 + core size:20.85 Q: 254.80 Maximum Thrust: 27158.0 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1019.66 11.989 535.54 128.00 0.0000 1270.10 10.106 510.01 4958.3 0.5000 1.40020 +FS_2 Inlet.Fl_O 1019.66 11.929 535.54 128.00 0.0000 1276.49 10.697 519.11 5943.4 0.3976 1.40020 +FS_21 Fan.Fl_O 1019.66 15.553 581.75 139.09 0.0000 1020.40 13.746 561.60 4515.2 0.4238 1.39933 +FS_13 Splitter.Fl_O2 887.96 15.553 581.75 139.09 0.0000 888.61 13.590 559.77 3795.6 0.4433 1.39933 +FS_22 Splitter.Fl_O1 131.70 15.553 581.75 139.09 0.0000 131.79 14.426 569.40 719.5 0.3295 1.39933 +FS_23 Duct1.Fl_O 131.70 15.514 581.75 139.09 0.0000 132.12 14.390 569.40 721.3 0.3295 1.39933 +FS_24 LPC.Fl_O 131.70 28.315 710.25 170.04 0.0000 79.99 25.270 687.69 366.0 0.4069 1.39567 +FS_25 Duct2.Fl_O 131.70 28.244 710.25 170.04 0.0000 80.19 25.207 687.69 366.9 0.4069 1.39567 +FS_3 HPC.Fl_O 131.70 139.389 1169.09 283.46 0.0000 20.85 130.358 1148.10 119.9 0.3139 1.37009 +FS_36 Bld3.Fl_O 119.85 139.389 1169.09 283.46 0.0000 18.97 130.358 1148.10 109.1 0.3139 1.37009 +FS_4 Burner.Fl_O 121.61 131.723 2109.54 544.55 0.0147 27.36 130.876 2106.29 483.4 0.0991 1.31402 +FS_45 HPT.Fl_O 133.46 47.791 1630.37 409.45 0.0134 72.76 44.995 1605.90 439.1 0.3016 1.33427 +FS_48 Duct3.Fl_O 133.46 47.552 1630.37 409.45 0.0134 73.13 44.770 1605.90 441.4 0.3016 1.33427 +FS_5 LPT.Fl_O 133.46 12.643 1198.12 294.16 0.0134 235.79 11.961 1180.68 1477.4 0.2865 1.35900 +FS_7 Duct4.Fl_O 133.46 12.516 1198.12 294.16 0.0134 238.17 12.158 1188.96 2018.9 0.2070 1.35900 +FS_9 Core_Nozz.Fl_O 133.46 12.516 1198.12 294.16 0.0134 238.17 10.106 1132.09 862.9 0.5679 1.35900 +FS_15 BypBld.Fl_O 887.96 15.553 581.75 139.09 0.0000 888.61 13.590 559.77 3795.6 0.4433 1.39933 +FS_17 Duct5.Fl_O 887.96 15.436 581.75 139.09 0.0000 895.32 13.488 559.77 3824.3 0.4433 1.39933 +FS_19 Byp_Nozz.Fl_O 887.96 15.436 581.75 139.09 0.0000 895.32 10.106 515.42 2706.4 0.8020 1.39933 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1276.49 1.304 0.9126 2870.690 1.0863 0.9159 -16002.2 46.94 20.18 +LPC 132.12 1.825 0.8457 2754.320 1.2209 0.8582 -5767.7 26.10 13.75 +HPC 80.19 4.935 0.8646 6216.697 1.6460 0.8903 -21132.4 30.33 30.54 +HPT 27.36 2.756 0.9154 158.389 1.2504 0.9051 21132.5 +LPT 73.13 3.761 0.9180 72.243 1.3608 0.9036 21769.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2447.50 1.211 0.9428 0.728 2.0297 0.5215 1.4369 0.9679 3943.9586 +LPC 141.72 1.253 0.8809 0.752 1.6026 0.9323 3.2631 0.9600 3662.6571 +HPC 190.64 19.191 0.8530 0.978 2.1743 0.4206 0.2163 1.0137 6357.1603 +HPT 30.10 5.133 0.9338 103.447 5.1334 1.4085 0.4249 0.9803 1.5311 +LPT 151.95 4.852 0.9168 89.066 4.8519 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4958.31 17546.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 873.37 209.74 44.527 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 873.37 209.74 44.527 +Duct1 0.0025 0.3295 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 873.37 209.74 44.527 +Duct2 0.0025 0.4069 365.99 +Duct3 0.0050 0.3016 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2865 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.6094 1169.09 283.46 139.389 +Duct5 0.0075 0.4433 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.2434 1169.09 283.46 139.389 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 581.75 139.09 15.553 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.7424 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7274.8 15256.9 21132.5 +LP_Shaft 2917.0 39196.5 21769.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2109.54 0.9940 0.0550 1.76285 0.01471 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.527 0.9975 1.0000 0.9975 2706.36 0.802 890.5 24576.7 +Core_Nozz 1.238 0.9999 1.0000 0.9999 862.88 0.568 924.2 3833.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:48 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 168 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 10000.0 27.00 867.60 5431.6 0.6873 3732.98 7.6914 553.67 8.139 1807.4 1767.1 1385.5 + core size:21.40 Q: 254.80 Maximum Thrust: 27158.0 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 867.60 11.989 535.54 128.00 0.0000 1080.69 10.106 510.01 4218.9 0.5000 1.40020 +FS_2 Inlet.Fl_O 867.60 11.929 535.54 128.00 0.0000 1086.13 11.069 524.21 5943.4 0.3286 1.40020 +FS_21 Fan.Fl_O 867.60 14.033 563.76 134.77 0.0000 947.22 12.659 547.41 4515.2 0.3865 1.39964 +FS_13 Splitter.Fl_O2 767.78 14.033 563.76 134.77 0.0000 838.24 12.488 545.28 3795.6 0.4116 1.39964 +FS_22 Splitter.Fl_O1 99.82 14.033 563.76 134.77 0.0000 108.98 13.357 555.87 719.5 0.2665 1.39964 +FS_23 Duct1.Fl_O 99.82 13.998 563.76 134.77 0.0000 109.26 13.324 555.87 721.3 0.2665 1.39964 +FS_24 LPC.Fl_O 99.82 21.535 651.91 155.96 0.0000 76.37 19.451 633.29 366.0 0.3843 1.39775 +FS_25 Duct2.Fl_O 99.82 21.481 651.91 155.96 0.0000 76.56 19.402 633.29 366.9 0.3843 1.39775 +FS_3 HPC.Fl_O 99.82 97.571 1051.20 253.75 0.0000 21.40 90.879 1030.91 119.9 0.3226 1.37751 +FS_36 Bld3.Fl_O 90.84 97.571 1051.20 253.75 0.0000 19.48 90.879 1030.91 109.1 0.3226 1.37751 +FS_4 Burner.Fl_O 91.88 92.204 1807.37 457.37 0.0114 27.34 91.613 1804.50 483.4 0.0985 1.32751 +FS_45 HPT.Fl_O 100.86 33.042 1385.53 342.45 0.0104 73.32 31.079 1363.70 439.1 0.3024 1.34940 +FS_48 Duct3.Fl_O 100.86 32.877 1385.53 342.45 0.0104 73.69 30.923 1363.70 441.4 0.3024 1.34940 +FS_5 LPT.Fl_O 100.86 11.443 1080.40 263.23 0.0104 186.94 11.065 1070.65 1477.4 0.2222 1.36854 +FS_7 Duct4.Fl_O 100.86 11.329 1080.40 263.23 0.0104 188.83 11.128 1075.19 2018.9 0.1620 1.36854 +FS_9 Core_Nozz.Fl_O 100.86 11.329 1080.40 263.23 0.0104 188.83 10.106 1047.56 863.0 0.4117 1.36854 +FS_15 BypBld.Fl_O 767.78 14.033 563.76 134.77 0.0000 838.24 12.488 545.28 3795.6 0.4116 1.39964 +FS_17 Duct5.Fl_O 767.78 13.928 563.76 134.77 0.0000 844.58 12.395 545.28 3824.3 0.4116 1.39964 +FS_19 Byp_Nozz.Fl_O 767.78 13.928 563.76 134.77 0.0000 844.58 10.106 514.36 2706.3 0.6927 1.39964 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1086.13 1.176 0.9023 2338.782 1.0527 0.9046 -8311.0 55.81 19.79 +LPC 109.26 1.538 0.8357 2279.506 1.1564 0.8454 -2993.4 31.17 11.38 +HPC 76.56 4.542 0.8627 6150.471 1.6125 0.8879 -13811.5 36.87 37.32 +HPT 27.34 2.791 0.9163 162.193 1.2637 0.9055 13811.9 +LPT 73.69 2.873 0.9050 63.846 1.2824 0.8921 11304.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2082.51 1.123 0.9322 0.593 2.1574 0.5215 1.4369 0.9679 3943.9586 +LPC 117.19 1.165 0.8705 0.622 1.6465 0.9323 3.2631 0.9600 3662.6571 +HPC 182.02 17.375 0.8511 0.967 2.2353 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.214 0.9347 105.931 5.2141 1.4085 0.4249 0.9803 1.5311 +LPT 153.11 3.613 0.9038 78.714 3.6128 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4218.88 14930.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 793.32 190.19 32.628 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 793.32 190.19 32.628 +Duct1 0.0025 0.2665 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 793.32 190.19 32.628 +Duct2 0.0025 0.3843 365.99 +Duct3 0.0050 0.3024 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2222 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.4938 1051.20 253.75 97.571 +Duct5 0.0075 0.4116 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.4903 1051.20 253.75 97.571 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 563.76 134.77 14.033 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.6914 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6895.4 10520.4 13811.9 +LP_Shaft 2376.5 24981.9 11304.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1807.37 0.9940 0.0550 1.03694 0.01142 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.378 0.9975 1.0000 0.9975 2706.36 0.693 768.4 18336.0 +Core_Nozz 1.121 0.9999 1.0000 0.9999 862.88 0.412 646.2 2025.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 169 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 15000.0 0.00 1046.77 25009.3 0.4573 11435.56 5.0138 317.33 22.818 2505.4 2441.7 1959.3 + core size:19.91 Q: 75.30 Maximum Thrust: 25009.3 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1046.77 8.828 473.58 113.15 0.0000 1665.05 8.293 465.18 9871.3 0.3000 1.40116 +FS_2 Inlet.Fl_O 1046.77 8.775 473.58 113.15 0.0000 1675.11 7.005 443.99 5943.4 0.5763 1.40116 +FS_21 Fan.Fl_O 1046.77 14.499 557.62 133.30 0.0000 1100.11 12.486 534.30 4515.2 0.4671 1.39976 +FS_13 Splitter.Fl_O2 872.71 14.499 557.62 133.30 0.0000 917.18 12.525 534.79 3795.6 0.4620 1.39976 +FS_22 Splitter.Fl_O1 174.06 14.499 557.62 133.30 0.0000 182.93 12.264 531.57 719.5 0.4949 1.39976 +FS_23 Duct1.Fl_O 174.06 14.463 557.62 133.30 0.0000 183.39 12.233 531.57 721.3 0.4949 1.39976 +FS_24 LPC.Fl_O 174.06 35.909 747.24 179.00 0.0000 85.50 31.396 719.37 366.0 0.4429 1.39437 +FS_25 Duct2.Fl_O 174.06 35.819 747.24 179.00 0.0000 85.72 31.318 719.37 366.9 0.4429 1.39437 +FS_3 HPC.Fl_O 174.06 201.445 1274.63 310.41 0.0000 19.91 189.625 1254.22 119.9 0.2989 1.36346 +FS_36 Bld3.Fl_O 158.40 201.445 1274.63 310.41 0.0000 18.11 189.625 1254.22 109.1 0.2989 1.36346 +FS_4 Burner.Fl_O 161.57 190.365 2505.38 664.00 0.0201 27.41 189.137 2501.64 483.4 0.0998 1.29996 +FS_45 HPT.Fl_O 177.24 71.366 1959.31 503.68 0.0182 70.94 67.409 1932.57 439.1 0.2952 1.31676 +FS_48 Duct3.Fl_O 177.24 71.010 1959.31 503.68 0.0182 71.29 67.072 1932.57 441.4 0.2952 1.31676 +FS_5 LPT.Fl_O 177.24 14.644 1366.49 339.82 0.0182 288.71 13.416 1336.05 1477.4 0.3626 1.34528 +FS_7 Duct4.Fl_O 177.24 14.497 1366.49 339.82 0.0182 291.63 13.864 1350.90 2018.9 0.2583 1.34528 +FS_9 Core_Nozz.Fl_O 177.24 14.497 1366.49 339.82 0.0182 291.63 8.293 1181.93 862.9 0.9412 1.34528 +FS_15 BypBld.Fl_O 872.71 14.499 557.62 133.30 0.0000 917.18 12.525 534.79 3795.6 0.4620 1.39976 +FS_17 Duct5.Fl_O 872.71 14.390 557.62 133.30 0.0000 924.11 12.431 534.79 3824.3 0.4620 1.39976 +FS_19 Byp_Nozz.Fl_O 872.71 14.390 557.62 133.30 0.0000 924.11 8.293 476.30 2706.4 0.9231 1.39976 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.652 0.8704 3944.235 1.1775 0.8793 -29837.1 24.25 17.02 +LPC 183.39 2.483 0.8685 3634.860 1.3400 0.8840 -11255.5 28.58 23.46 +HPC 85.72 5.624 0.8649 6330.041 1.7058 0.8920 -32364.0 19.95 19.99 +HPT 27.41 2.667 0.9134 151.794 1.2309 0.9036 32365.3 +LPT 71.29 4.849 0.9326 85.145 1.4338 0.9186 41090.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.454 0.8992 1.000 2.3358 0.5215 1.4369 0.9679 3943.9586 +LPC 196.72 1.454 0.9047 0.992 1.7716 0.9323 3.2631 0.9600 3662.6571 +HPC 203.79 22.376 0.8532 0.996 2.0422 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.924 0.9317 99.139 4.9245 1.4085 0.4249 0.9803 1.5311 +LPT 148.13 6.369 0.9314 104.974 6.3694 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 9871.26 10324.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 935.44 224.99 60.083 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 935.44 224.99 60.083 +Duct1 0.0025 0.4949 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 935.44 224.99 60.083 +Duct2 0.0025 0.4429 365.99 +Duct3 0.0050 0.2952 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3626 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.0922 1274.63 310.41 201.445 +Duct5 0.0075 0.4620 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.5734 1274.63 310.41 201.445 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 557.62 133.30 14.499 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0138 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7597.9 22372.9 32365.3 +LP_Shaft 3768.9 57261.3 41090.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2505.38 0.9940 0.0550 3.17654 0.02005 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.735 0.9975 1.0000 0.9975 2706.36 0.923 985.6 26732.7 +Core_Nozz 1.748 0.9999 1.0000 0.9999 862.88 0.941 1561.3 8600.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 170 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 15000.0 0.00 1011.85 22508.3 0.4436 9984.71 5.2922 317.33 20.655 2409.2 2348.2 1876.5 + core size:19.99 Q: 75.30 Maximum Thrust: 25009.3 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1011.85 8.828 473.58 113.15 0.0000 1609.49 8.293 465.18 9541.9 0.3000 1.40116 +FS_2 Inlet.Fl_O 1011.85 8.775 473.58 113.15 0.0000 1619.21 7.160 446.78 5943.4 0.5467 1.40116 +FS_21 Fan.Fl_O 1011.85 14.103 550.24 131.52 0.0000 1086.02 12.204 527.96 4515.2 0.4591 1.39990 +FS_13 Splitter.Fl_O2 851.04 14.103 550.24 131.52 0.0000 913.42 12.202 527.94 3795.6 0.4594 1.39990 +FS_22 Splitter.Fl_O1 160.81 14.103 550.24 131.52 0.0000 172.60 12.217 528.12 719.5 0.4575 1.39990 +FS_23 Duct1.Fl_O 160.81 14.067 550.24 131.52 0.0000 173.03 12.186 528.12 721.3 0.4575 1.39990 +FS_24 LPC.Fl_O 160.81 32.299 719.91 172.38 0.0000 86.20 28.162 692.46 366.0 0.4474 1.39535 +FS_25 Duct2.Fl_O 160.81 32.218 719.91 172.38 0.0000 86.42 28.091 692.46 366.9 0.4474 1.39535 +FS_3 HPC.Fl_O 160.81 182.350 1233.79 299.94 0.0000 19.99 171.557 1213.76 119.9 0.3000 1.36602 +FS_36 Bld3.Fl_O 146.34 182.350 1233.79 299.94 0.0000 18.19 171.557 1213.76 109.1 0.3000 1.36602 +FS_4 Burner.Fl_O 149.11 172.320 2409.18 634.66 0.0190 27.41 171.209 2405.56 483.4 0.0997 1.30290 +FS_45 HPT.Fl_O 163.58 63.837 1876.46 479.65 0.0172 71.63 60.224 1850.07 439.1 0.2980 1.32065 +FS_48 Duct3.Fl_O 163.58 63.518 1876.46 479.65 0.0172 71.99 59.923 1850.07 441.4 0.2980 1.32065 +FS_5 LPT.Fl_O 163.58 13.447 1315.02 325.83 0.0172 284.67 12.354 1286.44 1477.4 0.3561 1.34908 +FS_7 Duct4.Fl_O 163.58 13.312 1315.02 325.83 0.0172 287.55 12.748 1300.35 2018.9 0.2540 1.34908 +FS_9 Core_Nozz.Fl_O 163.58 13.312 1315.02 325.83 0.0172 287.55 8.293 1162.10 862.9 0.8608 1.34908 +FS_15 BypBld.Fl_O 851.04 14.103 550.24 131.52 0.0000 913.42 12.202 527.94 3795.6 0.4594 1.39990 +FS_17 Duct5.Fl_O 851.04 13.997 550.24 131.52 0.0000 920.33 12.110 527.94 3824.3 0.4594 1.39990 +FS_19 Byp_Nozz.Fl_O 851.04 13.997 550.24 131.52 0.0000 920.33 8.293 473.72 2706.4 0.8978 1.39990 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1619.21 1.607 0.8980 3709.351 1.1619 0.9047 -26303.5 28.13 17.15 +LPC 173.03 2.296 0.8661 3441.268 1.3084 0.8807 -9296.1 29.49 22.40 +HPC 86.42 5.660 0.8632 6348.771 1.7138 0.8908 -29022.7 20.06 20.06 +HPT 27.41 2.699 0.9139 152.387 1.2362 0.9040 29022.6 +LPT 71.99 4.724 0.9282 81.824 1.4269 0.9135 35599.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3104.66 1.423 0.9278 0.941 2.1051 0.5215 1.4369 0.9679 3943.9586 +LPC 185.60 1.397 0.9022 0.940 1.7628 0.9323 3.2631 0.9600 3662.6571 +HPC 205.45 22.541 0.8516 0.999 2.0718 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 5.000 0.9322 99.527 4.9997 1.4085 0.4249 0.9803 1.5311 +LPT 149.59 6.195 0.9270 100.878 6.1945 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 9541.89 9979.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 903.07 217.03 54.213 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 903.07 217.03 54.213 +Duct1 0.0025 0.4575 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 903.07 217.03 54.213 +Duct2 0.0025 0.4474 365.99 +Duct3 0.0050 0.2980 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3561 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.6284 1233.79 299.94 182.350 +Duct5 0.0075 0.4594 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.8446 1233.79 299.94 182.350 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 550.24 131.52 14.103 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.2922 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7479.7 20379.3 29022.6 +LP_Shaft 3544.4 52751.3 35599.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2409.18 0.9940 0.0550 2.77353 0.01895 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.688 0.9975 1.0000 0.9975 2706.36 0.898 955.9 25284.2 +Core_Nozz 1.605 0.9999 1.0000 0.9999 862.88 0.861 1416.9 7203.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 171 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 15000.0 0.00 970.83 20007.5 0.4362 8727.49 5.4803 317.33 18.841 2313.6 2255.6 1797.2 + core size:20.13 Q: 75.30 Maximum Thrust: 25009.3 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 970.83 8.828 473.58 113.15 0.0000 1544.24 8.293 465.18 9155.1 0.3000 1.40116 +FS_2 Inlet.Fl_O 970.83 8.775 473.58 113.15 0.0000 1553.57 7.325 449.70 5943.4 0.5144 1.40116 +FS_21 Fan.Fl_O 970.83 13.619 543.51 129.91 0.0000 1072.39 11.840 522.20 4515.2 0.4515 1.40004 +FS_13 Splitter.Fl_O2 821.02 13.619 543.51 129.91 0.0000 906.91 11.815 521.87 3795.6 0.4551 1.40004 +FS_22 Splitter.Fl_O1 149.81 13.619 543.51 129.91 0.0000 165.48 11.971 523.84 719.5 0.4332 1.40004 +FS_23 Duct1.Fl_O 149.81 13.585 543.51 129.91 0.0000 165.90 11.941 523.84 721.3 0.4332 1.40004 +FS_24 LPC.Fl_O 149.81 29.957 702.60 168.20 0.0000 85.54 26.189 676.30 366.0 0.4429 1.39592 +FS_25 Duct2.Fl_O 149.81 29.882 702.60 168.20 0.0000 85.75 26.124 676.30 366.9 0.4429 1.39592 +FS_3 HPC.Fl_O 149.81 166.330 1199.36 291.15 0.0000 20.13 156.338 1179.51 119.9 0.3020 1.36818 +FS_36 Bld3.Fl_O 136.33 166.330 1199.36 291.15 0.0000 18.32 156.338 1179.51 109.1 0.3020 1.36818 +FS_4 Burner.Fl_O 138.75 157.181 2313.59 605.72 0.0178 27.40 156.169 2310.08 483.4 0.0995 1.30619 +FS_45 HPT.Fl_O 152.24 57.938 1797.24 456.86 0.0162 71.88 54.635 1771.53 439.1 0.2986 1.32468 +FS_48 Duct3.Fl_O 152.24 57.649 1797.24 456.86 0.0162 72.24 54.362 1771.53 441.4 0.2986 1.32468 +FS_5 LPT.Fl_O 152.24 12.557 1264.86 312.31 0.0162 278.24 11.587 1238.57 1477.4 0.3463 1.35291 +FS_7 Duct4.Fl_O 152.24 12.431 1264.86 312.31 0.0162 281.05 11.929 1251.31 2018.9 0.2475 1.35291 +FS_9 Core_Nozz.Fl_O 152.24 12.431 1264.86 312.31 0.0162 281.05 8.293 1137.22 862.9 0.7918 1.35291 +FS_15 BypBld.Fl_O 821.02 13.619 543.51 129.91 0.0000 906.91 11.815 521.87 3795.6 0.4551 1.40004 +FS_17 Duct5.Fl_O 821.02 13.517 543.51 129.91 0.0000 913.76 11.726 521.87 3824.3 0.4551 1.40004 +FS_19 Byp_Nozz.Fl_O 821.02 13.517 543.51 129.91 0.0000 913.76 8.293 472.62 2706.3 0.8651 1.40004 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1553.57 1.552 0.9074 3559.816 1.1477 0.9130 -23020.4 31.90 17.48 +LPC 165.90 2.205 0.8634 3322.913 1.2927 0.8777 -8115.2 29.03 20.82 +HPC 85.75 5.566 0.8639 6329.901 1.7070 0.8912 -26062.1 21.43 21.48 +HPT 27.40 2.713 0.9145 153.166 1.2401 0.9045 26062.0 +LPT 72.24 4.591 0.9263 80.237 1.4209 0.9114 31135.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2978.73 1.384 0.9375 0.903 2.0072 0.5215 1.4369 0.9679 3943.9586 +LPC 177.95 1.369 0.8994 0.907 1.7345 0.9323 3.2631 0.9600 3662.6571 +HPC 203.86 22.109 0.8523 0.996 2.0967 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 5.032 0.9328 100.036 5.0315 1.4085 0.4249 0.9803 1.5311 +LPT 150.11 6.009 0.9251 98.922 6.0094 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 9155.08 9575.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 879.46 211.23 49.871 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 879.46 211.23 49.871 +Duct1 0.0025 0.4332 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 879.46 211.23 49.871 +Duct2 0.0025 0.4429 365.99 +Duct3 0.0050 0.2986 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3463 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.2434 1199.36 291.15 166.330 +Duct5 0.0075 0.4551 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.2396 1199.36 291.15 166.330 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 543.51 129.91 13.619 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.4803 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7367.3 18579.6 26062.0 +LP_Shaft 3401.6 48074.5 31135.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2313.59 0.9940 0.0550 2.42430 0.01778 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.630 0.9975 1.0000 0.9975 2706.36 0.865 920.0 23477.3 +Core_Nozz 1.499 0.9999 1.0000 0.9999 862.88 0.792 1290.3 6105.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 172 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 15000.0 0.00 875.20 15005.5 0.4314 6473.32 5.8927 317.33 15.269 2122.8 2070.6 1640.8 + core size:20.40 Q: 75.30 Maximum Thrust: 25009.3 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 875.20 8.828 473.58 113.15 0.0000 1392.13 8.293 465.18 8253.3 0.3000 1.40116 +FS_2 Inlet.Fl_O 875.20 8.775 473.58 113.15 0.0000 1400.54 7.651 455.34 5943.4 0.4468 1.40116 +FS_21 Fan.Fl_O 875.20 12.583 529.98 126.66 0.0000 1033.23 11.078 511.02 4515.2 0.4304 1.40031 +FS_13 Splitter.Fl_O2 748.22 12.583 529.98 126.66 0.0000 883.33 11.017 510.22 3795.6 0.4397 1.40031 +FS_22 Splitter.Fl_O1 126.97 12.583 529.98 126.66 0.0000 149.90 11.370 514.84 719.5 0.3832 1.40031 +FS_23 Duct1.Fl_O 126.97 12.552 529.98 126.66 0.0000 150.28 11.342 514.84 721.3 0.3832 1.40031 +FS_24 LPC.Fl_O 126.97 25.208 666.09 159.38 0.0000 83.89 22.181 642.28 366.0 0.4317 1.39722 +FS_25 Duct2.Fl_O 126.97 25.145 666.09 159.38 0.0000 84.10 22.126 642.28 366.9 0.4317 1.39722 +FS_3 HPC.Fl_O 126.97 134.798 1126.70 272.73 0.0000 20.40 126.462 1107.32 119.9 0.3061 1.37276 +FS_36 Bld3.Fl_O 115.55 134.798 1126.70 272.73 0.0000 18.57 126.462 1107.32 109.1 0.3061 1.37276 +FS_4 Burner.Fl_O 117.34 127.384 2122.79 548.90 0.0156 27.39 126.564 2119.53 483.4 0.0992 1.31302 +FS_45 HPT.Fl_O 128.77 46.529 1640.78 412.62 0.0142 72.34 43.841 1616.53 439.1 0.2998 1.33324 +FS_48 Duct3.Fl_O 128.77 46.297 1640.78 412.62 0.0142 72.70 43.622 1616.53 441.4 0.2998 1.33324 +FS_5 LPT.Fl_O 128.77 11.105 1175.62 288.52 0.0142 256.57 10.387 1154.98 1477.4 0.3148 1.35992 +FS_7 Duct4.Fl_O 128.77 10.994 1175.62 288.52 0.0142 259.16 10.619 1164.87 2018.9 0.2263 1.35992 +FS_9 Core_Nozz.Fl_O 128.77 10.994 1175.62 288.52 0.0142 259.16 8.293 1090.65 863.0 0.6548 1.35992 +FS_15 BypBld.Fl_O 748.22 12.583 529.98 126.66 0.0000 883.33 11.017 510.22 3795.6 0.4397 1.40031 +FS_17 Duct5.Fl_O 748.22 12.489 529.98 126.66 0.0000 890.00 10.935 510.22 3824.3 0.4397 1.40031 +FS_19 Byp_Nozz.Fl_O 748.22 12.489 529.98 126.66 0.0000 890.00 8.293 471.39 2706.4 0.7874 1.40031 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1400.54 1.434 0.9121 3230.606 1.1191 0.9166 -16734.4 38.51 17.57 +LPC 150.28 2.008 0.8569 3053.861 1.2568 0.8702 -5877.7 28.19 17.78 +HPC 84.10 5.361 0.8649 6290.066 1.6915 0.8919 -20362.4 24.33 24.44 +HPT 27.39 2.738 0.9148 154.712 1.2476 0.9044 20362.3 +LPT 72.70 4.169 0.9223 76.209 1.3957 0.9075 22611.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2685.41 1.302 0.9423 0.819 1.9183 0.5215 1.4369 0.9679 3943.9586 +LPC 161.20 1.309 0.8926 0.834 1.6833 0.9323 3.2631 0.9600 3662.6571 +HPC 199.93 21.159 0.8532 0.989 2.1343 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.090 0.9331 101.045 5.0899 1.4085 0.4249 0.9803 1.5311 +LPT 151.07 5.421 0.9211 93.957 5.4208 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 8253.27 8632.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 829.69 199.05 41.209 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 829.69 199.05 41.209 +Duct1 0.0025 0.3832 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 829.69 199.05 41.209 +Duct2 0.0025 0.4317 365.99 +Duct3 0.0050 0.2998 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3148 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.4441 1126.70 272.73 134.798 +Duct5 0.0075 0.4397 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.9836 1126.70 272.73 134.798 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 529.98 126.66 12.583 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.8927 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7128.2 15003.2 20362.3 +LP_Shaft 3087.0 38470.0 22611.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2122.79 0.9940 0.0550 1.79814 0.01556 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.506 0.9975 1.0000 0.9975 2706.36 0.787 836.3 19448.2 +Core_Nozz 1.326 0.9999 1.0000 0.9999 862.88 0.655 1046.7 4189.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 173 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 15000.0 0.00 758.12 10003.7 0.4416 4417.27 6.3770 317.33 11.675 1901.9 1856.3 1460.2 + core size:20.75 Q: 75.30 Maximum Thrust: 25009.3 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 758.12 8.828 473.58 113.15 0.0000 1205.90 8.293 465.18 7149.2 0.3000 1.40116 +FS_2 Inlet.Fl_O 758.12 8.775 473.58 113.15 0.0000 1213.19 7.968 460.66 5943.4 0.3738 1.40116 +FS_21 Fan.Fl_O 758.12 11.480 515.10 123.10 0.0000 967.18 10.301 499.38 4515.2 0.3963 1.40058 +FS_13 Splitter.Fl_O2 655.35 11.480 515.10 123.10 0.0000 836.07 10.223 498.30 3795.6 0.4102 1.40058 +FS_22 Splitter.Fl_O1 102.77 11.480 515.10 123.10 0.0000 131.11 10.658 504.27 719.5 0.3274 1.40058 +FS_23 Duct1.Fl_O 102.77 11.451 515.10 123.10 0.0000 131.44 10.631 504.27 721.3 0.3274 1.40058 +FS_24 LPC.Fl_O 102.77 20.205 621.88 148.74 0.0000 81.85 17.914 600.91 366.0 0.4183 1.39863 +FS_25 Duct2.Fl_O 102.77 20.154 621.88 148.74 0.0000 82.05 17.869 600.91 366.9 0.4183 1.39863 +FS_3 HPC.Fl_O 102.77 103.074 1040.09 250.98 0.0000 20.75 96.466 1021.33 119.9 0.3113 1.37821 +FS_36 Bld3.Fl_O 93.52 103.074 1040.09 250.98 0.0000 18.88 96.466 1021.33 109.1 0.3113 1.37821 +FS_4 Burner.Fl_O 94.75 97.405 1901.88 484.66 0.0131 27.37 96.779 1898.89 483.4 0.0988 1.32245 +FS_45 HPT.Fl_O 104.00 35.178 1460.20 362.84 0.0119 72.90 33.113 1437.73 439.1 0.3010 1.34406 +FS_48 Duct3.Fl_O 104.00 35.002 1460.20 362.84 0.0119 73.26 32.947 1437.73 441.4 0.3010 1.34406 +FS_5 LPT.Fl_O 104.00 9.997 1086.03 264.99 0.0119 221.23 9.526 1072.05 1477.4 0.2664 1.36715 +FS_7 Duct4.Fl_O 104.00 9.897 1086.03 264.99 0.0119 223.46 9.648 1078.65 2018.9 0.1931 1.36715 +FS_9 Core_Nozz.Fl_O 104.00 9.897 1086.03 264.99 0.0119 223.46 8.293 1035.46 862.9 0.5144 1.36715 +FS_15 BypBld.Fl_O 655.35 11.480 515.10 123.10 0.0000 836.07 10.223 498.30 3795.6 0.4102 1.40058 +FS_17 Duct5.Fl_O 655.35 11.394 515.10 123.10 0.0000 842.39 10.147 498.30 3824.3 0.4102 1.40058 +FS_19 Byp_Nozz.Fl_O 655.35 11.394 515.10 123.10 0.0000 842.39 8.293 470.35 2706.4 0.6889 1.40058 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1213.19 1.308 0.9114 2809.588 1.0877 0.9147 -10669.5 41.08 16.83 +LPC 131.44 1.764 0.8494 2693.964 1.2073 0.8609 -3727.9 29.51 15.12 +HPC 82.05 5.114 0.8646 6249.004 1.6725 0.8912 -14866.1 28.03 28.20 +HPT 27.37 2.769 0.9152 156.901 1.2578 0.9045 14866.1 +LPT 73.26 3.501 0.9146 70.256 1.3445 0.9005 14397.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2326.13 1.214 0.9416 0.712 1.8820 0.5215 1.4369 0.9679 3943.9586 +LPC 140.98 1.234 0.8848 0.736 1.6720 0.9323 3.2631 0.9600 3662.6571 +HPC 195.07 20.019 0.8530 0.983 2.1734 0.4206 0.2163 1.0137 6357.1603 +HPT 30.12 5.163 0.9336 102.475 5.1634 1.4085 0.4249 0.9803 1.5311 +LPT 152.23 4.489 0.9134 86.617 4.4893 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 7149.23 7477.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 769.99 184.52 32.302 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 769.99 184.52 32.302 +Duct1 0.0025 0.3274 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 769.99 184.52 32.302 +Duct2 0.0025 0.4183 365.99 +Duct3 0.0050 0.3010 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2664 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.5969 1040.09 250.98 103.074 +Duct5 0.0075 0.4102 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.6523 1040.09 250.98 103.074 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 515.10 123.10 11.480 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.3770 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6842.6 11410.7 14866.1 +LP_Shaft 2684.7 28165.3 14397.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1901.88 0.9940 0.0550 1.22702 0.01312 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.374 0.9975 1.0000 0.9975 2706.36 0.689 730.9 14886.7 +Core_Nozz 1.193 0.9999 1.0000 0.9999 862.88 0.514 802.6 2594.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 174 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 15000.0 0.00 604.81 5001.8 0.4974 2487.73 6.9972 317.33 7.881 1606.6 1570.0 1223.0 + core size:21.31 Q: 75.30 Maximum Thrust: 25009.3 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 604.81 8.828 473.58 113.15 0.0000 962.03 8.293 465.18 5703.4 0.3000 1.40116 +FS_2 Inlet.Fl_O 604.81 8.775 473.58 113.15 0.0000 967.85 8.282 465.80 5943.4 0.2885 1.40116 +FS_21 Fan.Fl_O 604.81 10.306 498.05 119.01 0.0000 845.10 9.524 486.92 4515.2 0.3377 1.40085 +FS_13 Splitter.Fl_O2 529.18 10.306 498.05 119.01 0.0000 739.42 9.451 485.86 3795.6 0.3537 1.40085 +FS_22 Splitter.Fl_O1 75.63 10.306 498.05 119.01 0.0000 105.67 9.841 491.51 719.5 0.2576 1.40085 +FS_23 Duct1.Fl_O 75.63 10.280 498.05 119.01 0.0000 105.94 9.816 491.51 721.3 0.2576 1.40085 +FS_24 LPC.Fl_O 75.63 14.935 565.19 135.11 0.0000 77.68 13.434 548.34 366.0 0.3920 1.39962 +FS_25 Duct2.Fl_O 75.63 14.898 565.19 135.11 0.0000 77.87 13.400 548.34 366.9 0.3920 1.39962 +FS_3 HPC.Fl_O 75.63 69.573 923.03 221.93 0.0000 21.31 64.849 905.13 119.9 0.3200 1.38545 +FS_36 Bld3.Fl_O 68.82 69.573 923.03 221.93 0.0000 19.39 64.849 905.13 109.1 0.3200 1.38545 +FS_4 Burner.Fl_O 69.51 65.746 1606.58 401.60 0.0100 27.35 65.324 1603.97 483.4 0.0981 1.33774 +FS_45 HPT.Fl_O 76.32 23.467 1222.99 299.54 0.0091 73.39 22.071 1203.25 439.1 0.3014 1.36029 +FS_48 Duct3.Fl_O 76.32 23.350 1222.99 299.54 0.0091 73.76 21.960 1203.25 441.4 0.3014 1.36029 +FS_5 LPT.Fl_O 76.32 9.156 978.09 237.14 0.0091 168.22 8.912 970.91 1477.4 0.1982 1.37591 +FS_7 Duct4.Fl_O 76.32 9.064 978.09 237.14 0.0091 169.92 8.934 974.24 2018.9 0.1450 1.37591 +FS_9 Core_Nozz.Fl_O 76.32 9.064 978.09 237.14 0.0091 169.92 8.293 954.57 862.9 0.3615 1.37591 +FS_15 BypBld.Fl_O 529.18 10.306 498.05 119.01 0.0000 739.42 9.451 485.86 3795.6 0.3537 1.40085 +FS_17 Duct5.Fl_O 529.18 10.229 498.05 119.01 0.0000 745.01 9.381 485.86 3824.3 0.3537 1.40085 +FS_19 Byp_Nozz.Fl_O 529.18 10.229 498.05 119.01 0.0000 745.01 8.293 469.02 2706.4 0.5555 1.40085 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 967.85 1.174 0.9115 2202.527 1.0517 0.9136 -5015.1 46.44 13.92 +LPC 105.94 1.453 0.8360 2147.736 1.1348 0.8445 -1722.9 37.26 12.56 +HPC 77.87 4.670 0.8630 6175.574 1.6331 0.8885 -9290.1 34.88 35.22 +HPT 27.35 2.802 0.9161 160.834 1.2717 0.9049 9290.1 +LPT 73.76 2.550 0.8987 60.181 1.2504 0.8864 6738.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1855.71 1.121 0.9417 0.558 1.9131 0.5215 1.4369 0.9679 3943.9586 +LPC 113.63 1.139 0.8709 0.586 1.7508 0.9323 3.2631 0.9600 3662.6571 +HPC 185.14 17.965 0.8514 0.971 2.2175 0.4206 0.2163 1.0137 6357.1603 +HPT 30.09 5.240 0.9345 105.043 5.2403 1.4085 0.4249 0.9803 1.5311 +LPT 153.26 3.163 0.8976 74.196 3.1626 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 5703.44 5965.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 691.45 165.50 22.908 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 691.45 165.50 22.908 +Duct1 0.0025 0.2576 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 691.45 165.50 22.908 +Duct2 0.0025 0.3920 365.99 +Duct3 0.0050 0.3014 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1982 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.6470 923.03 221.93 69.573 +Duct5 0.0075 0.3537 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.1595 923.03 221.93 69.573 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 498.05 119.01 10.306 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.9972 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6446.6 7568.8 9290.1 +LP_Shaft 2104.6 16814.8 6738.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1606.58 0.9940 0.0550 0.69103 0.01004 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.233 0.9975 1.0000 0.9975 2706.36 0.555 588.5 9679.0 +Core_Nozz 1.093 0.9999 1.0000 0.9999 862.88 0.362 543.0 1288.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 175 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 11/ 31/ 2/ 8 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.300 15000.0 0.00 432.65 1250.4 0.8692 1086.88 7.2620 317.33 4.795 1244.0 1219.4 939.3 + core size:22.49 Q: 75.30 Maximum Thrust: 25009.3 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 432.65 8.828 473.58 113.15 0.0000 688.19 8.293 465.18 4080.0 0.3000 1.40116 +FS_2 Inlet.Fl_O 432.65 8.775 473.58 113.15 0.0000 692.35 8.531 469.76 5943.4 0.2012 1.40116 +FS_21 Fan.Fl_O 432.65 9.324 482.71 115.34 0.0000 657.85 8.910 476.47 4515.2 0.2554 1.40106 +FS_13 Splitter.Fl_O2 380.28 9.324 482.71 115.34 0.0000 578.22 8.869 475.85 3795.6 0.2681 1.40106 +FS_22 Splitter.Fl_O1 52.37 9.324 482.71 115.34 0.0000 79.62 9.090 479.21 719.5 0.1907 1.40106 +FS_23 Duct1.Fl_O 52.37 9.301 482.71 115.34 0.0000 79.82 9.068 479.21 721.3 0.1907 1.40106 +FS_24 LPC.Fl_O 52.37 11.089 513.57 122.73 0.0000 69.06 10.231 501.88 366.0 0.3409 1.40060 +FS_25 Duct2.Fl_O 52.37 11.061 513.57 122.73 0.0000 69.23 10.206 501.88 366.9 0.3409 1.40060 +FS_3 HPC.Fl_O 52.37 42.336 793.66 190.27 0.0000 22.49 39.105 776.09 119.9 0.3395 1.39225 +FS_36 Bld3.Fl_O 47.65 42.336 793.66 190.27 0.0000 20.46 39.105 776.09 109.1 0.3395 1.39225 +FS_4 Burner.Fl_O 47.96 40.007 1244.03 304.25 0.0063 27.28 39.752 1241.91 483.4 0.0971 1.36089 +FS_45 HPT.Fl_O 52.67 14.140 939.34 226.90 0.0058 73.66 13.293 923.45 439.1 0.3004 1.38057 +FS_48 Duct3.Fl_O 52.67 14.070 939.34 226.90 0.0058 74.03 13.226 923.45 441.4 0.3004 1.38057 +FS_5 LPT.Fl_O 52.67 8.692 836.96 201.59 0.0058 113.11 8.590 834.19 1477.4 0.1311 1.38647 +FS_7 Duct4.Fl_O 52.67 8.606 836.96 201.59 0.0058 114.26 8.550 835.46 2018.9 0.0964 1.38647 +FS_9 Core_Nozz.Fl_O 52.67 8.606 836.96 201.59 0.0058 114.26 8.293 828.38 862.9 0.2316 1.38647 +FS_15 BypBld.Fl_O 380.28 9.324 482.71 115.34 0.0000 578.22 8.869 475.85 3795.6 0.2681 1.40106 +FS_17 Duct5.Fl_O 380.28 9.254 482.71 115.34 0.0000 582.59 8.803 475.85 3824.3 0.2681 1.40106 +FS_19 Byp_Nozz.Fl_O 380.28 9.254 482.71 115.34 0.0000 582.59 8.293 467.79 2706.4 0.3986 1.40106 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 692.35 1.063 0.9087 1540.241 1.0193 0.9096 -1338.0 60.83 10.03 +LPC 79.82 1.192 0.8070 1525.608 1.0639 0.8119 -547.8 54.49 10.70 +HPC 69.23 3.828 0.8526 6015.672 1.5454 0.8772 -5004.3 50.59 51.61 +HPT 27.28 2.829 0.9181 169.716 1.2901 0.9066 5004.3 +LPT 74.03 1.619 0.8725 48.021 1.1223 0.8650 1885.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1327.49 1.044 0.9388 0.391 1.9418 0.5215 1.4369 0.9679 3943.9586 +LPC 85.62 1.059 0.8406 0.417 1.9750 0.9323 3.2631 0.9600 3662.6571 +HPC 164.59 14.071 0.8411 0.946 2.3896 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.305 0.9366 110.844 5.3054 1.4085 0.4249 0.9803 1.5311 +LPT 153.84 1.863 0.8713 59.203 1.8629 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9940 4079.96 4267.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 612.04 146.37 15.643 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 612.04 146.37 15.643 +Duct1 0.0025 0.1907 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 612.04 146.37 15.643 +Duct2 0.0025 0.3409 365.99 +Duct3 0.0050 0.3004 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1311 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.8328 793.66 190.27 42.336 +Duct5 0.0075 0.2681 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.8802 793.66 190.27 42.336 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 482.71 115.34 9.324 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.2620 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 5986.0 4390.8 5004.3 +LP_Shaft 1471.8 6729.6 1885.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1244.03 0.9940 0.0550 0.30191 0.00634 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.116 0.9975 1.0000 0.9975 2706.36 0.399 421.8 4985.3 +Core_Nozz 1.038 0.9999 1.0000 0.9999 862.88 0.232 325.2 532.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 176 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 15000.0 0.00 1091.68 24055.5 0.4999 12025.66 5.0347 423.10 22.730 2531.1 2466.9 1980.5 + core size:19.91 Q: 133.87 Maximum Thrust: 24055.5 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1091.68 9.261 480.11 114.71 0.0000 1666.72 8.293 465.18 7721.1 0.4000 1.40109 +FS_2 Inlet.Fl_O 1091.68 9.215 480.11 114.71 0.0000 1675.11 7.356 450.11 5943.4 0.5763 1.40109 +FS_21 Fan.Fl_O 1091.68 15.169 564.84 135.03 0.0000 1103.73 13.045 541.03 4515.2 0.4692 1.39962 +FS_13 Splitter.Fl_O2 910.78 15.169 564.84 135.03 0.0000 920.83 13.084 541.49 3795.6 0.4644 1.39962 +FS_22 Splitter.Fl_O1 180.90 15.169 564.84 135.03 0.0000 182.90 12.831 538.48 719.5 0.4948 1.39962 +FS_23 Duct1.Fl_O 180.90 15.131 564.84 135.03 0.0000 183.35 12.799 538.48 721.3 0.4948 1.39962 +FS_24 LPC.Fl_O 180.90 37.641 757.31 181.44 0.0000 85.34 32.932 729.21 366.0 0.4419 1.39396 +FS_25 Duct2.Fl_O 180.90 37.547 757.31 181.44 0.0000 85.56 32.849 729.21 366.9 0.4419 1.39396 +FS_3 HPC.Fl_O 180.90 210.501 1289.49 314.24 0.0000 19.91 198.140 1268.87 119.9 0.2991 1.36254 +FS_36 Bld3.Fl_O 164.62 210.501 1289.49 314.24 0.0000 18.12 198.140 1268.87 109.1 0.2991 1.36254 +FS_4 Burner.Fl_O 167.96 198.924 2531.15 671.85 0.0203 27.41 197.641 2527.38 483.4 0.0998 1.29923 +FS_45 HPT.Fl_O 184.24 74.617 1980.55 509.86 0.0185 70.91 70.483 1953.60 439.1 0.2952 1.31583 +FS_48 Duct3.Fl_O 184.24 74.243 1980.55 509.86 0.0185 71.26 70.130 1953.60 441.4 0.2952 1.31583 +FS_5 LPT.Fl_O 184.24 15.269 1381.55 343.91 0.0185 289.41 13.982 1350.67 1477.4 0.3638 1.34423 +FS_7 Duct4.Fl_O 184.24 15.116 1381.55 343.91 0.0185 292.33 14.453 1365.74 2018.9 0.2591 1.34423 +FS_9 Core_Nozz.Fl_O 184.24 15.116 1381.55 343.91 0.0185 292.33 8.293 1182.28 862.9 0.9786 1.34423 +FS_15 BypBld.Fl_O 910.78 15.169 564.84 135.03 0.0000 920.83 13.084 541.49 3795.6 0.4644 1.39962 +FS_17 Duct5.Fl_O 910.78 15.055 564.84 135.03 0.0000 927.79 12.986 541.49 3824.3 0.4644 1.39962 +FS_19 Byp_Nozz.Fl_O 910.78 15.055 564.84 135.03 0.0000 927.79 8.293 476.28 2706.3 0.9634 1.39962 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.646 0.8681 3944.235 1.1765 0.8771 -31378.3 24.61 17.36 +LPC 183.35 2.488 0.8683 3636.377 1.3407 0.8839 -11879.1 28.40 23.31 +HPC 85.56 5.606 0.8651 6325.645 1.7027 0.8921 -33989.9 20.14 20.19 +HPT 27.41 2.666 0.9135 151.928 1.2303 0.9037 33990.4 +LPT 71.26 4.862 0.9327 85.270 1.4336 0.9187 43257.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.450 0.8969 1.000 2.3634 0.5215 1.4369 0.9679 3943.9586 +LPC 196.67 1.456 0.9045 0.993 1.7669 0.9323 3.2631 0.9600 3662.6571 +HPC 203.39 22.294 0.8535 0.995 2.0435 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.921 0.9318 99.227 4.9210 1.4085 0.4249 0.9803 1.5311 +LPT 148.08 6.388 0.9315 105.127 6.3879 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 7721.07 14356.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 947.29 227.92 62.885 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 947.29 227.92 62.885 +Duct1 0.0025 0.4948 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 947.29 227.92 62.885 +Duct2 0.0025 0.4419 365.99 +Duct3 0.0050 0.2952 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3638 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.3315 1289.49 314.24 210.501 +Duct5 0.0075 0.4644 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.9495 1289.49 314.24 210.501 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 564.84 135.03 15.169 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0347 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7643.6 23355.8 33990.4 +LP_Shaft 3794.8 59869.8 43257.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2531.15 0.9940 0.0550 3.34046 0.02029 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.815 0.9975 1.0000 0.9975 2706.36 0.963 1028.5 29115.5 +Core_Nozz 1.823 0.9999 1.0000 0.9999 862.88 0.979 1623.4 9296.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 177 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 15000.0 0.00 1059.05 21650.0 0.4868 10538.66 5.3150 423.10 20.652 2435.4 2373.9 1898.4 + core size:20.00 Q: 133.87 Maximum Thrust: 24055.5 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1059.05 9.261 480.11 114.71 0.0000 1616.90 8.293 465.18 7490.3 0.4000 1.40109 +FS_2 Inlet.Fl_O 1059.05 9.215 480.11 114.71 0.0000 1625.03 7.502 452.66 5943.4 0.5497 1.40109 +FS_21 Fan.Fl_O 1059.05 14.779 557.69 133.31 0.0000 1091.98 12.763 534.80 4515.2 0.4625 1.39976 +FS_13 Splitter.Fl_O2 891.35 14.779 557.69 133.31 0.0000 919.06 12.757 534.73 3795.6 0.4632 1.39976 +FS_22 Splitter.Fl_O1 167.70 14.779 557.69 133.31 0.0000 172.92 12.794 535.17 719.5 0.4586 1.39976 +FS_23 Duct1.Fl_O 167.70 14.742 557.69 133.31 0.0000 173.35 12.762 535.17 721.3 0.4586 1.39976 +FS_24 LPC.Fl_O 167.70 34.070 731.12 175.09 0.0000 85.89 29.743 703.52 366.0 0.4454 1.39498 +FS_25 Duct2.Fl_O 167.70 33.984 731.12 175.09 0.0000 86.10 29.669 703.52 366.9 0.4454 1.39498 +FS_3 HPC.Fl_O 167.70 191.256 1249.53 303.97 0.0000 20.00 179.920 1229.26 119.9 0.3003 1.36503 +FS_36 Bld3.Fl_O 152.61 191.256 1249.53 303.97 0.0000 18.20 179.920 1229.26 109.1 0.3003 1.36503 +FS_4 Burner.Fl_O 155.54 180.737 2435.45 642.59 0.0192 27.41 179.571 2431.80 483.4 0.0997 1.30212 +FS_45 HPT.Fl_O 170.63 67.040 1898.43 485.97 0.0175 71.56 63.253 1871.85 439.1 0.2978 1.31963 +FS_48 Duct3.Fl_O 170.63 66.705 1898.43 485.97 0.0175 71.92 62.937 1871.85 441.4 0.2978 1.31963 +FS_5 LPT.Fl_O 170.63 13.982 1328.52 329.47 0.0175 287.04 12.824 1299.15 1477.4 0.3597 1.34811 +FS_7 Duct4.Fl_O 170.63 13.842 1328.52 329.47 0.0175 289.94 13.245 1313.46 2018.9 0.2564 1.34811 +FS_9 Core_Nozz.Fl_O 170.63 13.842 1328.52 329.47 0.0175 289.94 8.293 1162.28 862.9 0.8980 1.34811 +FS_15 BypBld.Fl_O 891.35 14.779 557.69 133.31 0.0000 919.06 12.757 534.73 3795.6 0.4632 1.39976 +FS_17 Duct5.Fl_O 891.35 14.668 557.69 133.31 0.0000 926.01 12.662 534.73 3824.3 0.4632 1.39976 +FS_19 Byp_Nozz.Fl_O 891.35 14.668 557.69 133.31 0.0000 926.01 8.293 473.75 2706.4 0.9403 1.39976 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1625.03 1.604 0.8954 3720.358 1.1616 0.9022 -27865.8 28.45 17.59 +LPC 173.35 2.311 0.8659 3451.915 1.3110 0.8806 -9914.3 29.10 22.18 +HPC 86.10 5.628 0.8638 6339.757 1.7091 0.8911 -30579.7 20.40 20.42 +HPT 27.41 2.696 0.9140 152.522 1.2353 0.9042 30579.7 +LPT 71.92 4.771 0.9282 82.151 1.4290 0.9134 37780.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3115.82 1.420 0.9251 0.943 2.1443 0.5215 1.4369 0.9679 3943.9586 +LPC 185.94 1.402 0.9020 0.942 1.7547 0.9323 3.2631 0.9600 3662.6571 +HPC 204.70 22.393 0.8521 0.997 2.0725 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.992 0.9323 99.615 4.9916 1.4085 0.4249 0.9803 1.5311 +LPT 149.44 6.260 0.9270 101.282 6.2604 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 7490.27 13927.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 915.99 220.20 57.025 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 915.99 220.20 57.025 +Duct1 0.0025 0.4586 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 915.99 220.20 57.025 +Duct2 0.0025 0.4454 365.99 +Duct3 0.0050 0.2978 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3597 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.8696 1249.53 303.97 191.256 +Duct5 0.0075 0.4632 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.2237 1249.53 303.97 191.256 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 557.69 133.31 14.779 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3150 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7527.0 21337.6 30579.7 +LP_Shaft 3579.4 55435.7 37780.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2435.45 0.9940 0.0550 2.92740 0.01918 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.769 0.9975 1.0000 0.9975 2706.36 0.940 1001.2 27737.8 +Core_Nozz 1.669 0.9999 1.0000 0.9999 862.88 0.898 1478.2 7839.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 178 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 15000.0 0.00 1020.45 19244.4 0.4800 9237.06 5.5154 423.10 18.889 2340.0 2281.5 1819.3 + core size:20.14 Q: 133.87 Maximum Thrust: 24055.5 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1020.45 9.261 480.11 114.71 0.0000 1557.96 8.293 465.18 7217.2 0.4000 1.40109 +FS_2 Inlet.Fl_O 1020.45 9.215 480.11 114.71 0.0000 1565.80 7.660 455.38 5943.4 0.5203 1.40109 +FS_21 Fan.Fl_O 1020.45 14.294 551.05 131.72 0.0000 1081.36 12.390 528.99 4515.2 0.4565 1.39989 +FS_13 Splitter.Fl_O2 863.82 14.294 551.05 131.72 0.0000 915.39 12.358 528.60 3795.6 0.4607 1.39989 +FS_22 Splitter.Fl_O1 156.62 14.294 551.05 131.72 0.0000 165.97 12.553 530.96 719.5 0.4348 1.39989 +FS_23 Duct1.Fl_O 156.62 14.259 551.05 131.72 0.0000 166.39 12.521 530.96 721.3 0.4348 1.39989 +FS_24 LPC.Fl_O 156.62 31.704 714.21 171.00 0.0000 85.19 27.754 687.76 366.0 0.4406 1.39554 +FS_25 Duct2.Fl_O 156.62 31.624 714.21 171.00 0.0000 85.41 27.685 687.76 366.9 0.4406 1.39554 +FS_3 HPC.Fl_O 156.62 174.927 1215.64 295.30 0.0000 20.14 164.400 1195.52 119.9 0.3024 1.36716 +FS_36 Bld3.Fl_O 142.52 174.927 1215.64 295.30 0.0000 18.33 164.400 1195.52 109.1 0.3024 1.36716 +FS_4 Burner.Fl_O 145.09 165.306 2340.03 613.62 0.0180 27.40 164.240 2336.50 483.4 0.0996 1.30532 +FS_45 HPT.Fl_O 159.19 60.995 1819.30 463.13 0.0164 71.83 57.523 1793.38 439.1 0.2986 1.32360 +FS_48 Duct3.Fl_O 159.19 60.690 1819.30 463.13 0.0164 72.19 57.235 1793.38 441.4 0.2986 1.32360 +FS_5 LPT.Fl_O 159.19 13.013 1276.70 315.48 0.0164 282.05 11.977 1249.38 1477.4 0.3519 1.35203 +FS_7 Duct4.Fl_O 159.19 12.883 1276.70 315.48 0.0164 284.90 12.347 1262.65 2018.9 0.2512 1.35203 +FS_9 Core_Nozz.Fl_O 159.19 12.883 1276.70 315.48 0.0164 284.90 8.293 1137.28 862.9 0.8280 1.35203 +FS_15 BypBld.Fl_O 863.82 14.294 551.05 131.72 0.0000 915.39 12.358 528.60 3795.6 0.4607 1.39989 +FS_17 Duct5.Fl_O 863.82 14.187 551.05 131.72 0.0000 922.31 12.265 528.60 3824.3 0.4607 1.39989 +FS_19 Byp_Nozz.Fl_O 863.82 14.187 551.05 131.72 0.0000 922.31 8.293 472.59 2706.3 0.9102 1.39989 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1565.80 1.551 0.9057 3575.828 1.1478 0.9114 -24551.3 32.28 18.06 +LPC 166.39 2.223 0.8632 3337.724 1.2961 0.8776 -8704.9 28.57 20.60 +HPC 85.41 5.531 0.8644 6321.007 1.7021 0.8915 -27544.6 21.81 21.88 +HPT 27.40 2.710 0.9145 153.335 1.2392 0.9046 27544.6 +LPT 72.19 4.664 0.9265 80.658 1.4250 0.9114 33256.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3002.25 1.384 0.9357 0.907 2.0513 0.5215 1.4369 0.9679 3943.9586 +LPC 178.47 1.375 0.8991 0.911 1.7249 0.9323 3.2631 0.9600 3662.6571 +HPC 203.04 21.948 0.8527 0.994 2.0975 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.025 0.9328 100.146 5.0250 1.4085 0.4249 0.9803 1.5311 +LPT 150.01 6.111 0.9253 99.441 6.1110 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 7217.23 13419.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 892.81 214.51 52.618 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 892.81 214.51 52.618 +Duct1 0.0025 0.4348 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 892.81 214.51 52.618 +Duct2 0.0025 0.4406 365.99 +Duct3 0.0050 0.2986 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3519 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.4817 1215.64 295.30 174.927 +Duct5 0.0075 0.4607 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.6141 1215.64 295.30 174.927 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 551.05 131.72 14.294 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5154 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7417.4 19503.8 27544.6 +LP_Shaft 3440.3 50770.2 33256.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2340.03 0.9940 0.0550 2.56585 0.01800 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.711 0.9975 1.0000 0.9975 2706.36 0.910 968.0 25987.9 +Core_Nozz 1.553 0.9999 1.0000 0.9999 862.88 0.828 1349.3 6675.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 179 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 15000.0 0.00 929.96 14433.4 0.4778 6896.94 5.9602 423.10 15.417 2149.5 2096.9 1663.2 + core size:20.43 Q: 133.87 Maximum Thrust: 24055.5 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 929.96 9.261 480.11 114.71 0.0000 1419.81 8.293 465.18 6577.3 0.4000 1.40109 +FS_2 Inlet.Fl_O 929.96 9.215 480.11 114.71 0.0000 1426.96 7.980 460.73 5943.4 0.4578 1.40109 +FS_21 Fan.Fl_O 929.96 13.239 537.56 128.48 0.0000 1050.97 11.590 517.51 4515.2 0.4399 1.40016 +FS_13 Splitter.Fl_O2 796.35 13.239 537.56 128.48 0.0000 899.97 11.517 516.57 3795.6 0.4505 1.40016 +FS_22 Splitter.Fl_O1 133.61 13.239 537.56 128.48 0.0000 151.00 11.941 521.95 719.5 0.3866 1.40016 +FS_23 Duct1.Fl_O 133.61 13.205 537.56 128.48 0.0000 151.38 11.912 521.95 721.3 0.3866 1.40016 +FS_24 LPC.Fl_O 133.61 26.952 679.17 162.54 0.0000 83.37 23.763 655.28 366.0 0.4284 1.39674 +FS_25 Duct2.Fl_O 133.61 26.885 679.17 162.54 0.0000 83.57 23.703 655.28 366.9 0.4284 1.39674 +FS_3 HPC.Fl_O 133.61 142.773 1144.47 277.22 0.0000 20.43 133.919 1124.77 119.9 0.3067 1.37164 +FS_36 Bld3.Fl_O 121.59 142.773 1144.47 277.22 0.0000 18.59 133.919 1124.77 109.1 0.3067 1.37164 +FS_4 Burner.Fl_O 123.50 134.921 2149.54 556.72 0.0158 27.39 134.052 2146.24 483.4 0.0993 1.31208 +FS_45 HPT.Fl_O 135.53 49.369 1663.22 418.86 0.0143 72.24 46.525 1638.77 439.1 0.2995 1.33204 +FS_48 Duct3.Fl_O 135.53 49.122 1663.22 418.86 0.0143 72.61 46.292 1638.77 441.4 0.2995 1.33204 +FS_5 LPT.Fl_O 135.53 11.433 1184.33 290.82 0.0143 263.24 10.651 1162.34 1477.4 0.3241 1.35925 +FS_7 Duct4.Fl_O 135.53 11.319 1184.33 290.82 0.0143 265.90 10.912 1172.91 2018.9 0.2326 1.35925 +FS_9 Core_Nozz.Fl_O 135.53 11.319 1184.33 290.82 0.0143 265.90 8.293 1090.32 862.9 0.6891 1.35925 +FS_15 BypBld.Fl_O 796.35 13.239 537.56 128.48 0.0000 899.97 11.517 516.57 3795.6 0.4505 1.40016 +FS_17 Duct5.Fl_O 796.35 13.139 537.56 128.48 0.0000 906.77 11.430 516.57 3824.3 0.4505 1.40016 +FS_19 Byp_Nozz.Fl_O 796.35 13.139 537.56 128.48 0.0000 906.77 8.293 471.24 2706.4 0.8379 1.40016 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1426.96 1.437 0.9128 3266.101 1.1197 0.9172 -18115.3 39.74 18.65 +LPC 151.38 2.041 0.8563 3086.640 1.2634 0.8700 -6437.8 27.35 17.46 +HPC 83.57 5.310 0.8652 6279.020 1.6851 0.8919 -21679.2 24.89 25.01 +HPT 27.39 2.733 0.9148 154.976 1.2465 0.9045 21679.1 +LPT 72.61 4.297 0.9223 77.051 1.4044 0.9072 24552.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2736.04 1.304 0.9430 0.828 1.9717 0.5215 1.4369 0.9679 3943.9586 +LPC 162.37 1.319 0.8920 0.843 1.6661 0.9323 3.2631 0.9600 3662.6571 +HPC 198.69 20.926 0.8536 0.988 2.1341 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.079 0.9331 101.217 5.0786 1.4085 0.4249 0.9803 1.5311 +LPT 150.87 5.599 0.9211 94.994 5.5986 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6577.27 12229.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 844.52 202.68 43.863 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 844.52 202.68 43.863 +Duct1 0.0025 0.3866 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 844.52 202.68 43.863 +Duct2 0.0025 0.4284 365.99 +Duct3 0.0050 0.2995 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3241 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.6764 1144.47 277.22 142.773 +Duct5 0.0075 0.4505 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.3486 1144.47 277.22 142.773 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 537.56 128.48 13.239 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9602 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7185.2 15846.7 21679.1 +LP_Shaft 3142.3 41036.4 24552.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2149.54 0.9940 0.0550 1.91582 0.01576 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.584 0.9975 1.0000 0.9975 2706.36 0.838 889.8 22023.4 +Core_Nozz 1.365 0.9999 1.0000 0.9999 862.88 0.689 1101.4 4639.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 180 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 15000.0 0.00 819.27 9622.3 0.4931 4744.84 6.5244 423.10 11.881 1929.8 1883.8 1483.4 + core size:20.78 Q: 133.87 Maximum Thrust: 24055.5 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 819.27 9.261 480.11 114.71 0.0000 1250.82 8.293 465.18 5794.4 0.4000 1.40109 +FS_2 Inlet.Fl_O 819.27 9.215 480.11 114.71 0.0000 1257.12 8.296 465.88 5943.4 0.3902 1.40109 +FS_21 Fan.Fl_O 819.27 12.100 522.70 124.92 0.0000 998.94 10.762 505.48 4515.2 0.4124 1.40044 +FS_13 Splitter.Fl_O2 710.39 12.100 522.70 124.92 0.0000 866.18 10.662 504.13 3795.6 0.4288 1.40044 +FS_22 Splitter.Fl_O1 108.88 12.100 522.70 124.92 0.0000 132.76 11.209 511.40 719.5 0.3322 1.40044 +FS_23 Duct1.Fl_O 108.88 12.069 522.70 124.92 0.0000 133.09 11.181 511.40 721.3 0.3322 1.40044 +FS_24 LPC.Fl_O 108.88 21.804 635.99 152.13 0.0000 81.27 19.372 614.92 366.0 0.4146 1.39826 +FS_25 Duct2.Fl_O 108.88 21.749 635.99 152.13 0.0000 81.47 19.324 614.92 366.9 0.4146 1.39826 +FS_3 HPC.Fl_O 108.88 110.034 1059.35 255.79 0.0000 20.78 102.955 1040.22 119.9 0.3120 1.37700 +FS_36 Bld3.Fl_O 99.08 110.034 1059.35 255.79 0.0000 18.91 102.955 1040.22 109.1 0.3120 1.37700 +FS_4 Burner.Fl_O 100.40 103.982 1929.77 492.60 0.0133 27.37 103.314 1926.74 483.4 0.0988 1.32124 +FS_45 HPT.Fl_O 110.20 37.617 1483.42 369.12 0.0121 72.81 35.415 1460.72 439.1 0.3008 1.34267 +FS_48 Duct3.Fl_O 110.20 37.429 1483.42 369.12 0.0121 73.17 35.238 1460.72 441.4 0.3008 1.34267 +FS_5 LPT.Fl_O 110.20 10.209 1091.30 266.37 0.0121 230.10 9.686 1076.01 1477.4 0.2781 1.36670 +FS_7 Duct4.Fl_O 110.20 10.107 1091.30 266.37 0.0121 232.43 9.832 1083.25 2018.9 0.2012 1.36670 +FS_9 Core_Nozz.Fl_O 110.20 10.107 1091.30 266.37 0.0121 232.43 8.293 1034.62 862.8 0.5449 1.36670 +FS_15 BypBld.Fl_O 710.39 12.100 522.70 124.92 0.0000 866.18 10.662 504.13 3795.6 0.4288 1.40044 +FS_17 Duct5.Fl_O 710.39 12.009 522.70 124.92 0.0000 872.73 10.582 504.13 3824.3 0.4288 1.40044 +FS_19 Byp_Nozz.Fl_O 710.39 12.009 522.70 124.92 0.0000 872.73 8.293 470.16 2706.4 0.7466 1.40044 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1257.12 1.313 0.9137 2864.741 1.0887 0.9170 -11829.1 44.13 18.61 +LPC 133.09 1.807 0.8486 2745.544 1.2167 0.8606 -4192.1 27.91 14.75 +HPC 81.47 5.059 0.8647 6238.493 1.6657 0.8911 -15969.4 28.70 28.88 +HPT 27.37 2.764 0.9153 157.256 1.2565 0.9047 15969.4 +LPT 73.17 3.666 0.9168 71.561 1.3593 0.9025 16020.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2410.35 1.218 0.9439 0.726 1.9592 0.5215 1.4369 0.9679 3943.9586 +LPC 142.76 1.247 0.8840 0.750 1.6431 0.9323 3.2631 0.9600 3662.6571 +HPC 193.68 19.765 0.8530 0.981 2.1726 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.152 0.9336 102.707 5.1523 1.4085 0.4249 0.9803 1.5311 +LPT 152.05 4.719 0.9156 88.226 4.7194 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5794.42 10773.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 786.01 188.41 34.683 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 786.01 188.41 34.683 +Duct1 0.0025 0.3322 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 786.01 188.41 34.683 +Duct2 0.0025 0.4146 365.99 +Duct3 0.0050 0.3008 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2781 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.8109 1059.35 255.79 110.034 +Duct5 0.0075 0.4288 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.9885 1059.35 255.79 110.034 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 522.70 124.92 12.100 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.5244 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6908.1 12141.2 15969.4 +LP_Shaft 2756.2 30528.7 16020.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1929.77 0.9940 0.0550 1.31801 0.01330 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.448 0.9975 1.0000 0.9975 2706.36 0.747 791.9 17485.3 +Core_Nozz 1.219 0.9999 1.0000 0.9999 862.88 0.545 849.9 2910.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 181 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 15000.0 0.00 675.46 4811.0 0.5663 2724.43 7.3342 423.10 8.137 1640.1 1602.9 1250.1 + core size:21.33 Q: 133.87 Maximum Thrust: 24055.5 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 675.46 9.261 480.11 114.71 0.0000 1031.25 8.293 465.18 4777.2 0.4000 1.40109 +FS_2 Inlet.Fl_O 675.46 9.215 480.11 114.71 0.0000 1036.44 8.615 470.95 5943.4 0.3114 1.40109 +FS_21 Fan.Fl_O 675.46 10.866 505.57 120.81 0.0000 901.97 9.913 492.47 4515.2 0.3644 1.40074 +FS_13 Splitter.Fl_O2 594.41 10.866 505.57 120.81 0.0000 793.74 9.809 490.99 3795.6 0.3849 1.40074 +FS_22 Splitter.Fl_O1 81.05 10.866 505.57 120.81 0.0000 108.22 10.350 498.59 719.5 0.2644 1.40074 +FS_23 Duct1.Fl_O 81.05 10.838 505.57 120.81 0.0000 108.50 10.324 498.59 721.3 0.2644 1.40074 +FS_24 LPC.Fl_O 81.05 16.275 580.00 138.67 0.0000 77.39 14.652 562.87 366.0 0.3903 1.39936 +FS_25 Duct2.Fl_O 81.05 16.234 580.00 138.67 0.0000 77.58 14.616 562.87 366.9 0.3903 1.39936 +FS_3 HPC.Fl_O 81.05 75.352 944.79 227.30 0.0000 21.33 70.224 926.47 119.9 0.3206 1.38412 +FS_36 Bld3.Fl_O 73.75 75.352 944.79 227.30 0.0000 19.41 70.224 926.47 109.1 0.3206 1.38412 +FS_4 Burner.Fl_O 74.51 71.208 1640.12 410.82 0.0103 27.34 70.751 1637.47 483.4 0.0982 1.33595 +FS_45 HPT.Fl_O 81.80 25.444 1250.15 306.64 0.0093 73.35 23.931 1230.07 439.1 0.3015 1.35843 +FS_48 Duct3.Fl_O 81.80 25.316 1250.15 306.64 0.0093 73.72 23.811 1230.07 441.4 0.3015 1.35843 +FS_5 LPT.Fl_O 81.80 9.278 983.69 238.58 0.0093 178.44 8.999 975.53 1477.4 0.2110 1.37542 +FS_7 Duct4.Fl_O 81.80 9.185 983.69 238.58 0.0093 180.24 9.037 979.32 2018.9 0.1540 1.37542 +FS_9 Core_Nozz.Fl_O 81.80 9.185 983.69 238.58 0.0093 180.24 8.293 956.58 862.9 0.3879 1.37542 +FS_15 BypBld.Fl_O 594.41 10.866 505.57 120.81 0.0000 793.74 9.809 490.99 3795.6 0.3849 1.40074 +FS_17 Duct5.Fl_O 594.41 10.784 505.57 120.81 0.0000 799.74 9.736 490.99 3824.3 0.3849 1.40074 +FS_19 Byp_Nozz.Fl_O 594.41 10.784 505.57 120.81 0.0000 799.74 8.293 468.96 2706.4 0.6239 1.40074 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1036.44 1.179 0.9105 2287.457 1.0530 0.9127 -5829.1 51.24 17.04 +LPC 108.50 1.502 0.8371 2229.108 1.1472 0.8462 -2047.4 34.18 12.15 +HPC 77.58 4.642 0.8630 6169.947 1.6290 0.8884 -10163.7 35.31 35.67 +HPT 27.34 2.799 0.9161 161.106 1.2703 0.9051 10164.0 +LPT 73.72 2.729 0.9018 62.244 1.2709 0.8889 7876.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1987.23 1.125 0.9407 0.580 2.0395 0.5215 1.4369 0.9679 3943.9586 +LPC 116.38 1.154 0.8719 0.609 1.7010 0.9323 3.2631 0.9600 3662.6571 +HPC 184.44 17.834 0.8513 0.971 2.2210 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.233 0.9345 105.221 5.2333 1.4085 0.4249 0.9803 1.5311 +LPT 153.18 3.411 0.9007 76.739 3.4114 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4777.25 8882.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 708.79 169.69 24.895 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 708.79 169.69 24.895 +Duct1 0.0025 0.2644 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 708.79 169.69 24.895 +Duct2 0.0025 0.3903 365.99 +Duct3 0.0050 0.3015 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2110 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.8366 944.79 227.30 75.352 +Duct5 0.0075 0.3849 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.4575 944.79 227.30 75.352 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 505.57 120.81 10.866 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.3342 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6524.5 8181.8 10164.0 +LP_Shaft 2200.8 18796.6 7876.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1640.12 0.9940 0.0550 0.75679 0.01026 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.300 0.9975 1.0000 0.9975 2706.36 0.624 660.9 12210.7 +Core_Nozz 1.108 0.9999 1.0000 0.9999 862.88 0.388 583.3 1482.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 182 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 12/ 22/ 1/10 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 15000.0 0.00 520.36 1202.7 1.0151 1220.92 8.2312 423.10 4.997 1282.3 1256.8 969.5 + core size:22.43 Q: 133.87 Maximum Thrust: 24055.5 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 520.36 9.261 480.11 114.71 0.0000 794.46 8.293 465.18 3680.3 0.4000 1.40109 +FS_2 Inlet.Fl_O 520.36 9.215 480.11 114.71 0.0000 798.46 8.870 474.89 5943.4 0.2340 1.40109 +FS_21 Fan.Fl_O 520.36 9.825 490.08 117.10 0.0000 756.56 9.239 481.51 4515.2 0.2978 1.40096 +FS_13 Splitter.Fl_O2 463.99 9.825 490.08 117.10 0.0000 674.60 9.159 480.32 3795.6 0.3182 1.40096 +FS_22 Splitter.Fl_O1 56.37 9.825 490.08 117.10 0.0000 81.96 9.564 486.31 719.5 0.1965 1.40096 +FS_23 Duct1.Fl_O 56.37 9.801 490.08 117.10 0.0000 82.16 9.540 486.31 721.3 0.1965 1.40096 +FS_24 LPC.Fl_O 56.37 12.033 526.32 125.79 0.0000 69.35 11.094 514.24 366.0 0.3426 1.40038 +FS_25 Duct2.Fl_O 56.37 12.003 526.32 125.79 0.0000 69.53 11.066 514.24 366.9 0.3426 1.40038 +FS_3 HPC.Fl_O 56.37 46.277 814.64 195.38 0.0000 22.43 42.763 796.73 119.9 0.3387 1.39124 +FS_36 Bld3.Fl_O 51.30 46.277 814.64 195.38 0.0000 20.42 42.763 796.73 109.1 0.3387 1.39124 +FS_4 Burner.Fl_O 51.64 43.732 1282.35 314.26 0.0066 27.28 43.453 1280.18 483.4 0.0972 1.35829 +FS_45 HPT.Fl_O 56.71 15.476 969.46 234.45 0.0060 73.62 14.549 953.15 439.1 0.3004 1.37852 +FS_48 Duct3.Fl_O 56.71 15.398 969.46 234.45 0.0060 73.99 14.477 953.15 441.4 0.3004 1.37852 +FS_5 LPT.Fl_O 56.71 8.747 846.25 203.91 0.0060 121.70 8.627 843.00 1477.4 0.1413 1.38586 +FS_7 Duct4.Fl_O 56.71 8.660 846.25 203.91 0.0060 122.93 8.595 844.49 2018.9 0.1039 1.38586 +FS_9 Core_Nozz.Fl_O 56.71 8.660 846.25 203.91 0.0060 122.93 8.293 836.12 863.0 0.2506 1.38586 +FS_15 BypBld.Fl_O 463.99 9.825 490.08 117.10 0.0000 674.60 9.159 480.32 3795.6 0.3182 1.40096 +FS_17 Duct5.Fl_O 463.99 9.752 490.08 117.10 0.0000 679.70 9.090 480.32 3824.3 0.3182 1.40096 +FS_19 Byp_Nozz.Fl_O 463.99 9.752 490.08 117.10 0.0000 679.70 8.293 467.87 2706.4 0.4864 1.40096 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 798.46 1.066 0.8930 1626.564 1.0208 0.8941 -1757.3 74.70 13.90 +LPC 82.16 1.228 0.8174 1609.940 1.0740 0.8227 -692.8 49.08 10.41 +HPC 69.53 3.856 0.8534 6021.054 1.5478 0.8780 -5550.6 49.95 50.95 +HPT 27.28 2.826 0.9180 169.375 1.2882 0.9066 5550.5 +LPT 73.99 1.760 0.8782 50.261 1.1456 0.8697 2450.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1530.94 1.046 0.9226 0.412 2.2176 0.5215 1.4369 0.9679 3943.9586 +LPC 88.13 1.070 0.8514 0.440 1.8930 0.9323 3.2631 0.9600 3662.6571 +HPC 165.29 14.201 0.8419 0.947 2.3850 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.297 0.9365 110.622 5.2973 1.4085 0.4249 0.9803 1.5311 +LPT 153.75 2.061 0.8771 61.965 2.0607 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3680.33 6843.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 627.74 150.14 17.024 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 627.74 150.14 17.024 +Duct1 0.0025 0.1965 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 627.74 150.14 17.024 +Duct2 0.0025 0.3426 365.99 +Duct3 0.0050 0.3004 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1413 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.9730 814.64 195.38 46.277 +Duct5 0.0075 0.3182 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.1004 814.64 195.38 46.277 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 490.08 117.10 9.825 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 8.2312 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6065.3 4806.4 5550.5 +LP_Shaft 1564.9 8222.8 2450.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1282.35 0.9940 0.0550 0.33914 0.00661 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.176 0.9975 1.0000 0.9975 2706.36 0.486 514.7 7422.9 +Core_Nozz 1.044 0.9999 1.0000 0.9999 862.88 0.251 353.4 622.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 183 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 15000.0 0.00 1149.85 23725.5 0.5439 12903.48 5.0400 528.88 22.697 2570.5 2505.3 2012.7 + core size:19.91 Q: 209.18 Maximum Thrust: 23725.5 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1149.85 9.839 488.51 116.72 0.0000 1666.72 8.293 465.18 6506.0 0.5000 1.40098 +FS_2 Inlet.Fl_O 1149.85 9.790 488.51 116.72 0.0000 1675.11 7.815 457.99 5943.4 0.5763 1.40098 +FS_21 Fan.Fl_O 1149.85 16.099 574.57 137.36 0.0000 1104.77 13.840 550.29 4515.2 0.4698 1.39945 +FS_13 Splitter.Fl_O2 959.47 16.099 574.57 137.36 0.0000 921.86 13.880 550.75 3795.6 0.4652 1.39945 +FS_22 Splitter.Fl_O1 190.37 16.099 574.57 137.36 0.0000 182.91 13.617 547.75 719.5 0.4949 1.39945 +FS_23 Duct1.Fl_O 190.37 16.058 574.57 137.36 0.0000 183.37 13.583 547.75 721.3 0.4949 1.39945 +FS_24 LPC.Fl_O 190.37 39.961 770.28 184.59 0.0000 85.32 34.965 741.74 366.0 0.4418 1.39338 +FS_25 Duct2.Fl_O 190.37 39.861 770.28 184.59 0.0000 85.53 34.877 741.74 366.9 0.4418 1.39338 +FS_3 HPC.Fl_O 190.37 223.324 1309.99 319.53 0.0000 19.91 210.215 1289.10 119.9 0.2992 1.36128 +FS_36 Bld3.Fl_O 173.24 223.324 1309.99 319.53 0.0000 18.12 210.215 1289.10 109.1 0.2992 1.36128 +FS_4 Burner.Fl_O 176.82 211.041 2570.46 683.90 0.0207 27.41 209.680 2566.65 483.4 0.0999 1.29808 +FS_45 HPT.Fl_O 193.96 79.195 2012.71 519.26 0.0188 70.90 74.809 1985.43 439.1 0.2953 1.31444 +FS_48 Duct3.Fl_O 193.96 78.799 2012.71 519.26 0.0188 71.26 74.435 1985.43 441.4 0.2953 1.31444 +FS_5 LPT.Fl_O 193.96 16.216 1405.90 350.56 0.0188 289.40 14.848 1374.59 1477.4 0.3640 1.34256 +FS_7 Duct4.Fl_O 193.96 16.053 1405.90 350.56 0.0188 292.33 15.349 1389.87 2018.9 0.2592 1.34256 +FS_9 Core_Nozz.Fl_O 193.96 16.053 1405.90 350.56 0.0188 292.33 8.597 1196.16 862.9 1.0000 1.34256 +FS_15 BypBld.Fl_O 959.47 16.099 574.57 137.36 0.0000 921.86 13.880 550.75 3795.6 0.4652 1.39945 +FS_17 Duct5.Fl_O 959.47 15.978 574.57 137.36 0.0000 928.83 13.776 550.75 3824.3 0.4652 1.39945 +FS_19 Byp_Nozz.Fl_O 959.47 15.978 574.57 137.36 0.0000 928.83 8.438 478.69 2706.3 1.0000 1.39945 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.644 0.8675 3944.235 1.1762 0.8765 -33577.3 24.72 17.46 +LPC 183.37 2.489 0.8683 3636.868 1.3406 0.8839 -12719.9 28.38 23.29 +HPC 85.53 5.603 0.8652 6324.897 1.7007 0.8922 -36346.5 20.19 20.25 +HPT 27.41 2.665 0.9136 152.029 1.2295 0.9038 36347.8 +LPT 71.26 4.860 0.9328 85.322 1.4316 0.9189 46297.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.448 0.8962 1.000 2.3714 0.5215 1.4369 0.9679 3943.9586 +LPC 196.68 1.456 0.9045 0.993 1.7665 0.9323 3.2631 0.9600 3662.6571 +HPC 203.32 22.276 0.8535 0.995 2.0445 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.918 0.9319 99.293 4.9183 1.4085 0.4249 0.9803 1.5311 +LPT 148.05 6.384 0.9316 105.191 6.3839 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6505.95 18901.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 963.05 231.82 66.739 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 963.05 231.82 66.739 +Duct1 0.0025 0.4949 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 963.05 231.82 66.739 +Duct2 0.0025 0.4418 365.99 +Duct3 0.0050 0.2953 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3640 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.6631 1309.99 319.53 223.324 +Duct5 0.0075 0.4652 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.4705 1309.99 319.53 223.324 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 574.57 137.36 16.099 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0400 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7707.8 24767.4 36347.8 +LP_Shaft 3827.8 63523.5 46297.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2570.46 0.9940 0.0550 3.58430 0.02069 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.927 0.9975 1.0000 0.9975 2706.36 1.000 1070.3 32309.5 +Core_Nozz 1.936 0.9999 1.0000 0.9999 862.88 1.000 1668.0 10317.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 184 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 15000.0 0.00 1118.95 21352.9 0.5314 11347.05 5.3176 528.88 20.701 2474.7 2412.3 1930.9 + core size:20.00 Q: 209.18 Maximum Thrust: 23725.5 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1118.95 9.839 488.51 116.72 0.0000 1621.92 8.293 465.18 6331.1 0.5000 1.40098 +FS_2 Inlet.Fl_O 1118.95 9.790 488.51 116.72 0.0000 1630.09 7.956 460.33 5943.4 0.5523 1.40098 +FS_21 Fan.Fl_O 1118.95 15.708 567.67 135.71 0.0000 1095.19 13.550 544.21 4515.2 0.4643 1.39957 +FS_13 Splitter.Fl_O2 941.83 15.708 567.67 135.71 0.0000 921.84 13.543 544.13 3795.6 0.4651 1.39957 +FS_22 Splitter.Fl_O1 177.11 15.708 567.67 135.71 0.0000 173.35 13.585 544.61 719.5 0.4602 1.39957 +FS_23 Duct1.Fl_O 177.11 15.669 567.67 135.71 0.0000 173.79 13.551 544.61 721.3 0.4602 1.39957 +FS_24 LPC.Fl_O 177.11 36.427 745.51 178.58 0.0000 85.67 31.829 717.57 366.0 0.4440 1.39444 +FS_25 Duct2.Fl_O 177.11 36.336 745.51 178.58 0.0000 85.88 31.750 717.57 366.9 0.4440 1.39444 +FS_3 HPC.Fl_O 177.11 203.687 1271.07 309.50 0.0000 20.00 191.609 1250.49 119.9 0.3005 1.36369 +FS_36 Bld3.Fl_O 161.17 203.687 1271.07 309.50 0.0000 18.20 191.609 1250.49 109.1 0.3005 1.36369 +FS_4 Burner.Fl_O 164.33 192.484 2474.67 654.49 0.0196 27.40 191.243 2470.97 483.4 0.0997 1.30099 +FS_45 HPT.Fl_O 180.27 71.489 1930.89 495.35 0.0178 71.50 67.457 1903.99 439.1 0.2977 1.31814 +FS_48 Duct3.Fl_O 180.27 71.131 1930.89 495.35 0.0178 71.86 67.120 1903.99 441.4 0.2977 1.31814 +FS_5 LPT.Fl_O 180.27 14.791 1350.44 335.40 0.0178 289.01 13.548 1320.21 1477.4 0.3629 1.34655 +FS_7 Duct4.Fl_O 180.27 14.643 1350.44 335.40 0.0178 291.93 14.002 1334.96 2018.9 0.2584 1.34655 +FS_9 Core_Nozz.Fl_O 180.27 14.643 1350.44 335.40 0.0178 291.93 8.293 1164.56 862.9 0.9498 1.34655 +FS_15 BypBld.Fl_O 941.83 15.708 567.67 135.71 0.0000 921.84 13.543 544.13 3795.6 0.4651 1.39957 +FS_17 Duct5.Fl_O 941.83 15.590 567.67 135.71 0.0000 928.80 13.442 544.13 3824.3 0.4651 1.39957 +FS_19 Byp_Nozz.Fl_O 941.83 15.590 567.67 135.71 0.0000 928.80 8.293 473.91 2706.3 0.9938 1.39957 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1630.09 1.604 0.8933 3733.195 1.1621 0.9002 -30053.7 28.43 17.78 +LPC 173.79 2.325 0.8658 3463.115 1.3133 0.8806 -10743.6 28.83 22.06 +HPC 85.88 5.606 0.8642 6333.667 1.7050 0.8913 -32807.3 20.63 20.66 +HPT 27.40 2.693 0.9141 152.644 1.2342 0.9042 32807.6 +LPT 71.86 4.809 0.9282 82.450 1.4298 0.9135 40793.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3125.40 1.421 0.9229 0.947 2.1687 0.5215 1.4369 0.9679 3943.9586 +LPC 186.41 1.406 0.9019 0.946 1.7496 0.9323 3.2631 0.9600 3662.6571 +HPC 204.16 22.291 0.8525 0.996 2.0727 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.983 0.9324 99.694 4.9835 1.4085 0.4249 0.9803 1.5311 +LPT 149.31 6.314 0.9270 101.651 6.3136 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6331.11 18393.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 933.04 224.40 60.853 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 933.04 224.40 60.853 +Duct1 0.0025 0.4602 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 933.04 224.40 60.853 +Duct2 0.0025 0.4440 365.99 +Duct3 0.0050 0.2977 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3629 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.1990 1271.07 309.50 203.687 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.7413 1271.07 309.50 203.687 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 567.67 135.71 15.708 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3176 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7593.4 22691.9 32807.6 +LP_Shaft 3623.0 59137.0 40793.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2474.67 0.9940 0.0550 3.15196 0.01956 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.880 0.9975 1.0000 0.9975 2706.36 0.994 1058.3 30979.6 +Core_Nozz 1.766 0.9999 1.0000 0.9999 862.88 0.950 1564.7 8766.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 185 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 15000.0 0.00 1082.44 18980.5 0.5253 9970.88 5.5286 528.88 18.984 2378.9 2319.6 1851.5 + core size:20.15 Q: 209.18 Maximum Thrust: 23725.5 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1082.44 9.839 488.51 116.72 0.0000 1569.01 8.293 465.18 6124.6 0.5000 1.40098 +FS_2 Inlet.Fl_O 1082.44 9.790 488.51 116.72 0.0000 1576.91 8.109 462.85 5943.4 0.5257 1.40098 +FS_21 Fan.Fl_O 1082.44 15.214 561.15 134.14 0.0000 1087.56 13.159 538.36 4515.2 0.4600 1.39969 +FS_13 Splitter.Fl_O2 916.64 15.214 561.15 134.14 0.0000 920.98 13.122 537.93 3795.6 0.4645 1.39969 +FS_22 Splitter.Fl_O1 165.80 15.214 561.15 134.14 0.0000 166.59 13.344 540.51 719.5 0.4369 1.39969 +FS_23 Duct1.Fl_O 165.80 15.176 561.15 134.14 0.0000 167.00 13.310 540.51 721.3 0.4369 1.39969 +FS_24 LPC.Fl_O 165.80 34.025 729.16 174.62 0.0000 84.91 29.820 702.40 366.0 0.4388 1.39504 +FS_25 Duct2.Fl_O 165.80 33.940 729.16 174.62 0.0000 85.12 29.745 702.40 366.9 0.4388 1.39504 +FS_3 HPC.Fl_O 165.80 186.788 1237.69 300.94 0.0000 20.15 175.538 1217.25 119.9 0.3027 1.36578 +FS_36 Bld3.Fl_O 150.88 186.788 1237.69 300.94 0.0000 18.34 175.538 1217.25 109.1 0.3027 1.36578 +FS_4 Burner.Fl_O 153.65 176.515 2378.95 625.30 0.0184 27.40 175.377 2375.36 483.4 0.0996 1.30406 +FS_45 HPT.Fl_O 168.57 65.204 1851.53 472.35 0.0167 71.78 61.497 1825.28 439.1 0.2985 1.32203 +FS_48 Duct3.Fl_O 168.57 64.878 1851.53 472.35 0.0167 72.14 61.189 1825.28 441.4 0.2985 1.32203 +FS_5 LPT.Fl_O 168.57 13.694 1296.15 320.69 0.0167 285.97 12.570 1267.60 1477.4 0.3578 1.35061 +FS_7 Duct4.Fl_O 168.57 13.557 1296.15 320.69 0.0167 288.86 12.977 1281.50 2018.9 0.2551 1.35061 +FS_9 Core_Nozz.Fl_O 168.57 13.557 1296.15 320.69 0.0167 288.86 8.293 1139.48 862.9 0.8777 1.35061 +FS_15 BypBld.Fl_O 916.64 15.214 561.15 134.14 0.0000 920.98 13.122 537.93 3795.6 0.4645 1.39969 +FS_17 Duct5.Fl_O 916.64 15.100 561.15 134.14 0.0000 927.94 13.024 537.93 3824.3 0.4645 1.39969 +FS_19 Byp_Nozz.Fl_O 916.64 15.100 561.15 134.14 0.0000 927.94 8.293 472.75 2706.4 0.9660 1.39969 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1576.91 1.554 0.9036 3594.495 1.1487 0.9095 -26674.7 32.24 18.39 +LPC 167.00 2.242 0.8630 3353.775 1.2994 0.8775 -9495.2 28.18 20.45 +HPC 85.12 5.503 0.8648 6313.981 1.6974 0.8916 -29632.8 22.11 22.18 +HPT 27.40 2.707 0.9145 153.488 1.2380 0.9047 29632.6 +LPT 72.14 4.738 0.9266 81.070 1.4285 0.9115 36170.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3023.54 1.386 0.9335 0.911 2.0846 0.5215 1.4369 0.9679 3943.9586 +LPC 179.13 1.381 0.8989 0.916 1.7173 0.9323 3.2631 0.9600 3662.6571 +HPC 202.36 21.819 0.8531 0.993 2.0976 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.018 0.9329 100.246 5.0178 1.4085 0.4249 0.9803 1.5311 +LPT 149.91 6.214 0.9254 99.950 6.2140 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6124.57 17793.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 910.42 218.83 56.332 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 910.42 218.83 56.332 +Duct1 0.0025 0.4369 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 910.42 218.83 56.332 +Duct2 0.0025 0.4388 365.99 +Duct3 0.0050 0.2985 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3578 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.8030 1237.69 300.94 186.788 +Duct5 0.0075 0.4645 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.1191 1237.69 300.94 186.788 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 561.15 134.14 15.214 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5286 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7486.3 20789.1 29632.6 +LP_Shaft 3488.4 54457.7 36170.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2378.95 0.9940 0.0550 2.76969 0.01836 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.821 0.9975 1.0000 0.9975 2706.36 0.966 1027.5 29273.0 +Core_Nozz 1.635 0.9999 1.0000 0.9999 862.88 0.878 1431.6 7500.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 186 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 15000.0 0.00 996.47 14234.0 0.5257 7482.67 6.0010 528.88 15.595 2186.6 2133.2 1694.1 + core size:20.45 Q: 209.18 Maximum Thrust: 23725.5 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 996.47 9.839 488.51 116.72 0.0000 1444.39 8.293 465.18 5638.1 0.5000 1.40098 +FS_2 Inlet.Fl_O 996.47 9.790 488.51 116.72 0.0000 1451.66 8.423 467.91 5943.4 0.4684 1.40098 +FS_21 Fan.Fl_O 996.47 14.118 547.65 130.90 0.0000 1065.84 12.301 526.50 4515.2 0.4480 1.39995 +FS_13 Splitter.Fl_O2 854.14 14.118 547.65 130.90 0.0000 913.60 12.214 525.44 3795.6 0.4595 1.39995 +FS_22 Splitter.Fl_O1 142.33 14.118 547.65 130.90 0.0000 152.24 12.709 531.43 719.5 0.3905 1.39995 +FS_23 Duct1.Fl_O 142.33 14.083 547.65 130.90 0.0000 152.62 12.677 531.43 721.3 0.3905 1.39995 +FS_24 LPC.Fl_O 142.33 29.243 695.79 166.55 0.0000 82.85 25.832 671.71 366.0 0.4251 1.39615 +FS_25 Duct2.Fl_O 142.33 29.170 695.79 166.55 0.0000 83.05 25.767 671.71 366.9 0.4251 1.39615 +FS_3 HPC.Fl_O 142.33 153.442 1167.76 283.12 0.0000 20.45 143.900 1147.65 119.9 0.3073 1.37017 +FS_36 Bld3.Fl_O 129.52 153.442 1167.76 283.12 0.0000 18.61 143.900 1147.65 109.1 0.3073 1.37017 +FS_4 Burner.Fl_O 131.60 145.003 2186.59 567.60 0.0160 27.39 144.069 2183.25 483.4 0.0993 1.31081 +FS_45 HPT.Fl_O 144.41 53.162 1694.08 427.47 0.0146 72.15 50.107 1669.33 439.1 0.2992 1.33040 +FS_48 Duct3.Fl_O 144.41 52.896 1694.08 427.47 0.0146 72.51 49.857 1669.33 441.4 0.2992 1.33040 +FS_5 LPT.Fl_O 144.41 11.907 1198.36 294.53 0.0146 270.91 11.041 1174.68 1477.4 0.3351 1.35818 +FS_7 Duct4.Fl_O 144.41 11.788 1198.36 294.53 0.0146 273.65 11.338 1186.11 2018.9 0.2400 1.35818 +FS_9 Core_Nozz.Fl_O 144.41 11.788 1198.36 294.53 0.0146 273.65 8.293 1091.53 862.9 0.7348 1.35818 +FS_15 BypBld.Fl_O 854.14 14.118 547.65 130.90 0.0000 913.60 12.214 525.44 3795.6 0.4595 1.39995 +FS_17 Duct5.Fl_O 854.14 14.012 547.65 130.90 0.0000 920.50 12.123 525.44 3824.3 0.4595 1.39995 +FS_19 Byp_Nozz.Fl_O 854.14 14.012 547.65 130.90 0.0000 920.50 8.293 471.34 2706.4 0.8988 1.39995 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1451.66 1.442 0.9119 3305.627 1.1211 0.9164 -19987.3 40.36 19.48 +LPC 152.62 2.077 0.8557 3122.041 1.2705 0.8697 -7178.9 26.51 17.15 +HPC 83.05 5.260 0.8655 6268.359 1.6783 0.8919 -23474.0 25.45 25.58 +HPT 27.39 2.728 0.9148 155.262 1.2451 0.9046 23474.6 +LPT 72.51 4.442 0.9224 77.943 1.4137 0.9068 27164.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2783.21 1.308 0.9421 0.838 2.0157 0.5215 1.4369 0.9679 3943.9586 +LPC 163.71 1.330 0.8913 0.852 1.6492 0.9323 3.2631 0.9600 3662.6571 +HPC 197.44 20.694 0.8539 0.986 2.1337 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.066 0.9332 101.404 5.0660 1.4085 0.4249 0.9803 1.5311 +LPT 150.66 5.802 0.9212 96.094 5.8018 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5638.12 16380.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 863.62 207.35 47.376 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 863.62 207.35 47.376 +Duct1 0.0025 0.3905 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 863.62 207.35 47.376 +Duct2 0.0025 0.4251 365.99 +Duct3 0.0050 0.2992 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3351 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.9816 1167.76 283.12 153.442 +Duct5 0.0075 0.4595 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.8282 1167.76 283.12 153.442 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 547.65 130.90 14.118 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.0010 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7260.2 16981.8 23474.6 +LP_Shaft 3208.1 44471.8 27164.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2186.59 0.9940 0.0550 2.07852 0.01605 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.690 0.9975 1.0000 0.9975 2706.36 0.899 954.5 25340.6 +Core_Nozz 1.421 0.9999 1.0000 0.9999 862.88 0.735 1174.9 5273.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 187 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 15000.0 0.00 891.40 9490.3 0.5458 5179.48 6.6350 528.88 12.107 1965.7 1919.2 1513.3 + core size:20.82 Q: 209.18 Maximum Thrust: 23725.5 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 891.40 9.839 488.51 116.72 0.0000 1292.09 8.293 465.18 5043.6 0.5000 1.40098 +FS_2 Inlet.Fl_O 891.40 9.790 488.51 116.72 0.0000 1298.60 8.738 472.87 5943.4 0.4060 1.40098 +FS_21 Fan.Fl_O 891.40 12.923 532.75 127.33 0.0000 1027.34 11.398 513.96 4515.2 0.4273 1.40025 +FS_13 Splitter.Fl_O2 774.65 12.923 532.75 127.33 0.0000 892.79 11.274 512.35 3795.6 0.4458 1.40025 +FS_22 Splitter.Fl_O1 116.75 12.923 532.75 127.33 0.0000 134.56 11.944 520.88 719.5 0.3374 1.40025 +FS_23 Duct1.Fl_O 116.75 12.891 532.75 127.33 0.0000 134.89 11.914 520.88 721.3 0.3374 1.40025 +FS_24 LPC.Fl_O 116.75 23.909 653.92 156.45 0.0000 80.58 21.294 632.71 366.0 0.4103 1.39768 +FS_25 Duct2.Fl_O 116.75 23.849 653.92 156.45 0.0000 80.78 21.241 632.71 366.9 0.4103 1.39768 +FS_3 HPC.Fl_O 116.75 119.123 1083.89 261.95 0.0000 20.82 111.427 1064.29 119.9 0.3129 1.37546 +FS_36 Bld3.Fl_O 106.24 119.123 1083.89 261.95 0.0000 18.95 111.427 1064.29 109.1 0.3129 1.37546 +FS_4 Burner.Fl_O 107.68 112.571 1965.71 502.89 0.0135 27.37 111.847 1962.64 483.4 0.0989 1.31973 +FS_45 HPT.Fl_O 118.19 40.805 1513.33 377.25 0.0123 72.71 38.422 1490.33 439.1 0.3006 1.34093 +FS_48 Duct3.Fl_O 118.19 40.600 1513.33 377.25 0.0123 73.08 38.230 1490.33 441.4 0.3006 1.34093 +FS_5 LPT.Fl_O 118.19 10.507 1099.52 268.52 0.0123 240.69 9.915 1082.56 1477.4 0.2924 1.36603 +FS_7 Duct4.Fl_O 118.19 10.402 1099.52 268.52 0.0123 243.12 10.092 1090.63 2018.9 0.2110 1.36603 +FS_9 Core_Nozz.Fl_O 118.19 10.402 1099.52 268.52 0.0123 243.12 8.293 1034.41 862.8 0.5843 1.36603 +FS_15 BypBld.Fl_O 774.65 12.923 532.75 127.33 0.0000 892.79 11.274 512.35 3795.6 0.4458 1.40025 +FS_17 Duct5.Fl_O 774.65 12.826 532.75 127.33 0.0000 899.53 11.189 512.35 3824.3 0.4458 1.40025 +FS_19 Byp_Nozz.Fl_O 774.65 12.826 532.75 127.33 0.0000 899.53 8.293 470.25 2706.4 0.8142 1.40025 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1298.60 1.320 0.9129 2926.371 1.0906 0.9163 -13372.3 46.35 20.13 +LPC 134.89 1.855 0.8474 2802.228 1.2274 0.8600 -4810.2 26.21 14.29 +HPC 80.78 4.995 0.8647 6226.590 1.6575 0.8909 -17426.9 29.50 29.69 +HPT 27.37 2.759 0.9153 157.691 1.2549 0.9050 17426.8 +LPT 73.08 3.864 0.9194 73.005 1.3764 0.9050 18182.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2489.89 1.223 0.9431 0.742 2.0233 0.5215 1.4369 0.9679 3943.9586 +LPC 144.69 1.262 0.8827 0.765 1.6111 0.9323 3.2631 0.9600 3662.6571 +HPC 192.04 19.467 0.8531 0.979 2.1717 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.139 0.9337 102.991 5.1395 1.4085 0.4249 0.9803 1.5311 +LPT 151.84 4.995 0.9183 90.006 4.9953 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5043.63 14652.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 806.39 193.37 37.807 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 806.39 193.37 37.807 +Duct1 0.0025 0.3374 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 806.39 193.37 37.807 +Duct2 0.0025 0.4103 365.99 +Duct3 0.0050 0.3006 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2924 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.0863 1083.89 261.95 119.123 +Duct5 0.0075 0.4458 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.4213 1083.89 261.95 119.123 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 532.75 127.33 12.923 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6350 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6991.4 13091.4 17426.8 +LP_Shaft 2840.0 33625.1 18182.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1965.71 0.9940 0.0550 1.43874 0.01354 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.547 0.9975 1.0000 0.9975 2706.36 0.814 863.7 20795.7 +Core_Nozz 1.254 0.9999 1.0000 0.9999 862.88 0.584 911.3 3347.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 188 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 15000.0 0.00 755.69 4745.2 0.6371 3023.35 7.5967 528.88 8.408 1679.1 1641.2 1281.9 + core size:21.37 Q: 209.18 Maximum Thrust: 23725.5 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 755.69 9.839 488.51 116.72 0.0000 1095.39 8.293 465.18 4275.8 0.5000 1.40098 +FS_2 Inlet.Fl_O 755.69 9.790 488.51 116.72 0.0000 1100.90 9.063 477.84 5943.4 0.3336 1.40098 +FS_21 Fan.Fl_O 755.69 11.605 515.45 123.18 0.0000 954.00 10.450 500.23 4515.2 0.3897 1.40057 +FS_13 Splitter.Fl_O2 667.79 11.605 515.45 123.18 0.0000 843.03 10.310 498.30 3795.6 0.4144 1.40057 +FS_22 Splitter.Fl_O1 87.91 11.605 515.45 123.18 0.0000 110.97 11.024 507.94 719.5 0.2717 1.40057 +FS_23 Duct1.Fl_O 87.91 11.576 515.45 123.18 0.0000 111.25 10.997 507.94 721.3 0.2717 1.40057 +FS_24 LPC.Fl_O 87.91 18.053 598.84 143.19 0.0000 76.89 16.280 581.43 366.0 0.3873 1.39906 +FS_25 Duct2.Fl_O 87.91 18.008 598.84 143.19 0.0000 77.08 16.239 581.43 366.9 0.3873 1.39906 +FS_3 HPC.Fl_O 87.91 82.727 971.53 233.92 0.0000 21.37 77.073 952.67 119.9 0.3214 1.38248 +FS_36 Bld3.Fl_O 79.99 82.727 971.53 233.92 0.0000 19.45 77.073 952.67 109.1 0.3214 1.38248 +FS_4 Burner.Fl_O 80.83 78.177 1679.09 421.57 0.0105 27.34 77.675 1676.38 483.4 0.0983 1.33393 +FS_45 HPT.Fl_O 88.75 27.972 1281.93 314.97 0.0096 73.30 26.312 1261.46 439.1 0.3015 1.35629 +FS_48 Duct3.Fl_O 88.75 27.832 1281.93 314.97 0.0096 73.67 26.180 1261.46 441.4 0.3015 1.35629 +FS_5 LPT.Fl_O 88.75 9.446 989.83 240.17 0.0096 190.73 9.120 980.40 1477.4 0.2264 1.37489 +FS_7 Duct4.Fl_O 88.75 9.352 989.83 240.17 0.0096 192.66 9.179 984.80 2018.9 0.1650 1.37489 +FS_9 Core_Nozz.Fl_O 88.75 9.352 989.83 240.17 0.0096 192.66 8.293 957.86 862.8 0.4212 1.37489 +FS_15 BypBld.Fl_O 667.79 11.605 515.45 123.18 0.0000 843.03 10.310 498.30 3795.6 0.4144 1.40057 +FS_17 Duct5.Fl_O 667.79 11.518 515.45 123.18 0.0000 849.40 10.233 498.30 3824.3 0.4144 1.40057 +FS_19 Byp_Nozz.Fl_O 667.79 11.518 515.45 123.18 0.0000 849.40 8.293 469.21 2706.4 0.7011 1.40057 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1100.90 1.185 0.9039 2383.066 1.0552 0.9063 -6903.4 54.72 19.89 +LPC 111.25 1.560 0.8369 2319.935 1.1618 0.8468 -2489.1 30.78 11.61 +HPC 77.08 4.594 0.8629 6160.360 1.6224 0.8883 -11283.6 36.03 36.44 +HPT 27.34 2.795 0.9162 161.539 1.2685 0.9053 11283.6 +LPT 73.67 2.946 0.9065 64.594 1.2951 0.8932 9392.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2110.83 1.129 0.9339 0.604 2.1424 0.5215 1.4369 0.9679 3943.9586 +LPC 119.33 1.171 0.8718 0.633 1.6442 0.9323 3.2631 0.9600 3662.6571 +HPC 183.25 17.614 0.8513 0.969 2.2271 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.224 0.9346 105.504 5.2242 1.4085 0.4249 0.9803 1.5311 +LPT 153.08 3.715 0.9054 79.636 3.7152 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4275.79 12422.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 730.52 174.95 27.489 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 730.52 174.95 27.489 +Duct1 0.0025 0.2717 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 730.52 174.95 27.489 +Duct2 0.0025 0.3873 365.99 +Duct3 0.0050 0.3015 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2264 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.0767 971.53 233.92 82.727 +Duct5 0.0075 0.4144 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.8348 971.53 233.92 82.727 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 515.45 123.18 11.605 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.5967 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6619.3 8952.9 11283.6 +LP_Shaft 2312.7 21330.1 9392.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1679.09 0.9940 0.0550 0.83982 0.01050 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.389 0.9975 1.0000 0.9975 2706.36 0.701 742.9 15419.6 +Core_Nozz 1.128 0.9999 1.0000 0.9999 862.88 0.421 633.7 1747.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 189 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 12/ 32/ 2/ 9 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 15000.0 0.00 613.82 1186.3 1.1870 1408.16 8.9369 528.88 5.254 1332.0 1305.4 1008.7 + core size:22.38 Q: 209.18 Maximum Thrust: 23725.5 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 613.82 9.839 488.51 116.72 0.0000 889.74 8.293 465.18 3473.0 0.5000 1.40098 +FS_2 Inlet.Fl_O 613.82 9.790 488.51 116.72 0.0000 894.22 9.325 481.75 5943.4 0.2645 1.40098 +FS_21 Fan.Fl_O 613.82 10.489 499.88 119.45 0.0000 844.25 9.695 488.73 4515.2 0.3373 1.40082 +FS_13 Splitter.Fl_O2 552.05 10.489 499.88 119.45 0.0000 759.29 9.567 486.88 3795.6 0.3650 1.40082 +FS_22 Splitter.Fl_O1 61.77 10.489 499.88 119.45 0.0000 84.96 10.189 495.74 719.5 0.2041 1.40082 +FS_23 Duct1.Fl_O 61.77 10.463 499.88 119.45 0.0000 85.17 10.164 495.74 721.3 0.2041 1.40082 +FS_24 LPC.Fl_O 61.77 13.359 544.02 130.03 0.0000 69.59 12.309 531.43 366.0 0.3440 1.40003 +FS_25 Duct2.Fl_O 61.77 13.326 544.02 130.03 0.0000 69.77 12.278 531.43 366.9 0.3440 1.40003 +FS_3 HPC.Fl_O 61.77 51.699 842.94 202.29 0.0000 22.38 47.792 824.55 119.9 0.3380 1.38992 +FS_36 Bld3.Fl_O 56.21 51.699 842.94 202.29 0.0000 20.37 47.792 824.55 109.1 0.3380 1.38992 +FS_4 Burner.Fl_O 56.60 48.856 1332.04 327.32 0.0070 27.29 48.544 1329.81 483.4 0.0973 1.35499 +FS_45 HPT.Fl_O 62.16 17.317 1008.74 244.33 0.0063 73.57 16.281 991.87 439.1 0.3005 1.37583 +FS_48 Duct3.Fl_O 62.16 17.230 1008.74 244.33 0.0063 73.94 16.200 991.87 441.4 0.3005 1.37583 +FS_5 LPT.Fl_O 62.16 8.829 858.26 206.91 0.0063 133.10 8.683 854.31 1477.4 0.1550 1.38504 +FS_7 Duct4.Fl_O 62.16 8.741 858.26 206.91 0.0063 134.45 8.663 856.13 2018.9 0.1138 1.38504 +FS_9 Core_Nozz.Fl_O 62.16 8.741 858.26 206.91 0.0063 134.45 8.293 845.82 862.9 0.2764 1.38504 +FS_15 BypBld.Fl_O 552.05 10.489 499.88 119.45 0.0000 759.29 9.567 486.88 3795.6 0.3650 1.40082 +FS_17 Duct5.Fl_O 552.05 10.411 499.88 119.45 0.0000 765.03 9.495 486.88 3824.3 0.3650 1.40082 +FS_19 Byp_Nozz.Fl_O 552.05 10.411 499.88 119.45 0.0000 765.03 8.293 468.38 2706.4 0.5791 1.40082 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 894.22 1.071 0.8565 1740.676 1.0233 0.8580 -2366.2 81.88 17.92 +LPC 85.17 1.277 0.8198 1720.759 1.0883 0.8260 -924.8 42.68 9.95 +HPC 69.77 3.880 0.8541 6025.518 1.5495 0.8787 -6315.3 49.39 50.37 +HPT 27.29 2.821 0.9179 169.081 1.2857 0.9067 6315.3 +LPT 73.94 1.952 0.8864 53.189 1.1753 0.8767 3291.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1714.54 1.050 0.8849 0.441 2.4223 0.5215 1.4369 0.9679 3943.9586 +LPC 91.36 1.085 0.8539 0.470 1.7928 0.9323 3.2631 0.9600 3662.6571 +HPC 165.87 14.312 0.8426 0.948 2.3807 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.287 0.9364 110.430 5.2867 1.4085 0.4249 0.9803 1.5311 +LPT 153.64 2.327 0.8853 65.575 2.3274 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3473.05 10090.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 649.25 155.32 18.947 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 649.25 155.32 18.947 +Duct1 0.0025 0.2041 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 649.25 155.32 18.947 +Duct2 0.0025 0.3440 365.99 +Duct3 0.0050 0.3005 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1550 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.1620 842.94 202.29 51.699 +Duct5 0.0075 0.3650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.3975 842.94 202.29 51.699 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 499.88 119.45 10.489 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 8.9369 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6171.0 5374.9 6315.3 +LP_Shaft 1689.3 10231.9 3291.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1332.04 0.9940 0.0550 0.39115 0.00696 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.255 0.9975 1.0000 0.9975 2706.36 0.579 613.1 10519.1 +Core_Nozz 1.054 0.9999 1.0000 0.9999 862.88 0.276 391.9 757.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 190 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 4/ 14/ 1/ 2 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 15000.0 0.00 1223.69 23956.4 0.5875 14074.89 5.0398 634.66 22.694 2620.3 2553.9 2053.5 + core size:19.90 Q: 301.21 Maximum Thrust: 23956.4 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1223.69 10.581 498.77 119.18 0.0000 1666.72 8.293 465.18 5769.8 0.6000 1.40084 +FS_2 Inlet.Fl_O 1223.69 10.528 498.77 119.18 0.0000 1675.11 8.404 467.61 5943.4 0.5763 1.40084 +FS_21 Fan.Fl_O 1223.69 17.311 586.60 140.26 0.0000 1104.77 14.882 561.83 4515.2 0.4698 1.39925 +FS_13 Splitter.Fl_O2 1021.09 17.311 586.60 140.26 0.0000 921.86 14.925 562.29 3795.6 0.4652 1.39925 +FS_22 Splitter.Fl_O1 202.60 17.311 586.60 140.26 0.0000 182.92 14.643 559.23 719.5 0.4950 1.39925 +FS_23 Duct1.Fl_O 202.60 17.268 586.60 140.26 0.0000 183.37 14.606 559.23 721.3 0.4950 1.39925 +FS_24 LPC.Fl_O 202.60 42.971 786.22 188.46 0.0000 85.31 37.599 757.13 366.0 0.4419 1.39261 +FS_25 Duct2.Fl_O 202.60 42.863 786.22 188.46 0.0000 85.52 37.505 757.13 366.9 0.4419 1.39261 +FS_3 HPC.Fl_O 202.60 240.116 1335.42 326.11 0.0000 19.90 226.038 1314.22 119.9 0.2991 1.35974 +FS_36 Bld3.Fl_O 184.37 240.116 1335.42 326.11 0.0000 18.11 226.038 1314.22 109.1 0.2991 1.35974 +FS_4 Burner.Fl_O 188.28 226.909 2620.27 699.24 0.0212 27.41 225.446 2616.40 483.4 0.0999 1.29663 +FS_45 HPT.Fl_O 206.51 85.188 2053.52 531.25 0.0193 70.89 80.471 2025.81 439.1 0.2955 1.31272 +FS_48 Duct3.Fl_O 206.51 84.762 2053.52 531.25 0.0193 71.24 80.068 2025.81 441.4 0.2955 1.31272 +FS_5 LPT.Fl_O 206.51 17.466 1437.05 359.09 0.0193 289.24 15.994 1405.22 1477.4 0.3641 1.34045 +FS_7 Duct4.Fl_O 206.51 17.291 1437.05 359.09 0.0193 292.16 16.533 1420.76 2018.9 0.2593 1.34045 +FS_9 Core_Nozz.Fl_O 206.51 17.291 1437.05 359.09 0.0193 292.16 9.266 1223.76 862.9 1.0000 1.34045 +FS_15 BypBld.Fl_O 1021.09 17.311 586.60 140.26 0.0000 921.86 14.925 562.29 3795.6 0.4652 1.39925 +FS_17 Duct5.Fl_O 1021.09 17.181 586.60 140.26 0.0000 928.82 14.813 562.29 3824.3 0.4652 1.39925 +FS_19 Byp_Nozz.Fl_O 1021.09 17.181 586.60 140.26 0.0000 928.82 9.074 488.75 2706.4 1.0000 1.39925 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.644 0.8675 3944.235 1.1761 0.8764 -36484.5 24.72 17.46 +LPC 183.37 2.488 0.8683 3636.963 1.3403 0.8839 -13818.6 28.38 23.30 +HPC 85.52 5.602 0.8651 6324.866 1.6985 0.8921 -39457.4 20.21 20.26 +HPT 27.41 2.664 0.9137 152.126 1.2285 0.9041 39457.3 +LPT 71.24 4.853 0.9329 85.353 1.4290 0.9190 50303.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.448 0.8962 1.000 2.3716 0.5215 1.4369 0.9679 3943.9586 +LPC 196.69 1.456 0.9045 0.993 1.7667 0.9323 3.2631 0.9600 3662.6571 +HPC 203.32 22.274 0.8535 0.995 2.0450 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.916 0.9320 99.356 4.9155 1.4085 0.4249 0.9803 1.5311 +LPT 148.04 6.375 0.9317 105.229 6.3749 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5769.81 24138.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 982.50 236.64 71.761 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 982.50 236.64 71.761 +Duct1 0.0025 0.4950 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 982.50 236.64 71.761 +Duct2 0.0025 0.4419 365.99 +Duct3 0.0050 0.2955 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3641 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.0912 1335.42 326.11 240.116 +Duct5 0.0075 0.4652 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.1433 1335.42 326.11 240.116 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 586.60 140.26 17.311 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0398 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7787.1 26612.4 39457.3 +LP_Shaft 3867.8 68306.6 50303.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2620.27 0.9940 0.0550 3.90969 0.02121 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.072 0.9976 1.0000 0.9975 2706.36 1.000 1081.4 36434.3 +Core_Nozz 2.085 0.9999 1.0000 0.9999 862.88 1.000 1685.8 11660.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 191 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 15000.0 0.00 1192.11 21560.0 0.5756 12409.04 5.3109 634.66 20.746 2524.1 2460.5 1971.3 + core size:20.00 Q: 301.21 Maximum Thrust: 23956.4 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1192.11 10.581 498.77 119.18 0.0000 1623.70 8.293 465.18 5620.9 0.6000 1.40084 +FS_2 Inlet.Fl_O 1192.11 10.528 498.77 119.18 0.0000 1631.87 8.549 469.92 5943.4 0.5533 1.40084 +FS_21 Fan.Fl_O 1192.11 16.909 579.80 138.62 0.0000 1095.45 14.585 555.83 4515.2 0.4645 1.39936 +FS_13 Splitter.Fl_O2 1003.21 16.909 579.80 138.62 0.0000 921.87 14.578 555.77 3795.6 0.4652 1.39936 +FS_22 Splitter.Fl_O1 188.90 16.909 579.80 138.62 0.0000 173.58 14.616 556.18 719.5 0.4610 1.39936 +FS_23 Duct1.Fl_O 188.90 16.867 579.80 138.62 0.0000 174.02 14.580 556.18 721.3 0.4610 1.39936 +FS_24 LPC.Fl_O 188.90 39.286 761.72 182.51 0.0000 85.63 34.331 733.23 366.0 0.4438 1.39377 +FS_25 Duct2.Fl_O 188.90 39.188 761.72 182.51 0.0000 85.85 34.246 733.23 366.9 0.4438 1.39377 +FS_3 HPC.Fl_O 188.90 219.506 1296.78 316.12 0.0000 20.00 206.499 1275.87 119.9 0.3005 1.36209 +FS_36 Bld3.Fl_O 171.90 219.506 1296.78 316.12 0.0000 18.20 206.499 1275.87 109.1 0.3005 1.36209 +FS_4 Burner.Fl_O 175.34 207.433 2524.11 669.56 0.0201 27.40 206.095 2520.35 483.4 0.0998 1.29955 +FS_45 HPT.Fl_O 192.34 77.098 1971.33 507.10 0.0182 71.48 72.753 1944.01 439.1 0.2978 1.31632 +FS_48 Duct3.Fl_O 192.34 76.712 1971.33 507.10 0.0182 71.84 72.389 1944.01 441.4 0.2978 1.31632 +FS_5 LPT.Fl_O 192.34 15.927 1380.39 343.54 0.0182 289.52 14.583 1349.50 1477.4 0.3639 1.34445 +FS_7 Duct4.Fl_O 192.34 15.768 1380.39 343.54 0.0182 292.45 15.075 1364.58 2018.9 0.2592 1.34445 +FS_9 Core_Nozz.Fl_O 192.34 15.768 1380.39 343.54 0.0182 292.45 8.439 1173.53 862.9 1.0000 1.34445 +FS_15 BypBld.Fl_O 1003.21 16.909 579.80 138.62 0.0000 921.87 14.578 555.77 3795.6 0.4652 1.39936 +FS_17 Duct5.Fl_O 1003.21 16.782 579.80 138.62 0.0000 928.84 14.469 555.77 3824.3 0.4652 1.39936 +FS_19 Byp_Nozz.Fl_O 1003.21 16.782 579.80 138.62 0.0000 928.84 8.863 483.06 2706.4 1.0000 1.39936 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1631.87 1.606 0.8929 3738.587 1.1625 0.8998 -32786.7 28.30 17.76 +LPC 174.02 2.329 0.8659 3467.499 1.3138 0.8806 -11730.2 28.80 22.07 +HPC 85.85 5.601 0.8642 6332.677 1.7024 0.8914 -35708.3 20.68 20.72 +HPT 27.40 2.691 0.9142 152.752 1.2331 0.9043 35708.9 +LPT 71.84 4.816 0.9283 82.572 1.4281 0.9137 44513.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3128.65 1.422 0.9224 0.948 2.1725 0.5215 1.4369 0.9679 3943.9586 +LPC 186.65 1.407 0.9019 0.947 1.7493 0.9323 3.2631 0.9600 3662.6571 +HPC 204.08 22.271 0.8526 0.996 2.0733 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.979 0.9325 99.765 4.9788 1.4085 0.4249 0.9803 1.5311 +LPT 149.26 6.324 0.9271 101.801 6.3237 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5620.90 23515.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 952.77 229.28 65.604 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 952.77 229.28 65.604 +Duct1 0.0025 0.4610 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 952.77 229.28 65.604 +Duct2 0.0025 0.4438 365.99 +Duct3 0.0050 0.2978 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3639 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.6113 1296.78 316.12 219.506 +Duct5 0.0075 0.4652 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.3893 1296.78 316.12 219.506 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 579.80 138.62 16.909 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3109 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7674.3 24438.2 35708.9 +LP_Shaft 3666.2 63769.2 44513.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2524.11 0.9940 0.0550 3.44695 0.02005 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.024 0.9976 1.0000 0.9975 2706.36 1.000 1075.1 35066.2 +Core_Nozz 1.901 0.9999 1.0000 0.9999 862.88 1.000 1653.3 10009.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 192 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 15000.0 0.00 1156.10 19165.2 0.5702 10928.56 5.5223 634.66 19.074 2427.4 2366.9 1891.5 + core size:20.15 Q: 301.21 Maximum Thrust: 23956.4 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1156.10 10.581 498.77 119.18 0.0000 1574.65 8.293 465.18 5451.1 0.6000 1.40084 +FS_2 Inlet.Fl_O 1156.10 10.528 498.77 119.18 0.0000 1582.57 8.703 472.32 5943.4 0.5284 1.40084 +FS_21 Fan.Fl_O 1156.10 16.408 573.51 137.11 0.0000 1088.80 14.186 550.16 4515.2 0.4608 1.39947 +FS_13 Splitter.Fl_O2 978.84 16.408 573.51 137.11 0.0000 921.87 14.147 549.73 3795.6 0.4652 1.39947 +FS_22 Splitter.Fl_O1 177.25 16.408 573.51 137.11 0.0000 166.94 14.381 552.32 719.5 0.4381 1.39947 +FS_23 Duct1.Fl_O 177.25 16.367 573.51 137.11 0.0000 167.35 14.345 552.32 721.3 0.4381 1.39947 +FS_24 LPC.Fl_O 177.25 36.891 746.36 178.79 0.0000 84.70 32.357 719.16 366.0 0.4376 1.39441 +FS_25 Duct2.Fl_O 177.25 36.799 746.36 178.79 0.0000 84.92 32.276 719.16 366.9 0.4376 1.39441 +FS_3 HPC.Fl_O 177.25 201.811 1263.85 307.65 0.0000 20.15 189.658 1243.04 119.9 0.3029 1.36414 +FS_36 Bld3.Fl_O 161.30 201.811 1263.85 307.65 0.0000 18.34 189.658 1243.04 109.1 0.3029 1.36414 +FS_4 Burner.Fl_O 164.34 190.712 2427.38 639.92 0.0188 27.40 189.483 2423.73 483.4 0.0996 1.30256 +FS_45 HPT.Fl_O 180.29 70.534 1891.49 483.83 0.0171 71.73 66.529 1864.83 439.1 0.2985 1.32013 +FS_48 Duct3.Fl_O 180.29 70.181 1891.49 483.83 0.0171 72.09 66.196 1864.83 441.4 0.2985 1.32013 +FS_5 LPT.Fl_O 180.29 14.648 1322.91 327.89 0.0171 288.87 13.419 1293.21 1477.4 0.3624 1.34867 +FS_7 Duct4.Fl_O 180.29 14.502 1322.91 327.89 0.0171 291.79 13.868 1307.70 2018.9 0.2581 1.34867 +FS_9 Core_Nozz.Fl_O 180.29 14.502 1322.91 327.89 0.0171 291.79 8.293 1143.05 862.9 0.9404 1.34867 +FS_15 BypBld.Fl_O 978.84 16.408 573.51 137.11 0.0000 921.87 14.147 549.73 3795.6 0.4652 1.39947 +FS_17 Duct5.Fl_O 978.84 16.285 573.51 137.11 0.0000 928.83 14.041 549.73 3824.3 0.4652 1.39947 +FS_19 Byp_Nozz.Fl_O 978.84 16.285 573.51 137.11 0.0000 928.83 8.601 477.80 2706.4 1.0000 1.39947 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1582.57 1.559 0.9027 3606.813 1.1499 0.9087 -29325.1 31.90 18.37 +LPC 167.35 2.254 0.8628 3363.575 1.3014 0.8774 -10451.9 27.91 20.32 +HPC 84.92 5.484 0.8650 6309.059 1.6933 0.8917 -32316.0 22.30 22.39 +HPT 27.40 2.704 0.9145 153.612 1.2366 0.9047 32315.9 +LPT 72.09 4.791 0.9264 81.325 1.4298 0.9113 39777.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3034.39 1.389 0.9326 0.915 2.0935 0.5215 1.4369 0.9679 3943.9586 +LPC 179.51 1.384 0.8988 0.918 1.7118 0.9323 3.2631 0.9600 3662.6571 +HPC 201.87 21.729 0.8533 0.992 2.0970 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.010 0.9329 100.327 5.0102 1.4085 0.4249 0.9803 1.5311 +LPT 149.81 6.289 0.9252 100.264 6.2885 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5451.09 22804.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 930.95 223.89 60.973 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 930.95 223.89 60.973 +Duct1 0.0025 0.4381 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 930.95 223.89 60.973 +Duct2 0.0025 0.4376 365.99 +Duct3 0.0050 0.2985 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3624 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.2038 1263.85 307.65 201.811 +Duct5 0.0075 0.4652 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.7489 1263.85 307.65 201.811 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 573.51 137.11 16.408 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5223 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7568.2 22426.2 32315.9 +LP_Shaft 3536.9 59066.6 39777.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2427.38 0.9940 0.0550 3.03571 0.01882 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.964 0.9976 1.0000 0.9975 2706.36 1.000 1069.3 33363.3 +Core_Nozz 1.749 0.9999 1.0000 0.9999 862.88 0.940 1536.0 8606.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 193 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 15000.0 0.00 1073.47 14374.2 0.5728 8233.89 6.0113 634.66 15.768 2231.7 2177.4 1731.4 + core size:20.47 Q: 301.21 Maximum Thrust: 23956.4 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1073.47 10.581 498.77 119.18 0.0000 1462.11 8.293 465.18 5061.5 0.6000 1.40084 +FS_2 Inlet.Fl_O 1073.47 10.528 498.77 119.18 0.0000 1469.47 9.013 477.07 5943.4 0.4762 1.40084 +FS_21 Fan.Fl_O 1073.47 15.259 560.10 133.89 0.0000 1074.32 13.258 538.04 4515.2 0.4527 1.39971 +FS_13 Splitter.Fl_O2 920.36 15.259 560.10 133.89 0.0000 921.09 13.161 536.92 3795.6 0.4646 1.39971 +FS_22 Splitter.Fl_O1 153.11 15.259 560.10 133.89 0.0000 153.23 13.714 543.27 719.5 0.3936 1.39971 +FS_23 Duct1.Fl_O 153.11 15.221 560.10 133.89 0.0000 153.61 13.679 543.27 721.3 0.3936 1.39971 +FS_24 LPC.Fl_O 153.11 32.074 714.99 171.19 0.0000 82.36 28.383 690.62 366.0 0.4221 1.39551 +FS_25 Duct2.Fl_O 153.11 31.994 714.99 171.19 0.0000 82.57 28.312 690.62 366.9 0.4221 1.39551 +FS_3 HPC.Fl_O 153.11 166.832 1195.24 290.10 0.0000 20.47 156.435 1174.68 119.9 0.3078 1.36844 +FS_36 Bld3.Fl_O 139.33 166.832 1195.24 290.10 0.0000 18.63 156.435 1174.68 109.1 0.3078 1.36844 +FS_4 Burner.Fl_O 141.61 157.656 2231.65 580.90 0.0164 27.38 156.641 2228.25 483.4 0.0993 1.30933 +FS_45 HPT.Fl_O 155.39 57.903 1731.41 437.95 0.0149 72.06 54.585 1706.30 439.1 0.2990 1.32845 +FS_48 Duct3.Fl_O 155.39 57.614 1731.41 437.95 0.0149 72.42 54.312 1706.30 441.4 0.2990 1.32845 +FS_5 LPT.Fl_O 155.39 12.562 1217.59 299.61 0.0149 278.53 11.590 1192.04 1477.4 0.3462 1.35673 +FS_7 Duct4.Fl_O 155.39 12.437 1217.59 299.61 0.0149 281.34 11.933 1204.42 2018.9 0.2474 1.35673 +FS_9 Core_Nozz.Fl_O 155.39 12.437 1217.59 299.61 0.0149 281.34 8.293 1093.63 862.8 0.7916 1.35673 +FS_15 BypBld.Fl_O 920.36 15.259 560.10 133.89 0.0000 921.09 13.161 536.92 3795.6 0.4646 1.39971 +FS_17 Duct5.Fl_O 920.36 15.145 560.10 133.89 0.0000 928.05 13.062 536.92 3824.3 0.4646 1.39971 +FS_19 Byp_Nozz.Fl_O 920.36 15.145 560.10 133.89 0.0000 928.05 8.293 471.46 2706.3 0.9686 1.39971 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1469.47 1.449 0.9107 3339.461 1.1230 0.9153 -22336.8 40.28 19.86 +LPC 153.61 2.107 0.8550 3151.330 1.2766 0.8693 -8080.4 25.76 16.84 +HPC 82.57 5.214 0.8657 6259.018 1.6717 0.8918 -25758.5 25.97 26.11 +HPT 27.38 2.723 0.9149 155.560 1.2435 0.9047 25758.9 +LPT 72.42 4.586 0.9222 78.701 1.4220 0.9064 30414.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2817.28 1.313 0.9409 0.847 2.0400 0.5215 1.4369 0.9679 3943.9586 +LPC 164.77 1.339 0.8906 0.860 1.6339 0.9323 3.2631 0.9600 3662.6571 +HPC 196.29 20.483 0.8541 0.985 2.1337 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.055 0.9332 101.599 5.0547 1.4085 0.4249 0.9803 1.5311 +LPT 150.48 6.003 0.9210 97.028 6.0027 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5061.49 21175.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 885.90 212.81 51.748 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 885.90 212.81 51.748 +Duct1 0.0025 0.3936 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 885.90 212.81 51.748 +Duct2 0.0025 0.4221 365.99 +Duct3 0.0050 0.2990 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3462 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.3587 1195.24 290.10 166.832 +Duct5 0.0075 0.4646 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.4208 1195.24 290.10 166.832 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 560.10 133.89 15.259 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.0113 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7348.7 18409.9 25758.9 +LP_Shaft 3274.8 48779.2 30414.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2231.65 0.9940 0.0550 2.28719 0.01642 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.826 0.9975 1.0000 0.9975 2706.36 0.969 1028.9 29431.1 +Core_Nozz 1.500 0.9999 1.0000 0.9999 862.88 0.792 1266.8 6118.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 194 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 15000.0 0.00 972.84 9582.6 0.5988 5737.94 6.7009 634.66 12.324 2010.0 1962.6 1550.4 + core size:20.85 Q: 301.21 Maximum Thrust: 23956.4 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 972.84 10.581 498.77 119.18 0.0000 1325.04 8.293 465.18 4587.0 0.6000 1.40084 +FS_2 Inlet.Fl_O 972.84 10.528 498.77 119.18 0.0000 1331.71 9.329 481.81 5943.4 0.4190 1.40084 +FS_21 Fan.Fl_O 972.84 13.983 545.08 130.29 0.0000 1048.13 12.254 524.89 4515.2 0.4384 1.40000 +FS_13 Splitter.Fl_O2 846.51 13.983 545.08 130.29 0.0000 912.03 12.105 523.07 3795.6 0.4585 1.40000 +FS_22 Splitter.Fl_O1 126.33 13.983 545.08 130.29 0.0000 136.11 12.896 532.62 719.5 0.3419 1.40000 +FS_23 Duct1.Fl_O 126.33 13.948 545.08 130.29 0.0000 136.45 12.864 532.62 721.3 0.3419 1.40000 +FS_24 LPC.Fl_O 126.33 26.512 674.57 161.43 0.0000 79.86 23.672 653.18 366.0 0.4059 1.39691 +FS_25 Duct2.Fl_O 126.33 26.446 674.57 161.43 0.0000 80.06 23.613 653.18 366.9 0.4059 1.39691 +FS_3 HPC.Fl_O 126.33 130.392 1112.40 269.12 0.0000 20.85 121.942 1092.28 119.9 0.3136 1.37366 +FS_36 Bld3.Fl_O 114.96 130.392 1112.40 269.12 0.0000 18.97 121.942 1092.28 109.1 0.3136 1.37366 +FS_4 Burner.Fl_O 116.55 123.221 2010.00 515.63 0.0139 27.36 122.429 2006.87 483.4 0.0990 1.31792 +FS_45 HPT.Fl_O 127.92 44.792 1550.36 387.37 0.0126 72.56 42.187 1527.00 439.1 0.3001 1.33880 +FS_48 Duct3.Fl_O 127.92 44.568 1550.36 387.37 0.0126 72.93 41.976 1527.00 441.4 0.3001 1.33880 +FS_5 LPT.Fl_O 127.92 10.915 1113.55 272.17 0.0126 252.36 10.235 1094.52 1477.4 0.3083 1.36493 +FS_7 Duct4.Fl_O 127.92 10.806 1113.55 272.17 0.0126 254.90 10.450 1103.62 2018.9 0.2219 1.36493 +FS_9 Core_Nozz.Fl_O 127.92 10.806 1113.55 272.17 0.0126 254.90 8.293 1037.01 862.9 0.6333 1.36493 +FS_15 BypBld.Fl_O 846.51 13.983 545.08 130.29 0.0000 912.03 12.105 523.07 3795.6 0.4585 1.40000 +FS_17 Duct5.Fl_O 846.51 13.878 545.08 130.29 0.0000 918.92 12.015 523.07 3824.3 0.4585 1.40000 +FS_19 Byp_Nozz.Fl_O 846.51 13.878 545.08 130.29 0.0000 918.92 8.293 470.42 2706.4 0.8899 1.40000 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1331.71 1.328 0.9108 2983.230 1.0929 0.9144 -15282.7 47.53 21.18 +LPC 136.45 1.901 0.8459 2853.679 1.2376 0.8592 -5565.7 24.63 13.76 +HPC 80.06 4.931 0.8648 6214.635 1.6491 0.8907 -19248.5 30.25 30.47 +HPT 27.36 2.751 0.9154 158.083 1.2527 0.9051 19248.6 +LPT 72.93 4.083 0.9190 74.297 1.3923 0.9039 20848.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2553.38 1.228 0.9410 0.756 2.0664 0.5215 1.4369 0.9679 3943.9586 +LPC 146.36 1.276 0.8811 0.779 1.5801 0.9323 3.2631 0.9600 3662.6571 +HPC 190.33 19.170 0.8532 0.978 2.1688 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.121 0.9337 103.247 5.1211 1.4085 0.4249 0.9803 1.5311 +LPT 151.54 5.301 0.9179 91.599 5.3007 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4587.00 19189.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 829.95 199.12 41.674 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 829.95 199.12 41.674 +Duct1 0.0025 0.3419 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 829.95 199.12 41.674 +Duct2 0.0025 0.4059 365.99 +Duct3 0.0050 0.3001 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3083 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.4215 1112.40 269.12 130.392 +Duct5 0.0075 0.4585 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.9480 1112.40 269.12 130.392 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 545.08 130.29 13.983 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.7009 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7087.3 14264.3 19248.6 +LP_Shaft 2925.4 37429.9 20848.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2010.00 0.9940 0.0550 1.59387 0.01386 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.673 0.9975 1.0000 0.9975 2706.36 0.890 944.2 24841.5 +Core_Nozz 1.303 0.9999 1.0000 0.9999 862.88 0.633 988.7 3931.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 195 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 15000.0 0.00 843.73 4791.2 0.7078 3391.05 7.7745 634.66 8.667 1723.0 1684.5 1318.4 + core size:21.42 Q: 301.21 Maximum Thrust: 23956.4 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 843.73 10.581 498.77 119.18 0.0000 1149.20 8.293 465.18 3978.3 0.6000 1.40084 +FS_2 Inlet.Fl_O 843.73 10.528 498.77 119.18 0.0000 1154.98 9.659 486.63 5943.4 0.3527 1.40084 +FS_21 Fan.Fl_O 843.73 12.556 527.56 126.08 0.0000 995.98 11.177 510.30 4515.2 0.4109 1.40035 +FS_13 Splitter.Fl_O2 747.58 12.556 527.56 126.08 0.0000 882.47 10.997 507.93 3795.6 0.4392 1.40035 +FS_22 Splitter.Fl_O1 96.16 12.556 527.56 126.08 0.0000 113.51 11.896 519.48 719.5 0.2786 1.40035 +FS_23 Duct1.Fl_O 96.16 12.524 527.56 126.08 0.0000 113.79 11.867 519.48 721.3 0.2786 1.40035 +FS_24 LPC.Fl_O 96.16 20.312 621.08 148.54 0.0000 76.13 18.360 603.46 366.0 0.3827 1.39864 +FS_25 Duct2.Fl_O 96.16 20.261 621.08 148.54 0.0000 76.32 18.315 603.46 366.9 0.3827 1.39864 +FS_3 HPC.Fl_O 96.16 91.705 1001.95 241.47 0.0000 21.42 85.409 982.48 119.9 0.3224 1.38059 +FS_36 Bld3.Fl_O 87.50 91.705 1001.95 241.47 0.0000 19.49 85.409 982.48 109.1 0.3224 1.38059 +FS_4 Burner.Fl_O 88.45 86.662 1723.03 433.75 0.0108 27.34 86.106 1720.27 483.4 0.0983 1.33170 +FS_45 HPT.Fl_O 97.10 31.109 1318.41 324.58 0.0098 73.13 29.271 1297.56 439.1 0.3010 1.35386 +FS_48 Duct3.Fl_O 97.10 30.953 1318.41 324.58 0.0098 73.50 29.124 1297.56 441.4 0.3010 1.35386 +FS_5 LPT.Fl_O 97.10 9.670 998.45 242.38 0.0098 204.73 9.284 987.41 1477.4 0.2443 1.37418 +FS_7 Duct4.Fl_O 97.10 9.574 998.45 242.38 0.0098 206.80 9.369 992.59 2018.9 0.1776 1.37418 +FS_9 Core_Nozz.Fl_O 97.10 9.574 998.45 242.38 0.0098 206.80 8.293 960.06 863.0 0.4613 1.37418 +FS_15 BypBld.Fl_O 747.58 12.556 527.56 126.08 0.0000 882.47 10.997 507.93 3795.6 0.4392 1.40035 +FS_17 Duct5.Fl_O 747.58 12.462 527.56 126.08 0.0000 889.14 10.914 507.93 3824.3 0.4392 1.40035 +FS_19 Byp_Nozz.Fl_O 747.58 12.462 527.56 126.08 0.0000 889.14 8.293 469.53 2706.4 0.7851 1.40035 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1154.98 1.193 0.8954 2478.782 1.0577 0.8981 -8237.6 56.89 22.13 +LPC 113.79 1.622 0.8352 2410.193 1.1773 0.8459 -3055.7 27.36 10.90 +HPC 76.32 4.526 0.8629 6145.902 1.6132 0.8881 -12642.6 36.97 37.45 +HPT 27.34 2.786 0.9163 162.020 1.2660 0.9055 12642.7 +LPT 73.50 3.201 0.9087 66.945 1.3205 0.8946 11293.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2214.52 1.134 0.9251 0.629 2.2127 0.5215 1.4369 0.9679 3943.9586 +LPC 122.06 1.191 0.8699 0.658 1.5842 0.9323 3.2631 0.9600 3662.6571 +HPC 181.45 17.301 0.8513 0.967 2.2339 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.203 0.9346 105.818 5.2030 1.4085 0.4249 0.9803 1.5311 +LPT 152.73 4.070 0.9075 82.534 4.0701 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3978.27 16643.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 755.77 181.07 30.727 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 755.77 181.07 30.727 +Duct1 0.0025 0.2786 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 755.77 181.07 30.727 +Duct2 0.0025 0.3827 365.99 +Duct3 0.0050 0.3010 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2443 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.3655 1001.95 241.47 91.705 +Duct5 0.0075 0.4392 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.2886 1001.95 241.47 91.705 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 527.56 126.08 12.556 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.7745 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6725.4 9873.2 12642.7 +LP_Shaft 2430.8 24401.4 11293.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1723.03 0.9940 0.0550 0.94196 0.01076 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.503 0.9975 1.0000 0.9975 2706.36 0.785 832.3 19337.8 +Core_Nozz 1.154 0.9999 1.0000 0.9999 862.88 0.461 694.8 2096.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:49 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 196 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 12/ 22/ 1/10 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 15000.0 0.00 711.56 1197.8 1.3648 1634.79 9.3886 634.66 5.525 1384.2 1356.6 1050.4 + core size:22.37 Q: 301.21 Maximum Thrust: 23956.4 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 711.56 10.581 498.77 119.18 0.0000 969.17 8.293 465.18 3355.1 0.6000 1.40084 +FS_2 Inlet.Fl_O 711.56 10.528 498.77 119.18 0.0000 974.05 9.928 490.47 5943.4 0.2906 1.40084 +FS_21 Fan.Fl_O 711.56 11.342 511.92 122.33 0.0000 915.97 10.312 498.17 4515.2 0.3711 1.40063 +FS_13 Splitter.Fl_O2 643.06 11.342 511.92 122.33 0.0000 827.80 10.129 495.61 3795.6 0.4051 1.40063 +FS_22 Splitter.Fl_O1 68.49 11.342 511.92 122.33 0.0000 88.17 10.991 507.34 719.5 0.2123 1.40063 +FS_23 Duct1.Fl_O 68.49 11.313 511.92 122.33 0.0000 88.39 10.964 507.34 721.3 0.2123 1.40063 +FS_24 LPC.Fl_O 68.49 15.125 565.83 135.27 0.0000 69.51 13.939 552.78 366.0 0.3436 1.39961 +FS_25 Duct2.Fl_O 68.49 15.087 565.83 135.27 0.0000 69.69 13.904 552.78 366.9 0.3436 1.39961 +FS_3 HPC.Fl_O 68.49 58.458 875.75 210.32 0.0000 22.37 54.044 856.72 119.9 0.3380 1.38824 +FS_36 Bld3.Fl_O 62.33 58.458 875.75 210.32 0.0000 20.36 54.044 856.72 109.1 0.3380 1.38824 +FS_4 Burner.Fl_O 62.78 55.242 1384.24 341.13 0.0073 27.29 54.889 1381.94 483.4 0.0974 1.35162 +FS_45 HPT.Fl_O 68.95 19.615 1050.39 254.87 0.0066 73.51 18.444 1032.95 439.1 0.3005 1.37298 +FS_48 Duct3.Fl_O 68.95 19.517 1050.39 254.87 0.0066 73.88 18.352 1032.95 441.4 0.3005 1.37298 +FS_5 LPT.Fl_O 68.95 8.940 868.58 209.50 0.0066 146.67 8.761 863.71 1477.4 0.1713 1.38429 +FS_7 Duct4.Fl_O 68.95 8.851 868.58 209.50 0.0066 148.15 8.755 865.96 2018.9 0.1256 1.38429 +FS_9 Core_Nozz.Fl_O 68.95 8.851 868.58 209.50 0.0066 148.15 8.293 853.04 862.9 0.3079 1.38429 +FS_15 BypBld.Fl_O 643.06 11.342 511.92 122.33 0.0000 827.80 10.129 495.61 3795.6 0.4051 1.40063 +FS_17 Duct5.Fl_O 643.06 11.257 511.92 122.33 0.0000 834.06 10.053 495.61 3824.3 0.4051 1.40063 +FS_19 Byp_Nozz.Fl_O 643.06 11.257 511.92 122.33 0.0000 834.06 8.293 469.06 2706.4 0.6750 1.40063 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 974.05 1.077 0.8169 1867.968 1.0264 0.8189 -3172.5 83.95 21.56 +LPC 88.39 1.337 0.8218 1843.818 1.1053 0.8290 -1253.2 36.18 9.27 +HPC 69.69 3.875 0.8541 6024.012 1.5477 0.8785 -7273.5 49.42 50.41 +HPT 27.29 2.816 0.9179 169.113 1.2830 0.9068 7273.5 +LPT 73.88 2.183 0.8966 56.519 1.2093 0.8860 4425.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1867.61 1.054 0.8439 0.474 2.5523 0.5215 1.4369 0.9679 3943.9586 +LPC 94.81 1.103 0.8561 0.503 1.6879 0.9323 3.2631 0.9600 3662.6571 +HPC 165.67 14.289 0.8426 0.948 2.3800 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.275 0.9363 110.451 5.2749 1.4085 0.4249 0.9803 1.5311 +LPT 153.52 2.650 0.8954 69.681 2.6503 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3355.06 14036.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 675.02 161.53 21.441 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 675.02 161.53 21.441 +Duct1 0.0025 0.2123 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 675.02 161.53 21.441 +Duct2 0.0025 0.3436 365.99 +Duct3 0.0050 0.3005 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1713 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.3973 875.75 210.32 58.458 +Duct5 0.0075 0.4051 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.7672 875.75 210.32 58.458 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 511.92 122.33 11.342 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.3886 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6291.9 6071.5 7273.5 +LP_Shaft 1831.8 12689.4 4425.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1384.24 0.9940 0.0550 0.45411 0.00729 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.357 0.9975 1.0000 0.9975 2706.36 0.675 715.2 14294.4 +Core_Nozz 1.067 0.9999 1.0000 0.9999 862.88 0.308 438.4 939.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 197 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 4/ 14/ 1/ 2 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 15000.0 0.00 1314.95 24668.9 0.6309 15563.71 5.0399 740.43 22.687 2679.0 2611.3 2101.8 + core size:19.88 Q: 409.99 Maximum Thrust: 24668.9 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1314.95 11.507 510.89 122.09 0.0000 1666.72 8.293 465.18 5314.4 0.7000 1.40065 +FS_2 Inlet.Fl_O 1314.95 11.449 510.89 122.09 0.0000 1675.11 9.140 478.99 5943.4 0.5764 1.40065 +FS_21 Fan.Fl_O 1314.95 18.827 600.83 143.67 0.0000 1104.72 16.185 575.46 4515.2 0.4698 1.39903 +FS_13 Splitter.Fl_O2 1097.24 18.827 600.83 143.67 0.0000 921.82 16.232 575.94 3795.6 0.4652 1.39903 +FS_22 Splitter.Fl_O1 217.71 18.827 600.83 143.67 0.0000 182.90 15.925 572.81 719.5 0.4950 1.39903 +FS_23 Duct1.Fl_O 217.71 18.780 600.83 143.67 0.0000 183.36 15.885 572.81 721.3 0.4950 1.39903 +FS_24 LPC.Fl_O 217.71 46.744 805.09 193.05 0.0000 85.27 40.906 775.38 366.0 0.4418 1.39170 +FS_25 Duct2.Fl_O 217.71 46.627 805.09 193.05 0.0000 85.49 40.803 775.38 366.9 0.4418 1.39170 +FS_3 HPC.Fl_O 217.71 261.062 1365.25 333.85 0.0000 19.88 245.778 1343.69 119.9 0.2991 1.35795 +FS_36 Bld3.Fl_O 198.11 261.062 1365.25 333.85 0.0000 18.09 245.778 1343.69 109.1 0.2991 1.35795 +FS_4 Burner.Fl_O 202.44 246.703 2679.04 717.43 0.0218 27.41 245.113 2675.10 483.4 0.1000 1.29503 +FS_45 HPT.Fl_O 222.03 92.669 2101.84 545.53 0.0199 70.88 87.538 2073.61 439.1 0.2957 1.31076 +FS_48 Duct3.Fl_O 222.03 92.206 2101.84 545.53 0.0199 71.24 87.100 2073.61 441.4 0.2957 1.31076 +FS_5 LPT.Fl_O 222.03 19.030 1473.95 369.27 0.0199 289.05 17.429 1441.52 1477.4 0.3642 1.33802 +FS_7 Duct4.Fl_O 222.03 18.839 1473.95 369.27 0.0199 291.97 18.015 1457.35 2018.9 0.2593 1.33802 +FS_9 Core_Nozz.Fl_O 222.03 18.839 1473.95 369.27 0.0199 291.97 10.104 1256.51 862.9 1.0000 1.33802 +FS_15 BypBld.Fl_O 1097.24 18.827 600.83 143.67 0.0000 921.82 16.232 575.94 3795.6 0.4652 1.39903 +FS_17 Duct5.Fl_O 1097.24 18.686 600.83 143.67 0.0000 928.79 16.111 575.94 3824.3 0.4652 1.39903 +FS_19 Byp_Nozz.Fl_O 1097.24 18.686 600.83 143.67 0.0000 928.79 9.870 500.65 2706.4 1.0000 1.39903 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.644 0.8675 3944.235 1.1760 0.8764 -40159.5 24.72 17.46 +LPC 183.36 2.489 0.8683 3637.070 1.3400 0.8839 -15210.6 28.36 23.28 +HPC 85.49 5.599 0.8652 6323.988 1.6958 0.8921 -43369.4 20.23 20.29 +HPT 27.41 2.662 0.9137 152.222 1.2272 0.9043 43369.2 +LPT 71.24 4.845 0.9331 85.385 1.4260 0.9193 55370.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.448 0.8962 1.000 2.3715 0.5215 1.4369 0.9679 3943.9586 +LPC 196.68 1.456 0.9045 0.993 1.7661 0.9323 3.2631 0.9600 3662.6571 +HPC 203.24 22.260 0.8535 0.995 2.0447 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.912 0.9321 99.419 4.9122 1.4085 0.4249 0.9803 1.5311 +LPT 148.03 6.364 0.9319 105.269 6.3641 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5314.36 30261.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 1005.42 242.33 78.042 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 1005.42 242.33 78.042 +Duct1 0.0025 0.4950 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 1005.42 242.33 78.042 +Duct2 0.0025 0.4418 365.99 +Duct3 0.0050 0.2957 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3642 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.6198 1365.25 333.85 261.062 +Duct5 0.0075 0.4652 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.9740 1365.25 333.85 261.062 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 600.83 143.67 18.827 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0399 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7878.9 28910.0 43369.2 +LP_Shaft 3914.5 74289.6 55370.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2679.04 0.9940 0.0550 4.32325 0.02182 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.253 0.9972 1.0000 0.9975 2706.36 1.000 1094.4 41590.0 +Core_Nozz 2.272 0.9993 1.0000 0.9999 862.88 1.000 1706.7 13340.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 198 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 15000.0 0.00 1281.60 22201.5 0.6191 13744.64 5.3064 740.43 20.770 2582.0 2517.1 2018.6 + core size:19.98 Q: 409.99 Maximum Thrust: 24668.9 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1281.60 11.507 510.89 122.09 0.0000 1624.45 8.293 465.18 5179.6 0.7000 1.40065 +FS_2 Inlet.Fl_O 1281.60 11.449 510.89 122.09 0.0000 1632.62 9.295 481.31 5943.4 0.5537 1.40065 +FS_21 Fan.Fl_O 1281.60 18.397 593.96 142.02 0.0000 1095.57 15.867 569.41 4515.2 0.4646 1.39914 +FS_13 Splitter.Fl_O2 1078.37 18.397 593.96 142.02 0.0000 921.85 15.861 569.35 3795.6 0.4652 1.39914 +FS_22 Splitter.Fl_O1 203.22 18.397 593.96 142.02 0.0000 173.72 15.897 569.72 719.5 0.4616 1.39914 +FS_23 Duct1.Fl_O 203.22 18.351 593.96 142.02 0.0000 174.16 15.858 569.72 721.3 0.4616 1.39914 +FS_24 LPC.Fl_O 203.22 42.767 780.23 187.01 0.0000 85.65 37.370 751.06 366.0 0.4441 1.39291 +FS_25 Duct2.Fl_O 203.22 42.660 780.23 187.01 0.0000 85.86 37.276 751.06 366.9 0.4441 1.39291 +FS_3 HPC.Fl_O 203.22 239.001 1326.50 323.80 0.0000 19.98 224.858 1305.22 119.9 0.3005 1.36028 +FS_36 Bld3.Fl_O 184.93 239.001 1326.50 323.80 0.0000 18.19 224.858 1305.22 109.1 0.3005 1.36028 +FS_4 Burner.Fl_O 188.75 225.856 2582.02 687.32 0.0206 27.40 224.400 2578.19 483.4 0.0999 1.29785 +FS_45 HPT.Fl_O 207.04 83.996 2018.62 520.93 0.0188 71.46 79.264 1990.79 439.1 0.2980 1.31426 +FS_48 Duct3.Fl_O 207.04 83.576 2018.62 520.93 0.0188 71.82 78.868 1990.79 441.4 0.2980 1.31426 +FS_5 LPT.Fl_O 207.04 17.377 1416.47 353.38 0.0188 289.36 15.912 1384.98 1477.4 0.3641 1.34197 +FS_7 Duct4.Fl_O 207.04 17.203 1416.47 353.38 0.0188 292.28 16.448 1400.35 2018.9 0.2592 1.34197 +FS_9 Core_Nozz.Fl_O 207.04 17.203 1416.47 353.38 0.0188 292.28 9.215 1205.46 862.9 1.0000 1.34197 +FS_15 BypBld.Fl_O 1078.37 18.397 593.96 142.02 0.0000 921.85 15.861 569.35 3795.6 0.4652 1.39914 +FS_17 Duct5.Fl_O 1078.37 18.259 593.96 142.02 0.0000 928.81 15.742 569.35 3824.3 0.4652 1.39914 +FS_19 Byp_Nozz.Fl_O 1078.37 18.259 593.96 142.02 0.0000 928.81 9.644 494.90 2706.4 1.0000 1.39914 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1632.62 1.607 0.8926 3741.038 1.1626 0.8996 -36148.5 28.25 17.75 +LPC 174.16 2.331 0.8660 3469.582 1.3136 0.8807 -12933.7 28.83 22.12 +HPC 85.86 5.603 0.8642 6333.188 1.7001 0.8914 -39332.0 20.68 20.72 +HPT 27.40 2.689 0.9142 152.865 1.2319 0.9045 39332.3 +LPT 71.82 4.810 0.9285 82.639 1.4251 0.9139 49079.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3130.14 1.422 0.9222 0.949 2.1746 0.5215 1.4369 0.9679 3943.9586 +LPC 186.81 1.408 0.9020 0.947 1.7504 0.9323 3.2631 0.9600 3662.6571 +HPC 204.12 22.276 0.8525 0.996 2.0740 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.975 0.9326 99.839 4.9750 1.4085 0.4249 0.9803 1.5311 +LPT 149.23 6.314 0.9273 101.883 6.3142 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5179.57 29493.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 975.42 234.88 71.424 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 975.42 234.88 71.424 +Duct1 0.0025 0.4616 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 975.42 234.88 71.424 +Duct2 0.0025 0.4441 365.99 +Duct3 0.0050 0.2980 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3641 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 7.1127 1326.50 323.80 239.001 +Duct5 0.0075 0.4652 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 11.1772 1326.50 323.80 239.001 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 593.96 142.02 18.397 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3064 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7767.6 26594.8 39332.3 +LP_Shaft 3712.9 69426.1 49079.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2582.02 0.9940 0.0550 3.81796 0.02065 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.202 0.9974 1.0000 0.9975 2706.36 1.000 1088.2 40127.4 +Core_Nozz 2.074 0.9999 1.0000 0.9999 862.88 1.000 1674.1 11567.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 199 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 15000.0 0.00 1243.95 19735.2 0.6141 12118.66 5.5164 740.43 19.117 2483.7 2421.9 1937.6 + core size:20.14 Q: 409.99 Maximum Thrust: 24668.9 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1243.95 11.507 510.89 122.09 0.0000 1576.73 8.293 465.18 5027.4 0.7000 1.40065 +FS_2 Inlet.Fl_O 1243.95 11.449 510.89 122.09 0.0000 1584.67 9.458 483.70 5943.4 0.5295 1.40065 +FS_21 Fan.Fl_O 1243.95 17.870 587.70 140.52 0.0000 1088.97 15.448 563.77 4515.2 0.4609 1.39923 +FS_13 Splitter.Fl_O2 1053.06 17.870 587.70 140.52 0.0000 921.85 15.407 563.34 3795.6 0.4652 1.39923 +FS_22 Splitter.Fl_O1 190.90 17.870 587.70 140.52 0.0000 167.11 15.657 565.93 719.5 0.4388 1.39923 +FS_23 Duct1.Fl_O 190.90 17.825 587.70 140.52 0.0000 167.53 15.617 565.93 721.3 0.4388 1.39923 +FS_24 LPC.Fl_O 190.90 40.251 765.08 183.33 0.0000 84.65 35.311 737.28 366.0 0.4373 1.39362 +FS_25 Duct2.Fl_O 190.90 40.150 765.08 183.33 0.0000 84.86 35.223 737.28 366.9 0.4373 1.39362 +FS_3 HPC.Fl_O 190.90 219.983 1293.33 315.23 0.0000 20.14 206.750 1272.14 119.9 0.3029 1.36231 +FS_36 Bld3.Fl_O 173.72 219.983 1293.33 315.23 0.0000 18.33 206.750 1272.14 109.1 0.3029 1.36231 +FS_4 Burner.Fl_O 177.08 207.884 2483.73 657.03 0.0194 27.39 206.545 2480.02 483.4 0.0997 1.30091 +FS_45 HPT.Fl_O 194.26 76.948 1937.64 497.18 0.0176 71.71 72.581 1910.49 439.1 0.2987 1.31799 +FS_48 Duct3.Fl_O 194.26 76.563 1937.64 497.18 0.0176 72.07 72.218 1910.49 441.4 0.2987 1.31799 +FS_5 LPT.Fl_O 194.26 15.944 1356.94 337.09 0.0176 289.62 14.597 1326.43 1477.4 0.3638 1.34626 +FS_7 Duct4.Fl_O 194.26 15.784 1356.94 337.09 0.0176 292.55 15.090 1341.32 2018.9 0.2591 1.34626 +FS_9 Core_Nozz.Fl_O 194.26 15.784 1356.94 337.09 0.0176 292.55 8.442 1152.72 862.9 1.0000 1.34626 +FS_15 BypBld.Fl_O 1053.06 17.870 587.70 140.52 0.0000 921.85 15.407 563.34 3795.6 0.4652 1.39923 +FS_17 Duct5.Fl_O 1053.06 17.736 587.70 140.52 0.0000 928.82 15.292 563.34 3824.3 0.4652 1.39923 +FS_19 Byp_Nozz.Fl_O 1053.06 17.736 587.70 140.52 0.0000 928.82 9.367 489.67 2706.4 1.0000 1.39923 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1584.67 1.561 0.9025 3611.792 1.1503 0.9084 -32439.2 31.74 18.34 +LPC 167.53 2.258 0.8628 3367.509 1.3018 0.8774 -11562.3 27.84 20.31 +HPC 84.86 5.479 0.8651 6307.823 1.6904 0.8918 -35626.1 22.35 22.44 +HPT 27.39 2.702 0.9145 153.722 1.2352 0.9047 35625.9 +LPT 72.07 4.802 0.9265 81.434 1.4280 0.9114 44002.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3038.42 1.390 0.9323 0.916 2.0955 0.5215 1.4369 0.9679 3943.9586 +LPC 179.70 1.386 0.8987 0.919 1.7108 0.9323 3.2631 0.9600 3662.6571 +HPC 201.75 21.705 0.8534 0.992 2.0971 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.005 0.9329 100.399 5.0050 1.4085 0.4249 0.9803 1.5311 +LPT 149.76 6.304 0.9253 100.398 6.3037 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5027.44 28627.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 953.65 229.49 66.496 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 953.65 229.49 66.496 +Duct1 0.0025 0.4388 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 953.65 229.49 66.496 +Duct2 0.0025 0.4373 365.99 +Duct3 0.0050 0.2987 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3638 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.6814 1293.33 315.23 219.983 +Duct5 0.0075 0.4652 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 10.4993 1293.33 315.23 219.983 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 587.70 140.52 17.870 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5164 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7661.1 24423.7 35625.9 +LP_Shaft 3584.6 64471.3 44002.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2483.73 0.9940 0.0550 3.36629 0.01938 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.139 0.9975 1.0000 0.9975 2706.36 1.000 1082.4 38334.7 +Core_Nozz 1.903 0.9999 1.0000 0.9999 862.88 1.000 1639.6 10028.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 200 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 15000.0 0.00 1160.13 14801.2 0.6182 9149.85 5.9988 740.43 15.883 2282.7 2227.4 1773.5 + core size:20.49 Q: 409.99 Maximum Thrust: 24668.9 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1160.13 11.507 510.89 122.09 0.0000 1470.48 8.293 465.18 4688.7 0.7000 1.40065 +FS_2 Inlet.Fl_O 1160.13 11.449 510.89 122.09 0.0000 1477.89 9.779 488.34 5943.4 0.4799 1.40065 +FS_21 Fan.Fl_O 1160.13 16.686 574.67 137.39 0.0000 1075.54 14.491 551.99 4515.2 0.4534 1.39945 +FS_13 Splitter.Fl_O2 994.37 16.686 574.67 137.39 0.0000 921.87 14.386 550.84 3795.6 0.4652 1.39945 +FS_22 Splitter.Fl_O1 165.76 16.686 574.67 137.39 0.0000 153.68 14.984 557.29 719.5 0.3950 1.39945 +FS_23 Duct1.Fl_O 165.76 16.644 574.67 137.39 0.0000 154.06 14.946 557.29 721.3 0.3950 1.39945 +FS_24 LPC.Fl_O 165.76 35.396 735.76 176.22 0.0000 81.97 31.368 711.01 366.0 0.4197 1.39481 +FS_25 Duct2.Fl_O 165.76 35.308 735.76 176.22 0.0000 82.17 31.289 711.01 366.9 0.4197 1.39481 +FS_3 HPC.Fl_O 165.76 182.763 1225.49 297.82 0.0000 20.49 171.355 1204.45 119.9 0.3083 1.36654 +FS_36 Bld3.Fl_O 150.84 182.763 1225.49 297.82 0.0000 18.64 171.355 1204.45 109.1 0.3083 1.36654 +FS_4 Burner.Fl_O 153.38 172.711 2282.70 596.04 0.0168 27.38 171.600 2279.23 483.4 0.0994 1.30766 +FS_45 HPT.Fl_O 168.30 63.520 1773.53 449.84 0.0153 72.00 59.886 1747.98 439.1 0.2990 1.32629 +FS_48 Duct3.Fl_O 168.30 63.203 1773.53 449.84 0.0153 72.36 59.586 1747.98 441.4 0.2990 1.32629 +FS_5 LPT.Fl_O 168.30 13.433 1242.13 306.12 0.0153 284.94 12.340 1214.77 1477.4 0.3557 1.35491 +FS_7 Duct4.Fl_O 168.30 13.299 1242.13 306.12 0.0153 287.82 12.734 1228.08 2018.9 0.2537 1.35491 +FS_9 Core_Nozz.Fl_O 168.30 13.299 1242.13 306.12 0.0153 287.82 8.293 1096.36 862.9 0.8585 1.35491 +FS_15 BypBld.Fl_O 994.37 16.686 574.67 137.39 0.0000 921.87 14.386 550.84 3795.6 0.4652 1.39945 +FS_17 Duct5.Fl_O 994.37 16.560 574.67 137.39 0.0000 928.83 14.278 550.84 3824.3 0.4652 1.39945 +FS_19 Byp_Nozz.Fl_O 994.37 16.560 574.67 137.39 0.0000 928.83 8.746 478.77 2706.3 1.0000 1.39945 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1477.89 1.457 0.9105 3360.142 1.1248 0.9152 -25115.2 39.71 19.77 +LPC 154.06 2.127 0.8542 3168.201 1.2803 0.8687 -9106.8 25.19 16.56 +HPC 82.17 5.176 0.8659 6251.578 1.6656 0.8917 -28518.2 26.42 26.57 +HPT 27.38 2.719 0.9149 155.844 1.2419 0.9049 28518.5 +LPT 72.36 4.705 0.9219 79.187 1.4278 0.9057 34222.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2833.61 1.318 0.9406 0.852 2.0410 0.5215 1.4369 0.9679 3943.9586 +LPC 165.25 1.345 0.8898 0.865 1.6216 0.9323 3.2631 0.9600 3662.6571 +HPC 195.35 20.306 0.8542 0.983 2.1341 0.4206 0.2163 1.0137 6357.1603 +HPT 30.12 5.046 0.9333 101.784 5.0458 1.4085 0.4249 0.9803 1.5311 +LPT 150.36 6.168 0.9207 97.628 6.1683 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4688.66 26698.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 910.21 218.78 56.910 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 910.21 218.78 56.910 +Duct1 0.0025 0.3950 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 910.21 218.78 56.910 +Duct2 0.0025 0.4197 365.99 +Duct3 0.0050 0.2990 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3557 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.8016 1225.49 297.82 182.763 +Duct5 0.0075 0.4652 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.1169 1225.49 297.82 182.763 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 574.67 137.39 16.686 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9988 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7445.8 20116.3 28518.5 +LP_Shaft 3334.8 53897.3 34222.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2282.70 0.9940 0.0550 2.54163 0.01685 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.997 0.9976 1.0000 0.9975 2706.36 1.000 1070.4 34305.7 +Core_Nozz 1.604 0.9999 1.0000 0.9999 862.88 0.858 1375.3 7194.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 201 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 15000.0 0.00 1061.89 9867.7 0.6495 6409.13 6.7193 740.43 12.493 2058.5 2010.3 1590.7 + core size:20.88 Q: 409.99 Maximum Thrust: 24668.9 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1061.89 11.507 510.89 122.09 0.0000 1345.96 8.293 465.18 4291.6 0.7000 1.40065 +FS_2 Inlet.Fl_O 1061.89 11.449 510.89 122.09 0.0000 1352.74 10.097 492.85 5943.4 0.4274 1.40065 +FS_21 Fan.Fl_O 1061.89 15.316 559.61 133.77 0.0000 1058.37 13.377 538.39 4515.2 0.4439 1.39972 +FS_13 Splitter.Fl_O2 924.33 15.316 559.61 133.77 0.0000 921.26 13.208 536.44 3795.6 0.4647 1.39972 +FS_22 Splitter.Fl_O1 137.56 15.316 559.61 133.77 0.0000 137.11 14.106 546.61 719.5 0.3449 1.39972 +FS_23 Duct1.Fl_O 137.56 15.277 559.61 133.77 0.0000 137.45 14.071 546.61 721.3 0.3449 1.39972 +FS_24 LPC.Fl_O 137.56 29.597 697.00 166.84 0.0000 79.18 26.487 675.38 366.0 0.4018 1.39611 +FS_25 Duct2.Fl_O 137.56 29.523 697.00 166.84 0.0000 79.38 26.421 675.38 366.9 0.4018 1.39611 +FS_3 HPC.Fl_O 137.56 143.761 1143.60 277.00 0.0000 20.88 134.414 1122.93 119.9 0.3143 1.37170 +FS_36 Bld3.Fl_O 125.18 143.761 1143.60 277.00 0.0000 19.00 134.414 1122.93 109.1 0.3143 1.37170 +FS_4 Burner.Fl_O 126.96 135.854 2058.50 529.65 0.0142 27.36 134.981 2055.32 483.4 0.0990 1.31601 +FS_45 HPT.Fl_O 139.34 49.501 1590.74 398.46 0.0129 72.45 46.633 1566.97 439.1 0.2999 1.33653 +FS_48 Duct3.Fl_O 139.34 49.254 1590.74 398.46 0.0129 72.81 46.400 1566.97 441.4 0.2999 1.33653 +FS_5 LPT.Fl_O 139.34 11.456 1131.13 276.76 0.0129 263.98 10.668 1109.81 1477.4 0.3246 1.36359 +FS_7 Duct4.Fl_O 139.34 11.341 1131.13 276.76 0.0129 266.65 10.931 1120.06 2018.9 0.2330 1.36359 +FS_9 Core_Nozz.Fl_O 139.34 11.341 1131.13 276.76 0.0129 266.65 8.293 1039.94 862.9 0.6909 1.36359 +FS_15 BypBld.Fl_O 924.33 15.316 559.61 133.77 0.0000 921.26 13.208 536.44 3795.6 0.4647 1.39972 +FS_17 Duct5.Fl_O 924.33 15.201 559.61 133.77 0.0000 928.22 13.109 536.44 3824.3 0.4647 1.39972 +FS_19 Byp_Nozz.Fl_O 924.33 15.201 559.61 133.77 0.0000 928.22 8.293 470.56 2706.4 0.9718 1.39972 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1352.74 1.338 0.9096 3026.662 1.0954 0.9133 -17556.3 47.62 21.57 +LPC 137.45 1.937 0.8443 2891.911 1.2455 0.8581 -6436.4 23.32 13.25 +HPC 79.38 4.870 0.8648 6203.842 1.6407 0.8904 -21439.4 31.01 31.24 +HPT 27.36 2.744 0.9154 158.510 1.2506 0.9052 21439.4 +LPT 72.81 4.300 0.9178 75.315 1.4063 0.9018 23992.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2593.70 1.235 0.9398 0.767 2.0820 0.5215 1.4369 0.9679 3943.9586 +LPC 147.43 1.287 0.8795 0.790 1.5533 0.9323 3.2631 0.9600 3662.6571 +HPC 188.72 18.888 0.8531 0.976 2.1668 0.4206 0.2163 1.0137 6357.1603 +HPT 30.10 5.106 0.9338 103.526 5.1057 1.4085 0.4249 0.9803 1.5311 +LPT 151.30 5.603 0.9166 92.854 5.6028 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4291.63 24437.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 855.64 205.40 46.259 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 855.64 205.40 46.259 +Duct1 0.0025 0.3449 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 855.64 205.40 46.259 +Duct2 0.0025 0.4018 365.99 +Duct3 0.0050 0.2999 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3246 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.8147 1143.60 277.00 143.761 +Duct5 0.0075 0.4647 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.5660 1143.60 277.00 143.761 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 559.61 133.77 15.316 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.7193 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7191.7 15657.2 21439.4 +LP_Shaft 3003.9 41950.3 23992.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2058.50 0.9940 0.0550 1.78031 0.01422 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.833 0.9975 1.0000 0.9975 2706.36 0.972 1031.3 29627.5 +Core_Nozz 1.367 0.9999 1.0000 0.9999 862.88 0.691 1080.1 4677.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 202 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 15000.0 0.00 937.97 4933.7 0.7733 3815.14 7.8736 740.43 8.878 1767.8 1728.6 1355.6 + core size:21.48 Q: 409.99 Maximum Thrust: 24668.9 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 937.97 11.507 510.89 122.09 0.0000 1188.90 8.293 465.18 3790.8 0.7000 1.40065 +FS_2 Inlet.Fl_O 937.97 11.449 510.89 122.09 0.0000 1194.88 10.431 497.45 5943.4 0.3671 1.40065 +FS_21 Fan.Fl_O 937.97 13.753 541.81 129.50 0.0000 1024.39 12.141 522.84 4515.2 0.4257 1.40007 +FS_13 Splitter.Fl_O2 832.27 13.753 541.81 129.50 0.0000 908.95 11.921 520.12 3795.6 0.4564 1.40007 +FS_22 Splitter.Fl_O1 105.70 13.753 541.81 129.50 0.0000 115.44 13.004 533.21 719.5 0.2839 1.40007 +FS_23 Duct1.Fl_O 105.70 13.719 541.81 129.50 0.0000 115.73 12.972 533.21 721.3 0.2839 1.40007 +FS_24 LPC.Fl_O 105.70 23.008 645.25 154.36 0.0000 75.31 20.851 627.41 366.0 0.3778 1.39797 +FS_25 Duct2.Fl_O 105.70 22.950 645.25 154.36 0.0000 75.49 20.799 627.41 366.9 0.3778 1.39797 +FS_3 HPC.Fl_O 105.70 102.154 1034.45 249.57 0.0000 21.48 95.098 1014.29 119.9 0.3237 1.37856 +FS_36 Bld3.Fl_O 96.19 102.154 1034.45 249.57 0.0000 19.54 95.098 1014.29 109.1 0.3237 1.37856 +FS_4 Burner.Fl_O 97.25 96.535 1767.80 446.21 0.0110 27.33 95.916 1764.99 483.4 0.0984 1.32951 +FS_45 HPT.Fl_O 106.76 34.752 1355.60 334.43 0.0100 72.99 32.707 1334.36 439.1 0.3006 1.35144 +FS_48 Duct3.Fl_O 106.76 34.578 1355.60 334.43 0.0100 73.36 32.544 1334.36 441.4 0.3006 1.35144 +FS_5 LPT.Fl_O 106.76 9.960 1007.42 244.68 0.0100 219.55 9.498 994.51 1477.4 0.2635 1.37345 +FS_7 Duct4.Fl_O 106.76 9.860 1007.42 244.68 0.0100 221.77 9.617 1000.60 2018.9 0.1911 1.37345 +FS_9 Core_Nozz.Fl_O 106.76 9.860 1007.42 244.68 0.0100 221.77 8.293 960.96 862.9 0.5076 1.37345 +FS_15 BypBld.Fl_O 832.27 13.753 541.81 129.50 0.0000 908.95 11.921 520.12 3795.6 0.4564 1.40007 +FS_17 Duct5.Fl_O 832.27 13.650 541.81 129.50 0.0000 915.82 11.832 520.12 3824.3 0.4564 1.40007 +FS_19 Byp_Nozz.Fl_O 832.27 13.650 541.81 129.50 0.0000 915.82 8.293 469.82 2706.4 0.8743 1.40007 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1194.88 1.201 0.8894 2559.299 1.0605 0.8923 -9839.2 57.71 23.52 +LPC 115.73 1.677 0.8327 2485.196 1.1909 0.8444 -3717.6 24.47 10.18 +HPC 75.49 4.451 0.8628 6130.295 1.6032 0.8877 -14238.9 38.08 38.61 +HPT 27.33 2.778 0.9163 162.623 1.2637 0.9056 14239.0 +LPT 73.36 3.472 0.9105 68.988 1.3456 0.8957 13556.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2291.03 1.140 0.9189 0.649 2.2505 0.5215 1.4369 0.9679 3943.9586 +LPC 124.14 1.208 0.8674 0.679 1.5310 0.9323 3.2631 0.9600 3662.6571 +HPC 179.48 16.954 0.8511 0.964 2.2439 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.184 0.9347 106.212 5.1843 1.4085 0.4249 0.9803 1.5311 +LPT 152.43 4.448 0.9094 85.054 4.4482 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3790.83 21586.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 783.01 187.68 34.554 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 783.01 187.68 34.554 +Duct1 0.0025 0.2839 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 783.01 187.68 34.554 +Duct2 0.0025 0.3778 365.99 +Duct3 0.0050 0.3006 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2635 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.6996 1034.45 249.57 102.154 +Duct5 0.0075 0.4564 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.8137 1034.45 249.57 102.154 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 541.81 129.50 13.753 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8736 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6837.5 10937.4 14239.0 +LP_Shaft 2540.0 28032.0 13556.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1767.80 0.9940 0.0550 1.05976 0.01102 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.646 0.9975 1.0000 0.9975 2706.36 0.874 927.1 23982.3 +Core_Nozz 1.189 0.9999 1.0000 0.9999 862.88 0.508 764.7 2537.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 203 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 11/ 21/ 1/ 9 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 15000.0 0.00 812.37 1233.5 1.5404 1900.03 9.6452 740.43 5.770 1437.5 1408.9 1093.5 + core size:22.39 Q: 409.99 Maximum Thrust: 24668.9 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 812.37 11.507 510.89 122.09 0.0000 1029.69 8.293 465.18 3283.2 0.7000 1.40065 +FS_2 Inlet.Fl_O 812.37 11.449 510.89 122.09 0.0000 1034.88 10.706 501.18 5943.4 0.3110 1.40065 +FS_21 Fan.Fl_O 812.37 12.410 525.97 125.70 0.0000 968.74 11.132 509.86 4515.2 0.3971 1.40038 +FS_13 Splitter.Fl_O2 736.06 12.410 525.97 125.70 0.0000 877.73 10.889 506.66 3795.6 0.4362 1.40038 +FS_22 Splitter.Fl_O1 76.31 12.410 525.97 125.70 0.0000 91.00 12.000 520.94 719.5 0.2195 1.40038 +FS_23 Duct1.Fl_O 76.31 12.379 525.97 125.70 0.0000 91.23 11.970 520.94 721.3 0.2195 1.40038 +FS_24 LPC.Fl_O 76.31 17.300 590.32 141.15 0.0000 69.16 15.958 576.88 366.0 0.3416 1.39919 +FS_25 Duct2.Fl_O 76.31 17.257 590.32 141.15 0.0000 69.33 15.918 576.88 366.9 0.3416 1.39919 +FS_3 HPC.Fl_O 76.31 66.398 911.02 218.98 0.0000 22.39 61.379 891.27 119.9 0.3385 1.38618 +FS_36 Bld3.Fl_O 69.45 66.398 911.02 218.98 0.0000 20.37 61.379 891.27 109.1 0.3385 1.38618 +FS_4 Burner.Fl_O 69.97 62.746 1437.54 355.32 0.0076 27.28 62.345 1435.16 483.4 0.0975 1.34832 +FS_45 HPT.Fl_O 76.84 22.342 1093.50 265.84 0.0069 73.39 21.013 1075.52 439.1 0.3003 1.37004 +FS_48 Duct3.Fl_O 76.84 22.230 1093.50 265.84 0.0069 73.76 20.908 1075.52 441.4 0.3003 1.37004 +FS_5 LPT.Fl_O 76.84 9.087 879.68 212.29 0.0069 161.84 8.864 873.64 1477.4 0.1899 1.38348 +FS_7 Duct4.Fl_O 76.84 8.996 879.68 212.29 0.0069 163.48 8.877 876.44 2018.9 0.1390 1.38348 +FS_9 Core_Nozz.Fl_O 76.84 8.996 879.68 212.29 0.0069 163.48 8.293 860.08 862.8 0.3446 1.38348 +FS_15 BypBld.Fl_O 736.06 12.410 525.97 125.70 0.0000 877.73 10.889 506.66 3795.6 0.4362 1.40038 +FS_17 Duct5.Fl_O 736.06 12.317 525.97 125.70 0.0000 884.37 10.807 506.66 3824.3 0.4362 1.40038 +FS_19 Byp_Nozz.Fl_O 736.06 12.317 525.97 125.70 0.0000 884.37 8.293 469.68 2706.4 0.7732 1.40038 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1034.88 1.084 0.7901 1986.863 1.0295 0.7926 -4154.4 83.20 24.29 +LPC 91.23 1.397 0.8201 1958.176 1.1224 0.8284 -1667.8 30.61 8.51 +HPC 69.33 3.848 0.8536 6017.536 1.5433 0.8778 -8403.4 49.85 50.86 +HPT 27.28 2.808 0.9179 169.320 1.2800 0.9069 8403.4 +LPT 73.76 2.446 0.8999 59.632 1.2431 0.8880 5822.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1984.24 1.058 0.8163 0.504 2.6182 0.5215 1.4369 0.9679 3943.9586 +LPC 97.86 1.122 0.8543 0.535 1.5943 0.9323 3.2631 0.9600 3662.6571 +HPC 164.83 14.164 0.8420 0.947 2.3811 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.256 0.9363 110.586 5.2564 1.4085 0.4249 0.9803 1.5311 +LPT 153.27 3.018 0.8987 73.518 3.0176 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3283.20 18695.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 703.40 168.39 24.456 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 703.40 168.39 24.456 +Duct1 0.0025 0.2195 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 703.40 168.39 24.456 +Duct2 0.0025 0.3416 365.99 +Duct3 0.0050 0.3003 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1899 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.6710 911.02 218.98 66.398 +Duct5 0.0075 0.4362 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.1972 911.02 218.98 66.398 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 525.97 125.70 12.410 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.6452 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6419.7 6875.0 8403.4 +LP_Shaft 1971.9 15507.3 5822.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1437.54 0.9940 0.0550 0.52778 0.00760 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.485 0.9975 1.0000 0.9975 2706.36 0.773 819.7 18752.3 +Core_Nozz 1.085 0.9999 1.0000 0.9999 862.88 0.345 492.7 1176.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 204 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 9/ 19/ 1/ 7 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 20000.0 0.00 906.50 19557.8 0.4878 9539.57 5.0354 414.93 22.741 2441.8 2379.7 1907.5 + core size:19.93 Q: 109.02 Maximum Thrust: 19557.8 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 906.50 7.541 461.71 110.31 0.0000 1666.72 6.753 447.35 7720.9 0.4000 1.40126 +FS_2 Inlet.Fl_O 906.50 7.503 461.71 110.31 0.0000 1675.11 5.990 432.86 5943.4 0.5763 1.40126 +FS_21 Fan.Fl_O 906.50 12.353 543.24 129.84 0.0000 1103.71 10.624 520.32 4515.2 0.4691 1.40004 +FS_13 Splitter.Fl_O2 756.30 12.353 543.24 129.84 0.0000 920.84 10.655 520.76 3795.6 0.4644 1.40004 +FS_22 Splitter.Fl_O1 150.20 12.353 543.24 129.84 0.0000 182.87 10.450 517.88 719.5 0.4946 1.40004 +FS_23 Duct1.Fl_O 150.20 12.322 543.24 129.84 0.0000 183.33 10.424 517.88 721.3 0.4946 1.40004 +FS_24 LPC.Fl_O 150.20 30.653 728.63 174.49 0.0000 85.35 26.818 701.55 366.0 0.4417 1.39506 +FS_25 Duct2.Fl_O 150.20 30.577 728.63 174.49 0.0000 85.56 26.751 701.55 366.9 0.4417 1.39506 +FS_3 HPC.Fl_O 150.20 171.498 1243.50 302.43 0.0000 19.93 161.413 1223.47 119.9 0.2990 1.36541 +FS_36 Bld3.Fl_O 136.68 171.498 1243.50 302.43 0.0000 18.14 161.413 1223.47 109.1 0.2990 1.36541 +FS_4 Burner.Fl_O 139.33 162.066 2441.81 644.63 0.0194 27.41 161.020 2438.15 483.4 0.0997 1.30184 +FS_45 HPT.Fl_O 152.85 60.740 1907.54 488.64 0.0176 70.92 57.374 1881.38 439.1 0.2949 1.31914 +FS_48 Duct3.Fl_O 152.85 60.436 1907.54 488.64 0.0176 71.28 57.088 1881.38 441.4 0.2949 1.31914 +FS_5 LPT.Fl_O 152.85 12.404 1326.19 328.91 0.0176 289.58 11.357 1296.28 1477.4 0.3635 1.34813 +FS_7 Duct4.Fl_O 152.85 12.280 1326.19 328.91 0.0176 292.50 11.740 1310.88 2018.9 0.2588 1.34813 +FS_9 Core_Nozz.Fl_O 152.85 12.280 1326.19 328.91 0.0176 292.50 6.753 1134.27 862.9 0.9753 1.34813 +FS_15 BypBld.Fl_O 756.30 12.353 543.24 129.84 0.0000 920.84 10.655 520.76 3795.6 0.4644 1.40004 +FS_17 Duct5.Fl_O 756.30 12.260 543.24 129.84 0.0000 927.80 10.575 520.76 3824.3 0.4644 1.40004 +FS_19 Byp_Nozz.Fl_O 756.30 12.260 543.24 129.84 0.0000 927.80 6.753 458.02 2706.4 0.9634 1.40004 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.646 0.8682 3944.235 1.1766 0.8772 -25056.2 24.61 17.36 +LPC 183.33 2.488 0.8683 3636.227 1.3413 0.8839 -9487.8 28.39 23.30 +HPC 85.56 5.609 0.8651 6325.867 1.7066 0.8922 -27187.0 20.09 20.14 +HPT 27.41 2.668 0.9134 151.730 1.2322 0.9036 27187.5 +LPT 71.28 4.872 0.9324 85.205 1.4384 0.9183 34543.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.450 0.8969 1.000 2.3630 0.5215 1.4369 0.9679 3943.9586 +LPC 196.65 1.456 0.9045 0.993 1.7667 0.9323 3.2631 0.9600 3662.6571 +HPC 203.41 22.306 0.8535 0.995 2.0419 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.926 0.9317 99.098 4.9262 1.4085 0.4249 0.9803 1.5311 +LPT 148.10 6.402 0.9312 105.047 6.4020 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 7720.89 11690.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 912.20 219.27 51.222 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 912.20 219.27 51.222 +Duct1 0.0025 0.4946 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 912.20 219.27 51.222 +Duct2 0.0025 0.4417 365.99 +Duct3 0.0050 0.2949 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3635 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.2569 1243.50 302.43 171.498 +Duct5 0.0075 0.4644 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.2608 1243.50 302.43 171.498 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 543.24 129.84 12.353 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0354 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7497.7 19044.7 27187.5 +LP_Shaft 3721.4 48752.0 34543.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2441.81 0.9940 0.0550 2.64988 0.01939 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.815 0.9975 1.0000 0.9975 2706.36 0.963 1008.6 23709.7 +Core_Nozz 1.818 0.9999 1.0000 0.9999 862.88 0.975 1586.9 7538.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 205 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 20000.0 0.00 879.36 17602.0 0.4750 8360.45 5.3136 414.93 20.667 2349.0 2289.5 1827.7 + core size:20.02 Q: 109.02 Maximum Thrust: 19557.8 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 879.36 7.541 461.71 110.31 0.0000 1616.82 6.753 447.35 7489.7 0.4000 1.40126 +FS_2 Inlet.Fl_O 879.36 7.503 461.71 110.31 0.0000 1624.96 6.109 435.32 5943.4 0.5496 1.40126 +FS_21 Fan.Fl_O 879.36 12.034 536.34 128.19 0.0000 1092.01 10.393 514.31 4515.2 0.4624 1.40018 +FS_13 Splitter.Fl_O2 740.08 12.034 536.34 128.19 0.0000 919.04 10.388 514.25 3795.6 0.4631 1.40018 +FS_22 Splitter.Fl_O1 139.28 12.034 536.34 128.19 0.0000 172.96 10.417 514.65 719.5 0.4587 1.40018 +FS_23 Duct1.Fl_O 139.28 12.004 536.34 128.19 0.0000 173.39 10.391 514.65 721.3 0.4587 1.40018 +FS_24 LPC.Fl_O 139.28 27.724 703.19 168.34 0.0000 85.96 24.196 676.54 366.0 0.4457 1.39590 +FS_25 Duct2.Fl_O 139.28 27.655 703.19 168.34 0.0000 86.18 24.136 676.54 366.9 0.4457 1.39590 +FS_3 HPC.Fl_O 139.28 155.853 1204.86 292.55 0.0000 20.02 146.601 1185.17 119.9 0.3002 1.36784 +FS_36 Bld3.Fl_O 126.75 155.853 1204.86 292.55 0.0000 18.22 146.601 1185.17 109.1 0.3002 1.36784 +FS_4 Burner.Fl_O 129.07 147.281 2348.97 616.48 0.0183 27.41 146.331 2345.43 483.4 0.0996 1.30486 +FS_45 HPT.Fl_O 141.60 54.581 1827.67 465.62 0.0167 71.57 51.497 1801.87 439.1 0.2974 1.32305 +FS_48 Duct3.Fl_O 141.60 54.308 1827.67 465.62 0.0167 71.93 51.240 1801.87 441.4 0.2974 1.32305 +FS_5 LPT.Fl_O 141.60 11.363 1274.97 315.10 0.0167 287.13 10.422 1246.55 1477.4 0.3593 1.35195 +FS_7 Duct4.Fl_O 141.60 11.249 1274.97 315.10 0.0167 290.03 10.764 1260.39 2018.9 0.2561 1.35195 +FS_9 Core_Nozz.Fl_O 141.60 11.249 1274.97 315.10 0.0167 290.03 6.753 1114.87 862.9 0.8951 1.35195 +FS_15 BypBld.Fl_O 740.08 12.034 536.34 128.19 0.0000 919.04 10.388 514.25 3795.6 0.4631 1.40018 +FS_17 Duct5.Fl_O 740.08 11.944 536.34 128.19 0.0000 925.99 10.310 514.25 3824.3 0.4631 1.40018 +FS_19 Byp_Nozz.Fl_O 740.08 11.944 536.34 128.19 0.0000 925.99 6.753 455.59 2706.4 0.9402 1.40018 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1624.96 1.604 0.8954 3720.136 1.1616 0.9022 -22245.5 28.46 17.60 +LPC 173.39 2.310 0.8660 3451.632 1.3111 0.8808 -7911.9 29.18 22.24 +HPC 86.18 5.636 0.8636 6341.962 1.7134 0.8912 -24477.9 20.32 20.33 +HPT 27.41 2.698 0.9139 152.362 1.2375 0.9040 24477.9 +LPT 71.93 4.779 0.9280 82.101 1.4335 0.9129 30157.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3115.68 1.420 0.9251 0.943 2.1441 0.5215 1.4369 0.9679 3943.9586 +LPC 185.99 1.401 0.9020 0.942 1.7566 0.9323 3.2631 0.9600 3662.6571 +HPC 204.88 22.430 0.8520 0.998 2.0724 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.997 0.9322 99.510 4.9974 1.4085 0.4249 0.9803 1.5311 +LPT 149.47 6.272 0.9268 101.220 6.2720 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 7489.74 11340.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 881.84 211.81 46.436 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 881.84 211.81 46.436 +Duct1 0.0025 0.4587 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 881.84 211.81 46.436 +Duct2 0.0025 0.4457 365.99 +Duct3 0.0050 0.2974 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3593 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.8748 1204.86 292.55 155.853 +Duct5 0.0075 0.4631 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.6604 1204.86 292.55 155.853 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 536.34 128.19 12.034 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3136 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7384.4 17409.8 24477.9 +LP_Shaft 3509.9 45126.5 30157.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2348.97 0.9940 0.0550 2.32235 0.01832 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.769 0.9975 1.0000 0.9975 2706.36 0.940 981.8 22583.0 +Core_Nozz 1.666 0.9999 1.0000 0.9999 862.88 0.895 1445.0 6359.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 206 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 20000.0 0.00 847.29 15646.2 0.4683 7327.67 5.5129 414.93 18.904 2256.4 2199.9 1750.9 + core size:20.16 Q: 109.02 Maximum Thrust: 19557.8 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 847.29 7.541 461.71 110.31 0.0000 1557.85 6.753 447.35 7216.6 0.4000 1.40126 +FS_2 Inlet.Fl_O 847.29 7.503 461.71 110.31 0.0000 1565.69 6.238 437.93 5943.4 0.5202 1.40126 +FS_21 Fan.Fl_O 847.29 11.639 529.95 126.66 0.0000 1081.39 10.088 508.71 4515.2 0.4565 1.40031 +FS_13 Splitter.Fl_O2 717.20 11.639 529.95 126.66 0.0000 915.36 10.062 508.34 3795.6 0.4607 1.40031 +FS_22 Splitter.Fl_O1 130.09 11.639 529.95 126.66 0.0000 166.04 10.219 510.60 719.5 0.4350 1.40031 +FS_23 Duct1.Fl_O 130.09 11.610 529.95 126.66 0.0000 166.45 10.194 510.60 721.3 0.4350 1.40031 +FS_24 LPC.Fl_O 130.09 25.795 686.86 164.39 0.0000 85.29 22.573 661.31 366.0 0.4411 1.39646 +FS_25 Duct2.Fl_O 130.09 25.730 686.86 164.39 0.0000 85.51 22.516 661.31 366.9 0.4411 1.39646 +FS_3 HPC.Fl_O 130.09 142.560 1172.00 284.19 0.0000 20.16 133.969 1152.47 119.9 0.3024 1.36991 +FS_36 Bld3.Fl_O 118.38 142.560 1172.00 284.19 0.0000 18.34 133.969 1152.47 109.1 0.3024 1.36991 +FS_4 Burner.Fl_O 120.42 134.719 2256.43 588.63 0.0172 27.40 133.851 2253.00 483.4 0.0994 1.30813 +FS_45 HPT.Fl_O 132.13 49.665 1750.95 443.70 0.0156 71.84 46.837 1725.80 439.1 0.2982 1.32709 +FS_48 Duct3.Fl_O 132.13 49.416 1750.95 443.70 0.0156 72.20 46.603 1725.80 441.4 0.2982 1.32709 +FS_5 LPT.Fl_O 132.13 10.576 1224.95 301.71 0.0156 282.14 9.734 1198.52 1477.4 0.3515 1.35580 +FS_7 Duct4.Fl_O 132.13 10.471 1224.95 301.71 0.0156 284.99 10.035 1211.36 2018.9 0.2509 1.35580 +FS_9 Core_Nozz.Fl_O 132.13 10.471 1224.95 301.71 0.0156 284.99 6.753 1090.71 862.9 0.8254 1.35580 +FS_15 BypBld.Fl_O 717.20 11.639 529.95 126.66 0.0000 915.36 10.062 508.34 3795.6 0.4607 1.40031 +FS_17 Duct5.Fl_O 717.20 11.552 529.95 126.66 0.0000 922.27 9.987 508.34 3824.3 0.4607 1.40031 +FS_19 Byp_Nozz.Fl_O 717.20 11.552 529.95 126.66 0.0000 922.27 6.753 454.47 2706.3 0.9100 1.40031 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1565.69 1.551 0.9057 3575.573 1.1478 0.9114 -19597.0 32.29 18.07 +LPC 166.45 2.222 0.8633 3337.444 1.2961 0.8777 -6945.8 28.67 20.68 +HPC 85.51 5.541 0.8642 6323.524 1.7063 0.8916 -22051.0 21.72 21.79 +HPT 27.40 2.713 0.9145 153.192 1.2415 0.9044 22051.0 +LPT 72.20 4.672 0.9263 80.621 1.4294 0.9110 26543.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3002.04 1.384 0.9357 0.907 2.0513 0.5215 1.4369 0.9679 3943.9586 +LPC 178.54 1.374 0.8992 0.911 1.7275 0.9323 3.2631 0.9600 3662.6571 +HPC 203.28 21.990 0.8526 0.995 2.0980 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.031 0.9328 100.052 5.0308 1.4085 0.4249 0.9803 1.5311 +LPT 150.02 6.123 0.9251 99.396 6.1227 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 7216.57 10927.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 859.43 206.32 42.846 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 859.43 206.32 42.846 +Duct1 0.0025 0.4350 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 859.43 206.32 42.846 +Duct2 0.0025 0.4411 365.99 +Duct3 0.0050 0.2982 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3515 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.5533 1172.00 284.19 142.560 +Duct5 0.0075 0.4607 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.1551 1172.00 284.19 142.560 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 529.95 126.66 11.639 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5129 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7276.9 15915.3 22051.0 +LP_Shaft 3373.5 41323.8 26543.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2256.43 0.9940 0.0550 2.03546 0.01719 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.711 0.9975 1.0000 0.9975 2706.36 0.910 949.1 21156.3 +Core_Nozz 1.550 0.9999 1.0000 0.9999 862.88 0.825 1319.1 5417.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 207 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 20000.0 0.00 772.10 11734.8 0.4664 5473.03 5.9583 414.93 15.427 2072.4 2021.6 1600.5 + core size:20.44 Q: 109.02 Maximum Thrust: 19557.8 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 772.10 7.541 461.71 110.31 0.0000 1419.60 6.753 447.35 6576.1 0.4000 1.40126 +FS_2 Inlet.Fl_O 772.10 7.503 461.71 110.31 0.0000 1426.75 6.498 443.08 5943.4 0.4577 1.40126 +FS_21 Fan.Fl_O 772.10 10.779 516.96 123.54 0.0000 1050.94 9.437 497.67 4515.2 0.4398 1.40055 +FS_13 Splitter.Fl_O2 661.14 10.779 516.96 123.54 0.0000 899.91 9.377 496.76 3795.6 0.4504 1.40055 +FS_22 Splitter.Fl_O1 110.96 10.779 516.96 123.54 0.0000 151.04 9.722 501.93 719.5 0.3866 1.40055 +FS_23 Duct1.Fl_O 110.96 10.752 516.96 123.54 0.0000 151.41 9.698 501.93 721.3 0.3866 1.40055 +FS_24 LPC.Fl_O 110.96 21.932 653.16 156.26 0.0000 83.44 19.332 630.11 366.0 0.4287 1.39770 +FS_25 Duct2.Fl_O 110.96 21.877 653.16 156.26 0.0000 83.64 19.283 630.11 366.9 0.4287 1.39770 +FS_3 HPC.Fl_O 110.96 116.340 1102.91 266.73 0.0000 20.44 109.118 1083.81 119.9 0.3066 1.37426 +FS_36 Bld3.Fl_O 100.98 116.340 1102.91 266.73 0.0000 18.60 109.118 1083.81 109.1 0.3066 1.37426 +FS_4 Burner.Fl_O 102.50 109.941 2072.44 534.14 0.0151 27.39 109.233 2069.24 483.4 0.0991 1.31497 +FS_45 HPT.Fl_O 112.48 40.193 1600.53 401.43 0.0137 72.25 37.877 1576.82 439.1 0.2991 1.33552 +FS_48 Duct3.Fl_O 112.48 39.992 1600.53 401.43 0.0137 72.61 37.688 1576.82 441.4 0.2991 1.33552 +FS_5 LPT.Fl_O 112.48 9.297 1136.51 278.31 0.0137 263.21 8.661 1115.27 1477.4 0.3236 1.36274 +FS_7 Duct4.Fl_O 112.48 9.204 1136.51 278.31 0.0137 265.87 8.873 1125.48 2018.9 0.2323 1.36274 +FS_9 Core_Nozz.Fl_O 112.48 9.204 1136.51 278.31 0.0137 265.87 6.753 1046.00 862.8 0.6872 1.36274 +FS_15 BypBld.Fl_O 661.14 10.779 516.96 123.54 0.0000 899.91 9.377 496.76 3795.6 0.4504 1.40055 +FS_17 Duct5.Fl_O 661.14 10.698 516.96 123.54 0.0000 906.71 9.307 496.76 3824.3 0.4504 1.40055 +FS_19 Byp_Nozz.Fl_O 661.14 10.698 516.96 123.54 0.0000 906.71 6.753 453.18 2706.4 0.8377 1.40055 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1426.75 1.437 0.9128 3265.601 1.1197 0.9172 -14456.7 39.75 18.65 +LPC 151.41 2.040 0.8565 3086.165 1.2635 0.8700 -5137.2 27.43 17.51 +HPC 83.64 5.318 0.8652 6280.488 1.6886 0.8921 -17342.2 24.80 24.92 +HPT 27.39 2.735 0.9148 154.817 1.2488 0.9045 17342.2 +LPT 72.61 4.302 0.9222 77.014 1.4083 0.9070 19593.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2735.63 1.304 0.9430 0.828 1.9717 0.5215 1.4369 0.9679 3943.9586 +LPC 162.42 1.319 0.8921 0.843 1.6680 0.9323 3.2631 0.9600 3662.6571 +HPC 198.86 20.960 0.8536 0.988 2.1337 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.084 0.9331 101.113 5.0844 1.4085 0.4249 0.9803 1.5311 +LPT 150.88 5.606 0.9210 94.949 5.6059 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6576.15 9957.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 812.78 194.93 35.716 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 812.78 194.93 35.716 +Duct1 0.0025 0.3866 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 812.78 194.93 35.716 +Duct2 0.0025 0.4287 365.99 +Duct3 0.0050 0.2991 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3236 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.8837 1102.91 266.73 116.340 +Duct5 0.0075 0.4504 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.1029 1102.91 266.73 116.340 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 516.96 123.54 10.779 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9583 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7047.9 12923.5 17342.2 +LP_Shaft 3081.1 33399.1 19593.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2072.44 0.9940 0.0550 1.52029 0.01506 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.584 0.9975 1.0000 0.9975 2706.36 0.838 872.4 17926.8 +Core_Nozz 1.363 0.9999 1.0000 0.9999 862.88 0.687 1077.0 3765.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 208 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 20000.0 0.00 680.17 7823.2 0.4815 3766.94 6.5218 414.93 11.889 1860.1 1815.6 1427.1 + core size:20.79 Q: 109.02 Maximum Thrust: 19557.8 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 680.17 7.541 461.71 110.31 0.0000 1250.57 6.753 447.35 5793.2 0.4000 1.40126 +FS_2 Inlet.Fl_O 680.17 7.503 461.71 110.31 0.0000 1256.87 6.755 448.03 5943.4 0.3901 1.40126 +FS_21 Fan.Fl_O 680.17 9.851 502.66 120.12 0.0000 998.88 8.762 486.09 4515.2 0.4124 1.40078 +FS_13 Splitter.Fl_O2 589.74 9.851 502.66 120.12 0.0000 866.08 8.681 484.80 3795.6 0.4287 1.40078 +FS_22 Splitter.Fl_O1 90.43 9.851 502.66 120.12 0.0000 132.80 9.126 491.78 719.5 0.3322 1.40078 +FS_23 Duct1.Fl_O 90.43 9.827 502.66 120.12 0.0000 133.13 9.103 491.78 721.3 0.3322 1.40078 +FS_24 LPC.Fl_O 90.43 17.742 611.58 146.26 0.0000 81.33 15.760 591.26 366.0 0.4150 1.39885 +FS_25 Duct2.Fl_O 90.43 17.698 611.58 146.26 0.0000 81.54 15.721 591.26 366.9 0.4150 1.39885 +FS_3 HPC.Fl_O 90.43 89.661 1020.50 246.09 0.0000 20.79 83.890 1001.97 119.9 0.3119 1.37943 +FS_36 Bld3.Fl_O 82.29 89.661 1020.50 246.09 0.0000 18.92 83.890 1001.97 109.1 0.3119 1.37943 +FS_4 Burner.Fl_O 83.33 84.730 1860.06 472.72 0.0127 27.37 84.185 1857.12 483.4 0.0987 1.32440 +FS_45 HPT.Fl_O 91.47 30.625 1427.07 353.87 0.0116 72.81 28.832 1405.08 439.1 0.3004 1.34617 +FS_48 Duct3.Fl_O 91.47 30.472 1427.07 353.87 0.0116 73.18 28.688 1405.08 441.4 0.3004 1.34617 +FS_5 LPT.Fl_O 91.47 8.309 1047.46 255.10 0.0116 229.92 7.884 1032.72 1477.4 0.2776 1.36987 +FS_7 Duct4.Fl_O 91.47 8.226 1047.46 255.10 0.0116 232.25 8.002 1039.70 2018.9 0.2008 1.36987 +FS_9 Core_Nozz.Fl_O 91.47 8.226 1047.46 255.10 0.0116 232.25 6.753 992.89 862.8 0.5435 1.36987 +FS_15 BypBld.Fl_O 589.74 9.851 502.66 120.12 0.0000 866.08 8.681 484.80 3795.6 0.4287 1.40078 +FS_17 Duct5.Fl_O 589.74 9.777 502.66 120.12 0.0000 872.63 8.616 484.80 3824.3 0.4287 1.40078 +FS_19 Byp_Nozz.Fl_O 589.74 9.777 502.66 120.12 0.0000 872.63 6.753 452.14 2706.4 0.7464 1.40078 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1256.87 1.313 0.9137 2864.106 1.0887 0.9170 -9438.0 44.13 18.61 +LPC 133.13 1.806 0.8488 2744.957 1.2167 0.8608 -3344.6 28.00 14.79 +HPC 81.54 5.066 0.8647 6239.681 1.6686 0.8911 -12772.1 28.60 28.78 +HPT 27.37 2.767 0.9152 157.101 1.2588 0.9044 12772.2 +LPT 73.18 3.668 0.9166 71.533 1.3624 0.9022 12782.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2409.88 1.218 0.9439 0.726 1.9593 0.5215 1.4369 0.9679 3943.9586 +LPC 142.80 1.247 0.8841 0.749 1.6451 0.9323 3.2631 0.9600 3662.6571 +HPC 193.84 19.797 0.8531 0.982 2.1722 0.4206 0.2163 1.0137 6357.1603 +HPT 30.12 5.158 0.9336 102.605 5.1581 1.4085 0.4249 0.9803 1.5311 +LPT 152.05 4.721 0.9155 88.191 4.7211 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5793.15 8771.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 756.31 181.20 28.241 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 756.31 181.20 28.241 +Duct1 0.0025 0.3322 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 756.31 181.20 28.241 +Duct2 0.0025 0.4150 365.99 +Duct3 0.0050 0.3004 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2776 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.1649 1020.50 246.09 89.661 +Duct5 0.0075 0.4287 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.9734 1020.50 246.09 89.661 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 502.66 120.12 9.851 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.5218 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6775.5 9900.5 12772.2 +LP_Shaft 2702.3 24843.6 12782.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1860.06 0.9940 0.0550 1.04637 0.01272 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.448 0.9975 1.0000 0.9975 2706.36 0.746 776.4 14231.3 +Core_Nozz 1.218 0.9999 1.0000 0.9999 862.88 0.544 831.4 2363.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 209 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 20000.0 0.00 560.74 3911.5 0.5536 2165.43 7.3325 414.93 8.141 1580.7 1544.7 1202.6 + core size:21.33 Q: 109.02 Maximum Thrust: 19557.8 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 560.74 7.541 461.71 110.31 0.0000 1031.00 6.753 447.35 4776.0 0.4000 1.40126 +FS_2 Inlet.Fl_O 560.74 7.503 461.71 110.31 0.0000 1036.19 7.015 452.90 5943.4 0.3113 1.40126 +FS_21 Fan.Fl_O 560.74 8.847 486.19 116.17 0.0000 901.86 8.071 473.58 4515.2 0.3643 1.40101 +FS_13 Splitter.Fl_O2 493.45 8.847 486.19 116.17 0.0000 793.63 7.987 472.17 3795.6 0.3848 1.40101 +FS_22 Splitter.Fl_O1 67.30 8.847 486.19 116.17 0.0000 108.23 8.427 479.47 719.5 0.2644 1.40101 +FS_23 Duct1.Fl_O 67.30 8.825 486.19 116.17 0.0000 108.51 8.406 479.47 721.3 0.2644 1.40101 +FS_24 LPC.Fl_O 67.30 13.245 557.72 133.32 0.0000 77.43 11.923 541.21 366.0 0.3904 1.39976 +FS_25 Duct2.Fl_O 67.30 13.212 557.72 133.32 0.0000 77.62 11.894 541.21 366.9 0.3904 1.39976 +FS_3 HPC.Fl_O 67.30 61.395 909.75 218.67 0.0000 21.33 57.216 892.04 119.9 0.3203 1.38626 +FS_36 Bld3.Fl_O 61.24 61.395 909.75 218.67 0.0000 19.41 57.216 892.04 109.1 0.3203 1.38626 +FS_4 Burner.Fl_O 61.84 58.018 1580.66 394.49 0.0098 27.35 57.645 1578.08 483.4 0.0981 1.33918 +FS_45 HPT.Fl_O 67.90 20.713 1202.56 294.21 0.0089 73.35 19.481 1183.11 439.1 0.3011 1.36172 +FS_48 Duct3.Fl_O 67.90 20.609 1202.56 294.21 0.0089 73.72 19.384 1183.11 441.4 0.3011 1.36172 +FS_5 LPT.Fl_O 67.90 7.554 944.95 228.81 0.0089 178.29 7.328 937.09 1477.4 0.2106 1.37813 +FS_7 Duct4.Fl_O 67.90 7.479 944.95 228.81 0.0089 180.09 7.358 940.74 2018.9 0.1538 1.37813 +FS_9 Core_Nozz.Fl_O 67.90 7.479 944.95 228.81 0.0089 180.09 6.753 918.83 862.9 0.3872 1.37813 +FS_15 BypBld.Fl_O 493.45 8.847 486.19 116.17 0.0000 793.63 7.987 472.17 3795.6 0.3848 1.40101 +FS_17 Duct5.Fl_O 493.45 8.780 486.19 116.17 0.0000 799.62 7.927 472.17 3824.3 0.3848 1.40101 +FS_19 Byp_Nozz.Fl_O 493.45 8.780 486.19 116.17 0.0000 799.62 6.753 450.99 2706.4 0.6237 1.40101 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1036.19 1.179 0.9105 2286.710 1.0530 0.9126 -4649.8 51.26 17.04 +LPC 108.51 1.501 0.8371 2228.404 1.1471 0.8462 -1632.8 34.26 12.18 +HPC 77.62 4.647 0.8630 6170.674 1.6312 0.8885 -8126.2 35.20 35.56 +HPT 27.35 2.801 0.9161 160.944 1.2726 0.9049 8126.5 +LPT 73.72 2.728 0.9017 62.215 1.2726 0.8886 6282.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1986.75 1.125 0.9407 0.580 2.0397 0.5215 1.4369 0.9679 3943.9586 +LPC 116.39 1.154 0.8720 0.608 1.7024 0.9323 3.2631 0.9600 3662.6571 +HPC 184.53 17.859 0.8514 0.971 2.2195 0.4206 0.2163 1.0137 6357.1603 +HPT 30.09 5.239 0.9345 105.115 5.2391 1.4085 0.4249 0.9803 1.5311 +LPT 153.19 3.411 0.9006 76.704 3.4107 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4776.00 7231.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 681.88 163.19 20.271 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 681.88 163.19 20.271 +Duct1 0.0025 0.2644 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 681.88 163.19 20.271 +Duct2 0.0025 0.3904 365.99 +Duct3 0.0050 0.3011 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2106 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.3554 909.75 218.67 61.395 +Duct5 0.0075 0.3848 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.7013 909.75 218.67 61.395 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 486.19 116.17 8.847 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.3325 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6398.7 6670.2 8126.5 +LP_Shaft 2157.5 15293.7 6282.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1580.66 0.9940 0.0550 0.60151 0.00982 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.300 0.9975 1.0000 0.9975 2706.36 0.624 648.0 9938.0 +Core_Nozz 1.107 0.9999 1.0000 0.9999 862.88 0.387 571.1 1205.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 210 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 12/ 22/ 1/10 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.400 20000.0 0.00 432.06 977.9 0.9931 971.15 8.2281 414.93 5.000 1234.8 1210.1 931.9 + core size:22.44 Q: 109.02 Maximum Thrust: 19557.8 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 432.06 7.541 461.71 110.31 0.0000 794.40 6.753 447.35 3680.0 0.4000 1.40126 +FS_2 Inlet.Fl_O 432.06 7.503 461.71 110.31 0.0000 798.40 7.223 456.69 5943.4 0.2340 1.40126 +FS_21 Fan.Fl_O 432.06 8.001 471.29 112.60 0.0000 756.53 7.523 463.05 4515.2 0.2978 1.40119 +FS_13 Splitter.Fl_O2 385.24 8.001 471.29 112.60 0.0000 674.55 7.458 461.91 3795.6 0.3182 1.40119 +FS_22 Splitter.Fl_O1 46.82 8.001 471.29 112.60 0.0000 81.98 7.788 467.67 719.5 0.1966 1.40119 +FS_23 Duct1.Fl_O 46.82 7.981 471.29 112.60 0.0000 82.19 7.768 467.67 721.3 0.1966 1.40119 +FS_24 LPC.Fl_O 46.82 9.796 506.13 120.95 0.0000 69.39 9.031 494.49 366.0 0.3427 1.40073 +FS_25 Duct2.Fl_O 46.82 9.771 506.13 120.95 0.0000 69.56 9.008 494.49 366.9 0.3427 1.40073 +FS_3 HPC.Fl_O 46.82 37.706 784.04 187.93 0.0000 22.44 34.843 766.76 119.9 0.3385 1.39272 +FS_36 Bld3.Fl_O 42.61 37.706 784.04 187.93 0.0000 20.42 34.843 766.76 109.1 0.3385 1.39272 +FS_4 Burner.Fl_O 42.88 35.632 1234.75 301.86 0.0063 27.28 35.405 1232.65 483.4 0.0971 1.36148 +FS_45 HPT.Fl_O 47.09 12.600 931.94 225.06 0.0058 73.62 11.845 916.19 439.1 0.3001 1.38103 +FS_48 Duct3.Fl_O 47.09 12.537 931.94 225.06 0.0058 73.99 11.786 916.19 441.4 0.3001 1.38103 +FS_5 LPT.Fl_O 47.09 7.122 813.04 195.71 0.0058 121.65 7.025 809.91 1477.4 0.1412 1.38765 +FS_7 Duct4.Fl_O 47.09 7.051 813.04 195.71 0.0058 122.88 6.999 811.34 2018.9 0.1038 1.38765 +FS_9 Core_Nozz.Fl_O 47.09 7.051 813.04 195.71 0.0058 122.88 6.753 803.29 863.0 0.2503 1.38765 +FS_15 BypBld.Fl_O 385.24 8.001 471.29 112.60 0.0000 674.55 7.458 461.91 3795.6 0.3182 1.40119 +FS_17 Duct5.Fl_O 385.24 7.941 471.29 112.60 0.0000 679.65 7.402 461.91 3824.3 0.3182 1.40119 +FS_19 Byp_Nozz.Fl_O 385.24 7.941 471.29 112.60 0.0000 679.65 6.753 449.93 2706.4 0.4864 1.40119 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 798.40 1.066 0.8930 1626.327 1.0208 0.8940 -1402.3 74.72 13.90 +LPC 82.19 1.227 0.8173 1609.709 1.0739 0.8226 -552.7 49.16 10.43 +HPC 69.56 3.859 0.8535 6021.683 1.5491 0.8781 -4437.5 49.88 50.87 +HPT 27.28 2.828 0.9180 169.283 1.2903 0.9065 4437.5 +LPT 73.99 1.760 0.8782 50.264 1.1462 0.8697 1955.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1530.83 1.046 0.9226 0.412 2.2178 0.5215 1.4369 0.9679 3943.9586 +LPC 88.16 1.070 0.8513 0.439 1.8944 0.9323 3.2631 0.9600 3662.6571 +HPC 165.37 14.216 0.8420 0.947 2.3845 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.302 0.9365 110.562 5.3025 1.4085 0.4249 0.9803 1.5311 +LPT 153.75 2.060 0.8771 61.969 2.0605 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3680.00 5572.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 603.82 144.39 13.864 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 603.82 144.39 13.864 +Duct1 0.0025 0.1966 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 603.82 144.39 13.864 +Duct2 0.0025 0.3427 365.99 +Duct3 0.0050 0.3001 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1412 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.6387 784.04 187.93 37.706 +Duct5 0.0075 0.3182 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.5751 784.04 187.93 37.706 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 471.29 112.60 8.001 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 8.2281 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 5948.4 3918.0 4437.5 +LP_Shaft 1534.4 6692.0 1955.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1234.75 0.9940 0.0550 0.26976 0.00633 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.176 0.9975 1.0000 0.9975 2706.36 0.486 504.7 6043.2 +Core_Nozz 1.044 0.9999 1.0000 0.9999 862.88 0.250 346.2 506.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 211 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 20000.0 0.00 954.80 19285.2 0.5307 10234.04 5.0411 518.66 22.706 2479.8 2416.8 1938.6 + core size:19.93 Q: 170.34 Maximum Thrust: 19285.2 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 954.80 8.012 469.79 112.24 0.0000 1666.72 6.753 447.35 6505.8 0.5000 1.40120 +FS_2 Inlet.Fl_O 954.80 7.972 469.79 112.24 0.0000 1675.11 6.364 440.44 5943.4 0.5763 1.40120 +FS_21 Fan.Fl_O 954.80 13.110 552.60 132.09 0.0000 1104.75 11.271 529.24 4515.2 0.4697 1.39985 +FS_13 Splitter.Fl_O2 796.75 13.110 552.60 132.09 0.0000 921.87 11.303 529.68 3795.6 0.4651 1.39985 +FS_22 Splitter.Fl_O1 158.05 13.110 552.60 132.09 0.0000 182.87 11.091 526.81 719.5 0.4947 1.39985 +FS_23 Duct1.Fl_O 158.05 13.077 552.60 132.09 0.0000 183.33 11.063 526.81 721.3 0.4947 1.39985 +FS_24 LPC.Fl_O 158.05 32.551 741.21 177.54 0.0000 85.30 28.483 713.71 366.0 0.4415 1.39461 +FS_25 Duct2.Fl_O 158.05 32.470 741.21 177.54 0.0000 85.52 28.412 713.71 366.9 0.4415 1.39461 +FS_3 HPC.Fl_O 158.05 181.924 1263.35 307.52 0.0000 19.93 171.227 1243.06 119.9 0.2991 1.36417 +FS_36 Bld3.Fl_O 143.83 181.924 1263.35 307.52 0.0000 18.13 171.227 1243.06 109.1 0.2991 1.36417 +FS_4 Burner.Fl_O 146.67 171.918 2479.76 656.16 0.0198 27.41 170.809 2476.05 483.4 0.0998 1.30073 +FS_45 HPT.Fl_O 160.89 64.461 1938.62 497.65 0.0180 70.92 60.890 1912.12 439.1 0.2950 1.31771 +FS_48 Duct3.Fl_O 160.89 64.139 1938.62 497.65 0.0180 71.27 60.585 1912.12 441.4 0.2950 1.31771 +FS_5 LPT.Fl_O 160.89 13.168 1349.53 335.22 0.0180 289.65 12.055 1319.17 1477.4 0.3638 1.34648 +FS_7 Duct4.Fl_O 160.89 13.036 1349.53 335.22 0.0180 292.58 12.463 1333.99 2018.9 0.2591 1.34648 +FS_9 Core_Nozz.Fl_O 160.89 13.036 1349.53 335.22 0.0180 292.58 6.972 1146.32 862.9 1.0000 1.34648 +FS_15 BypBld.Fl_O 796.75 13.110 552.60 132.09 0.0000 921.87 11.303 529.68 3795.6 0.4651 1.39985 +FS_17 Duct5.Fl_O 796.75 13.012 552.60 132.09 0.0000 928.84 11.219 529.68 3824.3 0.4651 1.39985 +FS_19 Byp_Nozz.Fl_O 796.75 13.012 552.60 132.09 0.0000 928.84 6.871 460.33 2706.3 1.0000 1.39985 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.645 0.8675 3944.235 1.1763 0.8765 -26813.3 24.71 17.45 +LPC 183.33 2.489 0.8683 3636.697 1.3413 0.8839 -10162.9 28.34 23.26 +HPC 85.52 5.603 0.8652 6324.485 1.7044 0.8922 -29066.1 20.16 20.21 +HPT 27.41 2.667 0.9134 151.826 1.2314 0.9036 29067.3 +LPT 71.27 4.871 0.9325 85.256 1.4365 0.9185 36975.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8962 1.000 2.3709 0.5215 1.4369 0.9679 3943.9586 +LPC 196.64 1.456 0.9044 0.993 1.7654 0.9323 3.2631 0.9600 3662.6571 +HPC 203.28 22.278 0.8535 0.995 2.0426 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.923 0.9318 99.160 4.9235 1.4085 0.4249 0.9803 1.5311 +LPT 148.08 6.400 0.9313 105.109 6.3999 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6505.80 15391.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 927.48 223.03 54.365 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 927.48 223.03 54.365 +Duct1 0.0025 0.4947 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 927.48 223.03 54.365 +Duct2 0.0025 0.4415 365.99 +Duct3 0.0050 0.2950 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3638 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.5318 1263.35 307.52 181.924 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.6928 1263.35 307.52 181.924 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 552.60 132.09 13.110 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0411 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7560.5 20192.4 29067.3 +LP_Shaft 3753.8 51735.0 36975.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2479.76 0.9940 0.0550 2.84279 0.01977 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.927 0.9975 1.0000 0.9975 2706.36 1.000 1049.6 26311.7 +Core_Nozz 1.930 0.9999 1.0000 0.9999 862.88 1.000 1635.1 8365.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 212 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 20000.0 0.00 929.10 17356.6 0.5186 9000.58 5.3172 518.66 20.713 2386.9 2326.6 1859.2 + core size:20.02 Q: 170.34 Maximum Thrust: 19285.2 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 929.10 8.012 469.79 112.24 0.0000 1621.86 6.753 447.35 6330.7 0.5000 1.40120 +FS_2 Inlet.Fl_O 929.10 7.972 469.79 112.24 0.0000 1630.03 6.479 442.69 5943.4 0.5523 1.40120 +FS_21 Fan.Fl_O 929.10 12.791 545.95 130.50 0.0000 1095.21 11.034 523.37 4515.2 0.4643 1.39999 +FS_13 Splitter.Fl_O2 782.03 12.791 545.95 130.50 0.0000 921.84 11.028 523.30 3795.6 0.4650 1.39999 +FS_22 Splitter.Fl_O1 147.08 12.791 545.95 130.50 0.0000 173.37 11.062 523.75 719.5 0.4602 1.39999 +FS_23 Duct1.Fl_O 147.08 12.759 545.95 130.50 0.0000 173.80 11.034 523.75 721.3 0.4602 1.39999 +FS_24 LPC.Fl_O 147.08 29.651 717.13 171.71 0.0000 85.72 25.903 690.17 366.0 0.4441 1.39544 +FS_25 Duct2.Fl_O 147.08 29.576 717.13 171.71 0.0000 85.93 25.839 690.17 366.9 0.4441 1.39544 +FS_3 HPC.Fl_O 147.08 165.961 1225.68 297.87 0.0000 20.02 156.105 1205.69 119.9 0.3004 1.36653 +FS_36 Bld3.Fl_O 133.84 165.961 1225.68 297.87 0.0000 18.22 156.105 1205.69 109.1 0.3004 1.36653 +FS_4 Burner.Fl_O 136.34 156.834 2386.94 627.90 0.0187 27.41 155.822 2383.34 483.4 0.0996 1.30364 +FS_45 HPT.Fl_O 149.58 58.197 1859.16 474.64 0.0170 71.51 54.914 1833.05 439.1 0.2973 1.32152 +FS_48 Duct3.Fl_O 149.58 57.906 1859.16 474.64 0.0170 71.87 54.640 1833.05 441.4 0.2973 1.32152 +FS_5 LPT.Fl_O 149.58 12.017 1296.06 320.75 0.0170 289.16 11.006 1266.79 1477.4 0.3625 1.35042 +FS_7 Duct4.Fl_O 149.58 11.897 1296.06 320.75 0.0170 292.08 11.376 1281.07 2018.9 0.2582 1.35042 +FS_9 Core_Nozz.Fl_O 149.58 11.897 1296.06 320.75 0.0170 292.08 6.753 1117.08 862.9 0.9466 1.35042 +FS_15 BypBld.Fl_O 782.03 12.791 545.95 130.50 0.0000 921.84 11.028 523.30 3795.6 0.4650 1.39999 +FS_17 Duct5.Fl_O 782.03 12.695 545.95 130.50 0.0000 928.81 10.946 523.30 3824.3 0.4650 1.39999 +FS_19 Byp_Nozz.Fl_O 782.03 12.695 545.95 130.50 0.0000 928.81 6.753 455.74 2706.3 0.9937 1.39999 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1630.03 1.604 0.8934 3732.994 1.1621 0.9003 -23993.7 28.43 17.78 +LPC 173.80 2.324 0.8659 3462.829 1.3135 0.8807 -8576.4 28.88 22.09 +HPC 85.93 5.611 0.8641 6335.033 1.7091 0.8914 -26252.3 20.56 20.59 +HPT 27.41 2.695 0.9140 152.470 1.2363 0.9041 26252.4 +LPT 71.87 4.819 0.9280 82.396 1.4345 0.9130 32567.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3125.27 1.421 0.9229 0.947 2.1685 0.5215 1.4369 0.9679 3943.9586 +LPC 186.43 1.406 0.9019 0.945 1.7506 0.9323 3.2631 0.9600 3662.6571 +HPC 204.28 22.317 0.8524 0.997 2.0720 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.989 0.9323 99.581 4.9891 1.4085 0.4249 0.9803 1.5311 +LPT 149.34 6.327 0.9268 101.584 6.3270 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6330.72 14977.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 898.34 215.87 49.557 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 898.34 215.87 49.557 +Duct1 0.0025 0.4602 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 898.34 215.87 49.557 +Duct2 0.0025 0.4441 365.99 +Duct3 0.0050 0.2973 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3625 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.1476 1225.68 297.87 165.961 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.0892 1225.68 297.87 165.961 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 545.95 130.50 12.791 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3172 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7449.1 18509.7 26252.4 +LP_Shaft 3552.7 48145.4 32567.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2386.94 0.9940 0.0550 2.50016 0.01868 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.880 0.9975 1.0000 0.9975 2706.36 0.994 1037.8 25224.2 +Core_Nozz 1.762 0.9999 1.0000 0.9999 862.88 0.947 1529.4 7110.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 213 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 20000.0 0.00 898.78 15428.2 0.5126 7908.71 5.5263 518.66 18.999 2294.0 2236.7 1782.0 + core size:20.17 Q: 170.34 Maximum Thrust: 19285.2 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 898.78 8.012 469.79 112.24 0.0000 1568.92 6.753 447.35 6124.1 0.5000 1.40120 +FS_2 Inlet.Fl_O 898.78 7.972 469.79 112.24 0.0000 1576.82 6.603 445.11 5943.4 0.5256 1.40120 +FS_21 Fan.Fl_O 898.78 12.388 539.67 128.99 0.0000 1087.61 10.714 517.73 4515.2 0.4600 1.40011 +FS_13 Splitter.Fl_O2 761.06 12.388 539.67 128.99 0.0000 920.96 10.685 517.32 3795.6 0.4644 1.40011 +FS_22 Splitter.Fl_O1 137.72 12.388 539.67 128.99 0.0000 166.65 10.864 519.79 719.5 0.4371 1.40011 +FS_23 Duct1.Fl_O 137.72 12.357 539.67 128.99 0.0000 167.07 10.836 519.79 721.3 0.4371 1.40011 +FS_24 LPC.Fl_O 137.72 27.684 701.26 167.87 0.0000 85.01 24.254 675.41 366.0 0.4393 1.39597 +FS_25 Duct2.Fl_O 137.72 27.615 701.26 167.87 0.0000 85.22 24.193 675.41 366.9 0.4393 1.39597 +FS_3 HPC.Fl_O 137.72 152.222 1193.37 289.62 0.0000 20.17 143.039 1173.51 119.9 0.3027 1.36856 +FS_36 Bld3.Fl_O 125.32 152.222 1193.37 289.62 0.0000 18.35 143.039 1173.51 109.1 0.3027 1.36856 +FS_4 Burner.Fl_O 127.52 143.850 2294.01 599.82 0.0175 27.40 142.923 2290.53 483.4 0.0995 1.30689 +FS_45 HPT.Fl_O 139.91 53.090 1782.02 452.50 0.0160 71.79 50.071 1756.56 439.1 0.2981 1.32550 +FS_48 Duct3.Fl_O 139.91 52.825 1782.02 452.50 0.0160 72.15 49.821 1756.56 441.4 0.2981 1.32550 +FS_5 LPT.Fl_O 139.91 11.128 1243.57 306.66 0.0160 286.10 10.214 1215.95 1477.4 0.3575 1.35441 +FS_7 Duct4.Fl_O 139.91 11.017 1243.57 306.66 0.0160 288.99 10.545 1229.40 2018.9 0.2549 1.35441 +FS_9 Core_Nozz.Fl_O 139.91 11.017 1243.57 306.66 0.0160 288.99 6.753 1092.75 862.9 0.8750 1.35441 +FS_15 BypBld.Fl_O 761.06 12.388 539.67 128.99 0.0000 920.96 10.685 517.32 3795.6 0.4644 1.40011 +FS_17 Duct5.Fl_O 761.06 12.295 539.67 128.99 0.0000 927.92 10.605 517.32 3824.3 0.4644 1.40011 +FS_19 Byp_Nozz.Fl_O 761.06 12.295 539.67 128.99 0.0000 927.92 6.753 454.63 2706.3 0.9658 1.40011 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1576.82 1.554 0.9036 3594.263 1.1487 0.9095 -21292.5 32.25 18.40 +LPC 167.07 2.240 0.8631 3353.503 1.2994 0.8777 -7576.5 28.28 20.53 +HPC 85.22 5.512 0.8646 6316.326 1.7017 0.8917 -23723.5 22.02 22.08 +HPT 27.40 2.710 0.9145 153.342 1.2403 0.9045 23723.4 +LPT 72.15 4.747 0.9264 81.032 1.4330 0.9110 28869.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3023.38 1.385 0.9335 0.911 2.0847 0.5215 1.4369 0.9679 3943.9586 +LPC 179.20 1.380 0.8991 0.916 1.7198 0.9323 3.2631 0.9600 3662.6571 +HPC 202.59 21.860 0.8530 0.994 2.0981 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.024 0.9328 100.150 5.0236 1.4085 0.4249 0.9803 1.5311 +LPT 149.92 6.227 0.9252 99.903 6.2269 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6124.08 14488.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 876.42 210.48 45.870 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 876.42 210.48 45.870 +Duct1 0.0025 0.4371 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 876.42 210.48 45.870 +Duct2 0.0025 0.4393 365.99 +Duct3 0.0050 0.2981 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3575 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.8201 1193.37 289.62 152.222 +Duct5 0.0075 0.4644 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.5744 1193.37 289.62 152.222 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 539.67 128.99 12.388 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5263 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7344.4 16965.0 23723.4 +LP_Shaft 3420.7 44325.5 28869.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2294.01 0.9940 0.0550 2.19686 0.01753 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.821 0.9975 1.0000 0.9975 2706.36 0.966 1007.5 23831.6 +Core_Nozz 1.631 0.9999 1.0000 0.9999 862.88 0.875 1399.4 6085.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 214 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 20000.0 0.00 827.34 11571.2 0.5132 5938.05 5.9999 518.66 15.606 2108.5 2056.9 1630.6 + core size:20.46 Q: 170.34 Maximum Thrust: 19285.2 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 827.34 8.012 469.79 112.24 0.0000 1444.22 6.753 447.35 5637.3 0.5000 1.40120 +FS_2 Inlet.Fl_O 827.34 7.972 469.79 112.24 0.0000 1451.49 6.859 449.98 5943.4 0.4683 1.40120 +FS_21 Fan.Fl_O 827.34 11.495 526.67 125.87 0.0000 1065.81 10.016 506.33 4515.2 0.4479 1.40037 +FS_13 Splitter.Fl_O2 709.15 11.495 526.67 125.87 0.0000 913.55 9.946 505.30 3795.6 0.4594 1.40037 +FS_22 Splitter.Fl_O1 118.19 11.495 526.67 125.87 0.0000 152.26 10.348 511.07 719.5 0.3905 1.40037 +FS_23 Duct1.Fl_O 118.19 11.467 526.67 125.87 0.0000 152.64 10.322 511.07 721.3 0.3905 1.40037 +FS_24 LPC.Fl_O 118.19 23.803 669.23 160.14 0.0000 82.89 21.023 646.01 366.0 0.4252 1.39710 +FS_25 Duct2.Fl_O 118.19 23.744 669.23 160.14 0.0000 83.10 20.971 646.01 366.9 0.4252 1.39710 +FS_3 HPC.Fl_O 118.19 125.037 1125.47 272.42 0.0000 20.46 117.255 1105.98 119.9 0.3071 1.37284 +FS_36 Bld3.Fl_O 107.56 125.037 1125.47 272.42 0.0000 18.62 117.255 1105.98 109.1 0.3071 1.37284 +FS_4 Burner.Fl_O 109.20 118.160 2108.46 544.64 0.0153 27.38 117.399 2105.21 483.4 0.0992 1.31362 +FS_45 HPT.Fl_O 119.84 43.283 1630.57 409.74 0.0140 72.15 40.796 1606.57 439.1 0.2988 1.33387 +FS_48 Duct3.Fl_O 119.84 43.066 1630.57 409.74 0.0140 72.51 40.592 1606.57 441.4 0.2988 1.33387 +FS_5 LPT.Fl_O 119.84 9.680 1150.07 281.87 0.0140 270.93 8.975 1127.18 1477.4 0.3346 1.36170 +FS_7 Duct4.Fl_O 119.84 9.583 1150.07 281.87 0.0140 273.66 9.217 1138.23 2018.9 0.2397 1.36170 +FS_9 Core_Nozz.Fl_O 119.84 9.583 1150.07 281.87 0.0140 273.66 6.753 1047.22 862.8 0.7327 1.36170 +FS_15 BypBld.Fl_O 709.15 11.495 526.67 125.87 0.0000 913.55 9.946 505.30 3795.6 0.4594 1.40037 +FS_17 Duct5.Fl_O 709.15 11.409 526.67 125.87 0.0000 920.45 9.871 505.30 3824.3 0.4594 1.40037 +FS_19 Byp_Nozz.Fl_O 709.15 11.409 526.67 125.87 0.0000 920.45 6.753 453.27 2706.4 0.8986 1.40037 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1451.49 1.442 0.9119 3305.362 1.1211 0.9164 -15952.4 40.37 19.48 +LPC 152.64 2.076 0.8558 3121.765 1.2707 0.8698 -5730.5 26.55 17.17 +HPC 83.10 5.266 0.8655 6269.347 1.6817 0.8922 -18775.6 25.36 25.49 +HPT 27.38 2.730 0.9148 155.090 1.2472 0.9045 18775.5 +LPT 72.51 4.449 0.9222 77.903 1.4178 0.9066 21682.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2783.05 1.308 0.9421 0.838 2.0158 0.5215 1.4369 0.9679 3943.9586 +LPC 163.73 1.330 0.8914 0.852 1.6502 0.9323 3.2631 0.9600 3662.6571 +HPC 197.55 20.721 0.8539 0.986 2.1329 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.072 0.9332 101.292 5.0716 1.4085 0.4249 0.9803 1.5311 +LPT 150.67 5.811 0.9210 96.045 5.8113 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5637.32 13337.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 831.26 199.44 38.583 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 831.26 199.44 38.583 +Duct1 0.0025 0.3905 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 831.26 199.44 38.583 +Duct2 0.0025 0.4252 365.99 +Duct3 0.0050 0.2988 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3346 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.1367 1125.47 272.42 125.037 +Duct5 0.0075 0.4594 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.5006 1125.47 272.42 125.037 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 526.67 125.87 11.495 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9999 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7121.4 13847.2 18775.5 +LP_Shaft 3145.8 36200.7 21682.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2108.46 0.9940 0.0550 1.64946 0.01534 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.689 0.9975 1.0000 0.9975 2706.36 0.899 936.0 20629.2 +Core_Nozz 1.419 0.9999 1.0000 0.9999 862.88 0.733 1148.9 4279.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 215 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 20000.0 0.00 740.07 7714.2 0.5329 4111.02 6.6316 518.66 12.116 1894.6 1849.6 1455.7 + core size:20.83 Q: 170.34 Maximum Thrust: 19285.2 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 740.07 8.012 469.79 112.24 0.0000 1291.89 6.753 447.35 5042.7 0.5000 1.40120 +FS_2 Inlet.Fl_O 740.07 7.972 469.79 112.24 0.0000 1298.39 7.116 454.75 5943.4 0.4059 1.40120 +FS_21 Fan.Fl_O 740.07 10.522 512.33 122.43 0.0000 1027.32 9.280 494.25 4515.2 0.4272 1.40063 +FS_13 Splitter.Fl_O2 643.10 10.522 512.33 122.43 0.0000 892.70 9.180 492.71 3795.6 0.4457 1.40063 +FS_22 Splitter.Fl_O1 96.98 10.522 512.33 122.43 0.0000 134.61 9.724 500.89 719.5 0.3375 1.40063 +FS_23 Duct1.Fl_O 96.98 10.496 512.33 122.43 0.0000 134.95 9.699 500.89 721.3 0.3375 1.40063 +FS_24 LPC.Fl_O 96.98 19.454 628.82 150.40 0.0000 80.66 17.322 608.35 366.0 0.4108 1.39845 +FS_25 Duct2.Fl_O 96.98 19.406 628.82 150.40 0.0000 80.86 17.279 608.35 366.9 0.4108 1.39845 +FS_3 HPC.Fl_O 96.98 97.077 1044.26 252.02 0.0000 20.83 90.801 1025.27 119.9 0.3127 1.37795 +FS_36 Bld3.Fl_O 88.25 97.077 1044.26 252.02 0.0000 18.96 90.801 1025.27 109.1 0.3127 1.37795 +FS_4 Burner.Fl_O 89.39 91.738 1894.61 482.52 0.0129 27.37 91.148 1891.63 483.4 0.0988 1.32286 +FS_45 HPT.Fl_O 98.12 33.222 1455.72 361.58 0.0118 72.71 31.283 1433.43 439.1 0.3002 1.34442 +FS_48 Duct3.Fl_O 98.12 33.056 1455.72 361.58 0.0118 73.08 31.126 1433.43 441.4 0.3002 1.34442 +FS_5 LPT.Fl_O 98.12 8.550 1055.11 257.08 0.0118 240.52 8.070 1038.75 1477.4 0.2918 1.36924 +FS_7 Duct4.Fl_O 98.12 8.465 1055.11 257.08 0.0118 242.95 8.213 1046.53 2018.9 0.2106 1.36924 +FS_9 Core_Nozz.Fl_O 98.12 8.465 1055.11 257.08 0.0118 242.95 6.753 992.42 862.8 0.5829 1.36924 +FS_15 BypBld.Fl_O 643.10 10.522 512.33 122.43 0.0000 892.70 9.180 492.71 3795.6 0.4457 1.40063 +FS_17 Duct5.Fl_O 643.10 10.443 512.33 122.43 0.0000 899.45 9.111 492.71 3824.3 0.4457 1.40063 +FS_19 Byp_Nozz.Fl_O 643.10 10.443 512.33 122.43 0.0000 899.45 6.753 452.23 2706.4 0.8140 1.40063 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1298.39 1.320 0.9129 2925.788 1.0905 0.9163 -10669.2 46.36 20.14 +LPC 134.95 1.854 0.8476 2801.691 1.2274 0.8602 -3838.0 26.32 14.35 +HPC 80.86 5.003 0.8647 6227.989 1.6607 0.8910 -13942.0 29.40 29.59 +HPT 27.37 2.761 0.9153 157.545 1.2573 0.9046 13942.0 +LPT 73.08 3.866 0.9193 72.981 1.3797 0.9047 14507.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2489.49 1.223 0.9431 0.742 2.0234 0.5215 1.4369 0.9679 3943.9586 +LPC 144.75 1.262 0.8829 0.765 1.6135 0.9323 3.2631 0.9600 3662.6571 +HPC 192.24 19.503 0.8531 0.980 2.1718 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.145 0.9337 102.896 5.1455 1.4085 0.4249 0.9803 1.5311 +LPT 151.85 4.998 0.9181 89.976 4.9980 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5042.70 11930.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 775.96 185.97 30.785 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 775.96 185.97 30.785 +Duct1 0.0025 0.3375 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 775.96 185.97 30.785 +Duct2 0.0025 0.4108 365.99 +Duct3 0.0050 0.3002 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2918 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.3941 1044.26 252.02 97.077 +Duct5 0.0075 0.4457 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.3336 1044.26 252.02 97.077 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 512.33 122.43 10.522 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6316 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6857.5 10678.1 13942.0 +LP_Shaft 2784.5 27363.2 14507.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1894.61 0.9940 0.0550 1.14195 0.01294 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.546 0.9975 1.0000 0.9975 2706.36 0.814 846.8 16926.3 +Core_Nozz 1.253 0.9999 1.0000 0.9999 862.88 0.583 891.4 2718.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 216 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 20000.0 0.00 627.39 3857.1 0.6228 2402.34 7.5935 518.66 8.414 1618.1 1581.6 1233.0 + core size:21.38 Q: 170.34 Maximum Thrust: 19285.2 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 627.39 8.012 469.79 112.24 0.0000 1095.18 6.753 447.35 4274.9 0.5000 1.40120 +FS_2 Inlet.Fl_O 627.39 7.972 469.79 112.24 0.0000 1100.70 7.381 459.53 5943.4 0.3335 1.40120 +FS_21 Fan.Fl_O 627.39 9.449 495.69 118.45 0.0000 953.94 8.509 481.05 4515.2 0.3897 1.40088 +FS_13 Splitter.Fl_O2 554.38 9.449 495.69 118.45 0.0000 842.93 8.395 479.20 3795.6 0.4143 1.40088 +FS_22 Splitter.Fl_O1 73.01 9.449 495.69 118.45 0.0000 111.01 8.976 488.46 719.5 0.2718 1.40088 +FS_23 Duct1.Fl_O 73.01 9.425 495.69 118.45 0.0000 111.28 8.953 488.46 721.3 0.2718 1.40088 +FS_24 LPC.Fl_O 73.01 14.691 575.82 137.67 0.0000 76.95 13.246 559.04 366.0 0.3876 1.39943 +FS_25 Duct2.Fl_O 73.01 14.655 575.82 137.67 0.0000 77.14 13.212 559.04 366.9 0.3876 1.39943 +FS_3 HPC.Fl_O 73.01 67.414 935.64 225.04 0.0000 21.38 62.806 917.40 119.9 0.3212 1.38468 +FS_36 Bld3.Fl_O 66.44 67.414 935.64 225.04 0.0000 19.45 62.806 917.40 109.1 0.3212 1.38468 +FS_4 Burner.Fl_O 67.10 63.706 1618.13 404.74 0.0100 27.34 63.298 1615.50 483.4 0.0982 1.33717 +FS_45 HPT.Fl_O 73.67 22.774 1232.97 302.13 0.0091 73.30 21.422 1213.15 439.1 0.3011 1.35965 +FS_48 Duct3.Fl_O 73.67 22.660 1232.97 302.13 0.0091 73.67 21.315 1213.15 441.4 0.3011 1.35965 +FS_5 LPT.Fl_O 73.67 7.691 950.57 230.25 0.0091 190.58 7.426 941.48 1477.4 0.2260 1.37765 +FS_7 Duct4.Fl_O 73.67 7.614 950.57 230.25 0.0091 192.51 7.473 945.73 2018.9 0.1647 1.37765 +FS_9 Core_Nozz.Fl_O 73.67 7.614 950.57 230.25 0.0091 192.51 6.753 919.78 862.8 0.4204 1.37765 +FS_15 BypBld.Fl_O 554.38 9.449 495.69 118.45 0.0000 842.93 8.395 479.20 3795.6 0.4143 1.40088 +FS_17 Duct5.Fl_O 554.38 9.378 495.69 118.45 0.0000 849.30 8.332 479.20 3824.3 0.4143 1.40088 +FS_19 Byp_Nozz.Fl_O 554.38 9.378 495.69 118.45 0.0000 849.30 6.753 451.22 2706.4 0.7009 1.40088 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1100.70 1.185 0.9039 2382.350 1.0551 0.9062 -5507.0 54.74 19.89 +LPC 111.28 1.559 0.8371 2319.262 1.1616 0.8470 -1985.2 30.88 11.65 +HPC 77.14 4.600 0.8629 6161.493 1.6249 0.8883 -9025.7 35.92 36.32 +HPT 27.34 2.797 0.9162 161.391 1.2710 0.9051 9025.7 +LPT 73.67 2.946 0.9064 64.571 1.2971 0.8929 7492.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2110.44 1.129 0.9338 0.604 2.1428 0.5215 1.4369 0.9679 3943.9586 +LPC 119.37 1.171 0.8719 0.633 1.6462 0.9323 3.2631 0.9600 3662.6571 +HPC 183.40 17.643 0.8513 0.969 2.2259 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.230 0.9346 105.407 5.2302 1.4085 0.4249 0.9803 1.5311 +LPT 153.08 3.715 0.9052 79.607 3.7151 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4274.90 10113.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 702.82 168.25 22.384 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 702.82 168.25 22.384 +Duct1 0.0025 0.2718 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 702.82 168.25 22.384 +Duct2 0.0025 0.3876 365.99 +Duct3 0.0050 0.3011 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2260 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.5553 935.64 225.04 67.414 +Duct5 0.0075 0.4143 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.0154 935.64 225.04 67.414 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 495.69 118.45 9.449 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.5935 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6492.1 7301.8 9025.7 +LP_Shaft 2267.3 17355.4 7492.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1618.13 0.9940 0.0550 0.66732 0.01004 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.389 0.9975 1.0000 0.9975 2706.36 0.701 728.4 12550.5 +Core_Nozz 1.127 0.9999 1.0000 0.9999 862.88 0.420 620.4 1420.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 217 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 11/ 31/ 2/ 8 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 20000.0 0.00 509.68 964.3 1.1617 1120.14 8.9328 518.66 5.258 1282.8 1257.1 969.8 + core size:22.39 Q: 170.34 Maximum Thrust: 19285.2 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 509.68 8.012 469.79 112.24 0.0000 889.71 6.753 447.35 3472.9 0.5000 1.40120 +FS_2 Inlet.Fl_O 509.68 7.972 469.79 112.24 0.0000 894.19 7.594 463.29 5943.4 0.2644 1.40120 +FS_21 Fan.Fl_O 509.68 8.541 480.73 114.86 0.0000 844.25 7.894 470.00 4515.2 0.3372 1.40108 +FS_13 Splitter.Fl_O2 458.37 8.541 480.73 114.86 0.0000 759.26 7.790 468.22 3795.6 0.3649 1.40108 +FS_22 Splitter.Fl_O1 51.31 8.541 480.73 114.86 0.0000 85.00 8.296 476.74 719.5 0.2042 1.40108 +FS_23 Duct1.Fl_O 51.31 8.520 480.73 114.86 0.0000 85.21 8.276 476.74 721.3 0.2042 1.40108 +FS_24 LPC.Fl_O 51.31 10.876 523.15 125.03 0.0000 69.64 10.019 511.02 366.0 0.3442 1.40044 +FS_25 Duct2.Fl_O 51.31 10.848 523.15 125.03 0.0000 69.81 9.994 511.02 366.9 0.3442 1.40044 +FS_3 HPC.Fl_O 51.31 42.131 811.37 194.59 0.0000 22.39 38.947 793.62 119.9 0.3378 1.39140 +FS_36 Bld3.Fl_O 46.69 42.131 811.37 194.59 0.0000 20.37 38.947 793.62 109.1 0.3378 1.39140 +FS_4 Burner.Fl_O 47.01 39.814 1282.83 314.40 0.0067 27.29 39.560 1280.66 483.4 0.0972 1.35823 +FS_45 HPT.Fl_O 51.62 14.101 969.81 234.54 0.0061 73.57 13.258 953.52 439.1 0.3002 1.37847 +FS_48 Duct3.Fl_O 51.62 14.030 969.81 234.54 0.0061 73.94 13.191 953.52 441.4 0.3002 1.37847 +FS_5 LPT.Fl_O 51.62 7.188 824.55 198.58 0.0061 133.07 7.070 820.75 1477.4 0.1548 1.38689 +FS_7 Duct4.Fl_O 51.62 7.117 824.55 198.58 0.0061 134.41 7.053 822.50 2018.9 0.1137 1.38689 +FS_9 Core_Nozz.Fl_O 51.62 7.117 824.55 198.58 0.0061 134.41 6.753 812.57 862.9 0.2761 1.38689 +FS_15 BypBld.Fl_O 458.37 8.541 480.73 114.86 0.0000 759.26 7.790 468.22 3795.6 0.3649 1.40108 +FS_17 Duct5.Fl_O 458.37 8.477 480.73 114.86 0.0000 765.00 7.732 468.22 3824.3 0.3649 1.40108 +FS_19 Byp_Nozz.Fl_O 458.37 8.477 480.73 114.86 0.0000 765.00 6.753 450.43 2706.4 0.5790 1.40108 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 894.19 1.071 0.8564 1740.462 1.0233 0.8579 -1888.5 81.90 17.92 +LPC 85.21 1.276 0.8198 1720.548 1.0882 0.8260 -737.9 42.76 9.97 +HPC 69.81 3.884 0.8542 6026.294 1.5509 0.8788 -5050.1 49.30 50.28 +HPT 27.29 2.824 0.9179 168.979 1.2879 0.9065 5050.1 +LPT 73.94 1.952 0.8864 53.190 1.1762 0.8768 2626.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1714.48 1.050 0.8848 0.441 2.4225 0.5215 1.4369 0.9679 3943.9586 +LPC 91.39 1.085 0.8539 0.470 1.7943 0.9323 3.2631 0.9600 3662.6571 +HPC 165.97 14.331 0.8427 0.948 2.3800 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.292 0.9364 110.363 5.2920 1.4085 0.4249 0.9803 1.5311 +LPT 153.64 2.328 0.8853 65.576 2.3276 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3472.86 8216.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 624.53 149.37 15.431 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 624.53 149.37 15.431 +Duct1 0.0025 0.2042 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 624.53 149.37 15.431 +Duct2 0.0025 0.3442 365.99 +Duct3 0.0050 0.3002 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1548 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.7959 811.37 194.59 42.131 +Duct5 0.0075 0.3649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.8222 811.37 194.59 42.131 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 480.73 114.86 8.541 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 8.9328 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6052.2 4382.4 5050.1 +LP_Shaft 1656.4 8328.2 2626.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1282.83 0.9940 0.0550 0.31115 0.00666 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.255 0.9975 1.0000 0.9975 2706.36 0.579 601.2 8564.5 +Core_Nozz 1.054 0.9999 1.0000 0.9999 862.88 0.276 384.0 616.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 218 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 4/ 14/ 1/ 2 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 20000.0 0.00 1016.12 19469.4 0.5732 11159.83 5.0407 622.40 22.702 2527.7 2463.5 1977.8 + core size:19.92 Q: 245.29 Maximum Thrust: 19469.4 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1016.12 8.616 479.66 114.61 0.0000 1666.72 6.753 447.35 5769.7 0.6000 1.40110 +FS_2 Inlet.Fl_O 1016.12 8.573 479.66 114.61 0.0000 1675.11 6.843 449.69 5943.4 0.5763 1.40110 +FS_21 Fan.Fl_O 1016.12 14.097 564.19 134.87 0.0000 1104.76 12.119 540.34 4515.2 0.4697 1.39964 +FS_13 Splitter.Fl_O2 847.91 14.097 564.19 134.87 0.0000 921.88 12.155 540.79 3795.6 0.4651 1.39964 +FS_22 Splitter.Fl_O1 168.21 14.097 564.19 134.87 0.0000 182.89 11.925 537.86 719.5 0.4948 1.39964 +FS_23 Duct1.Fl_O 168.21 14.062 564.19 134.87 0.0000 183.34 11.896 537.86 721.3 0.4948 1.39964 +FS_24 LPC.Fl_O 168.21 34.998 756.56 181.26 0.0000 85.31 30.624 728.51 366.0 0.4416 1.39399 +FS_25 Duct2.Fl_O 168.21 34.911 756.56 181.26 0.0000 85.52 30.548 728.51 366.9 0.4416 1.39399 +FS_3 HPC.Fl_O 168.21 195.601 1288.03 313.86 0.0000 19.92 184.113 1267.42 119.9 0.2991 1.36263 +FS_36 Bld3.Fl_O 153.07 195.601 1288.03 313.86 0.0000 18.12 184.113 1267.42 109.1 0.2991 1.36263 +FS_4 Burner.Fl_O 156.17 184.843 2527.67 670.79 0.0203 27.41 183.651 2523.91 483.4 0.0998 1.29933 +FS_45 HPT.Fl_O 171.31 69.338 1977.75 509.04 0.0184 70.90 65.497 1950.85 439.1 0.2952 1.31596 +FS_48 Duct3.Fl_O 171.31 68.991 1977.75 509.04 0.0184 71.26 65.170 1950.85 441.4 0.2952 1.31596 +FS_5 LPT.Fl_O 171.31 14.181 1379.26 343.29 0.0184 289.51 12.984 1348.40 1477.4 0.3639 1.34440 +FS_7 Duct4.Fl_O 171.31 14.039 1379.26 343.29 0.0184 292.43 13.422 1363.46 2018.9 0.2591 1.34440 +FS_9 Core_Nozz.Fl_O 171.31 14.039 1379.26 343.29 0.0184 292.43 7.514 1172.59 862.9 1.0000 1.34440 +FS_15 BypBld.Fl_O 847.91 14.097 564.19 134.87 0.0000 921.88 12.155 540.79 3795.6 0.4651 1.39964 +FS_17 Duct5.Fl_O 847.91 13.992 564.19 134.87 0.0000 928.84 12.063 540.79 3824.3 0.4651 1.39964 +FS_19 Byp_Nozz.Fl_O 847.91 13.992 564.19 134.87 0.0000 928.84 7.389 470.01 2706.4 1.0000 1.39964 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.644 0.8675 3944.235 1.1762 0.8765 -29134.9 24.72 17.46 +LPC 183.34 2.489 0.8683 3636.786 1.3410 0.8838 -11039.8 28.36 23.27 +HPC 85.52 5.603 0.8652 6324.804 1.7025 0.8922 -31559.3 20.18 20.23 +HPT 27.41 2.666 0.9135 151.937 1.2304 0.9037 31559.2 +LPT 71.26 4.865 0.9327 85.290 1.4339 0.9187 40174.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.448 0.8962 1.000 2.3712 0.5215 1.4369 0.9679 3943.9586 +LPC 196.66 1.456 0.9045 0.993 1.7659 0.9323 3.2631 0.9600 3662.6571 +HPC 203.31 22.278 0.8535 0.995 2.0438 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.921 0.9319 99.232 4.9207 1.4085 0.4249 0.9803 1.5311 +LPT 148.07 6.392 0.9315 105.152 6.3917 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5769.69 19656.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 946.28 227.67 58.452 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 946.28 227.67 58.452 +Duct1 0.0025 0.4948 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 946.28 227.67 58.452 +Duct2 0.0025 0.4416 365.99 +Duct3 0.0050 0.2952 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3639 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.8874 1288.03 313.86 195.601 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.2516 1288.03 313.86 195.601 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 564.19 134.87 14.097 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0407 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7638.8 21698.9 31559.2 +LP_Shaft 3793.0 55629.0 40174.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2527.67 0.9940 0.0550 3.09995 0.02025 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.072 0.9976 1.0000 0.9975 2706.36 1.000 1060.6 29670.6 +Core_Nozz 2.079 0.9998 1.0000 0.9999 862.88 1.000 1652.6 9455.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 219 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 20000.0 0.00 989.87 17521.9 0.5617 9842.27 5.3117 622.40 20.755 2434.9 2373.5 1898.5 + core size:20.01 Q: 245.29 Maximum Thrust: 19469.4 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 989.87 8.616 479.66 114.61 0.0000 1623.66 6.753 447.35 5620.6 0.6000 1.40110 +FS_2 Inlet.Fl_O 989.87 8.573 479.66 114.61 0.0000 1631.84 6.962 451.91 5943.4 0.5532 1.40110 +FS_21 Fan.Fl_O 989.87 13.769 557.64 133.30 0.0000 1095.45 11.877 534.57 4515.2 0.4644 1.39976 +FS_13 Splitter.Fl_O2 833.04 13.769 557.64 133.30 0.0000 921.89 11.872 534.51 3795.6 0.4651 1.39976 +FS_22 Splitter.Fl_O1 156.83 13.769 557.64 133.30 0.0000 173.56 11.903 534.91 719.5 0.4609 1.39976 +FS_23 Duct1.Fl_O 156.83 13.735 557.64 133.30 0.0000 173.99 11.873 534.91 721.3 0.4609 1.39976 +FS_24 LPC.Fl_O 156.83 31.992 732.89 175.52 0.0000 85.64 27.958 705.43 366.0 0.4437 1.39491 +FS_25 Duct2.Fl_O 156.83 31.912 732.89 175.52 0.0000 85.85 27.888 705.43 366.9 0.4437 1.39491 +FS_3 HPC.Fl_O 156.83 178.826 1250.57 304.24 0.0000 20.01 168.213 1230.25 119.9 0.3005 1.36497 +FS_36 Bld3.Fl_O 142.72 178.826 1250.57 304.24 0.0000 18.21 168.213 1230.25 109.1 0.3005 1.36497 +FS_4 Burner.Fl_O 145.45 168.990 2434.90 642.40 0.0192 27.41 167.901 2431.24 483.4 0.0997 1.30215 +FS_45 HPT.Fl_O 159.57 62.757 1898.52 485.98 0.0174 71.49 59.220 1871.99 439.1 0.2974 1.31964 +FS_48 Duct3.Fl_O 159.57 62.443 1898.52 485.98 0.0174 71.85 58.924 1871.99 441.4 0.2974 1.31964 +FS_5 LPT.Fl_O 159.57 12.935 1324.98 328.53 0.0174 289.76 11.841 1295.03 1477.4 0.3637 1.34834 +FS_7 Duct4.Fl_O 159.57 12.805 1324.98 328.53 0.0174 292.69 12.242 1309.65 2018.9 0.2590 1.34834 +FS_9 Core_Nozz.Fl_O 159.57 12.805 1324.98 328.53 0.0174 292.69 6.844 1124.60 862.9 1.0000 1.34834 +FS_15 BypBld.Fl_O 833.04 13.769 557.64 133.30 0.0000 921.89 11.872 534.51 3795.6 0.4651 1.39976 +FS_17 Duct5.Fl_O 833.04 13.666 557.64 133.30 0.0000 928.86 11.783 534.51 3824.3 0.4651 1.39976 +FS_19 Byp_Nozz.Fl_O 833.04 13.666 557.64 133.30 0.0000 928.86 7.217 464.54 2706.4 1.0000 1.39976 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1631.84 1.606 0.8929 3738.526 1.1626 0.8998 -26179.7 28.30 17.75 +LPC 173.99 2.329 0.8659 3467.302 1.3143 0.8807 -9369.3 28.78 22.05 +HPC 85.85 5.604 0.8642 6332.857 1.7063 0.8914 -28561.0 20.63 20.67 +HPT 27.41 2.693 0.9140 152.558 1.2351 0.9042 28561.3 +LPT 71.85 4.828 0.9281 82.512 1.4329 0.9132 35546.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3128.59 1.422 0.9224 0.948 2.1722 0.5215 1.4369 0.9679 3943.9586 +LPC 186.63 1.407 0.9019 0.947 1.7489 0.9323 3.2631 0.9600 3662.6571 +HPC 204.09 22.282 0.8526 0.996 2.0717 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.984 0.9324 99.638 4.9841 1.4085 0.4249 0.9803 1.5311 +LPT 149.29 6.339 0.9269 101.726 6.3394 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5620.65 19148.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 917.50 220.57 53.435 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 917.50 220.57 53.435 +Duct1 0.0025 0.4609 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 917.50 220.57 53.435 +Duct2 0.0025 0.4437 365.99 +Duct3 0.0050 0.2974 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3637 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.4891 1250.57 304.24 178.826 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.6257 1250.57 304.24 178.826 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 557.64 133.30 13.769 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3117 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7527.9 19926.9 28561.3 +LP_Shaft 3595.2 51928.6 35546.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2434.90 0.9940 0.0550 2.73396 0.01916 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.024 0.9976 1.0000 0.9975 2706.36 1.000 1054.4 28554.7 +Core_Nozz 1.896 0.9999 1.0000 0.9999 862.88 1.000 1620.6 8115.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 220 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 20000.0 0.00 959.97 15575.6 0.5565 8667.32 5.5206 622.40 19.088 2340.9 2282.4 1820.7 + core size:20.17 Q: 245.29 Maximum Thrust: 19469.4 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 959.97 8.616 479.66 114.61 0.0000 1574.61 6.753 447.35 5450.8 0.6000 1.40110 +FS_2 Inlet.Fl_O 959.97 8.573 479.66 114.61 0.0000 1582.54 7.087 454.22 5943.4 0.5284 1.40110 +FS_21 Fan.Fl_O 959.97 13.361 551.57 131.84 0.0000 1088.87 11.551 529.10 4515.2 0.4607 1.39988 +FS_13 Splitter.Fl_O2 812.74 13.361 551.57 131.84 0.0000 921.88 11.520 528.69 3795.6 0.4651 1.39988 +FS_22 Splitter.Fl_O1 147.22 13.361 551.57 131.84 0.0000 166.99 11.709 531.16 719.5 0.4382 1.39988 +FS_23 Duct1.Fl_O 147.22 13.327 551.57 131.84 0.0000 167.41 11.680 531.16 721.3 0.4382 1.39988 +FS_24 LPC.Fl_O 147.22 30.022 717.89 171.89 0.0000 84.79 26.324 691.63 366.0 0.4379 1.39542 +FS_25 Duct2.Fl_O 147.22 29.947 717.89 171.89 0.0000 85.00 26.258 691.63 366.9 0.4379 1.39542 +FS_3 HPC.Fl_O 147.22 164.461 1218.73 296.09 0.0000 20.17 154.540 1198.52 119.9 0.3028 1.36697 +FS_36 Bld3.Fl_O 133.97 164.461 1218.73 296.09 0.0000 18.35 154.540 1198.52 109.1 0.3028 1.36697 +FS_4 Burner.Fl_O 136.38 155.415 2340.87 613.84 0.0180 27.40 154.414 2337.33 483.4 0.0995 1.30532 +FS_45 HPT.Fl_O 149.63 57.426 1820.67 463.50 0.0164 71.74 54.165 1794.80 439.1 0.2981 1.32356 +FS_48 Duct3.Fl_O 149.63 57.139 1820.67 463.50 0.0164 72.10 53.894 1794.80 441.4 0.2981 1.32356 +FS_5 LPT.Fl_O 149.63 11.900 1269.26 313.51 0.0164 289.06 10.900 1240.50 1477.4 0.3621 1.35252 +FS_7 Duct4.Fl_O 149.63 11.781 1269.26 313.51 0.0164 291.98 11.266 1254.53 2018.9 0.2579 1.35252 +FS_9 Core_Nozz.Fl_O 149.63 11.781 1269.26 313.51 0.0164 291.98 6.753 1096.12 862.9 0.9374 1.35252 +FS_15 BypBld.Fl_O 812.74 13.361 551.57 131.84 0.0000 921.88 11.520 528.69 3795.6 0.4651 1.39988 +FS_17 Duct5.Fl_O 812.74 13.261 551.57 131.84 0.0000 928.84 11.433 528.69 3824.3 0.4651 1.39988 +FS_19 Byp_Nozz.Fl_O 812.74 13.261 551.57 131.84 0.0000 928.84 7.002 459.47 2706.4 1.0000 1.39988 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1582.54 1.559 0.9027 3606.689 1.1499 0.9087 -23411.6 31.91 18.38 +LPC 167.41 2.253 0.8629 3363.371 1.3015 0.8776 -8342.3 27.99 20.39 +HPC 85.00 5.492 0.8649 6311.016 1.6977 0.8918 -25870.2 22.22 22.31 +HPT 27.40 2.706 0.9145 153.460 1.2388 0.9046 25870.0 +LPT 72.10 4.801 0.9262 81.286 1.4344 0.9108 31754.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3034.31 1.389 0.9326 0.914 2.0936 0.5215 1.4369 0.9679 3943.9586 +LPC 179.57 1.384 0.8989 0.918 1.7139 0.9323 3.2631 0.9600 3662.6571 +HPC 202.07 21.765 0.8532 0.993 2.0973 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.016 0.9329 100.228 5.0161 1.4085 0.4249 0.9803 1.5311 +LPT 149.82 6.303 0.9250 100.215 6.3029 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5450.84 18570.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 896.30 215.36 49.653 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 896.30 215.36 49.653 +Duct1 0.0025 0.4382 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 896.30 215.36 49.653 +Duct2 0.0025 0.4379 365.99 +Duct3 0.0050 0.2981 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3621 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.1527 1218.73 296.09 164.461 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.0972 1218.73 296.09 164.461 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 551.57 131.84 13.361 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5206 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7424.8 18299.8 25870.0 +LP_Shaft 3468.4 48084.2 31754.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2340.87 0.9940 0.0550 2.40759 0.01797 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.964 0.9976 1.0000 0.9975 2706.36 1.000 1048.6 27164.2 +Core_Nozz 1.745 0.9999 1.0000 0.9999 862.88 0.937 1501.2 6981.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 221 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 20000.0 0.00 891.30 11681.3 0.5592 6532.28 6.0107 622.40 15.776 2151.8 2099.4 1666.5 + core size:20.49 Q: 245.29 Maximum Thrust: 19469.4 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 891.30 8.616 479.66 114.61 0.0000 1461.98 6.753 447.35 5060.9 0.6000 1.40110 +FS_2 Inlet.Fl_O 891.30 8.573 479.66 114.61 0.0000 1469.34 7.339 458.80 5943.4 0.4761 1.40110 +FS_21 Fan.Fl_O 891.30 12.425 538.65 128.74 0.0000 1074.34 10.795 517.43 4515.2 0.4526 1.40014 +FS_13 Splitter.Fl_O2 764.16 12.425 538.65 128.74 0.0000 921.09 10.716 516.35 3795.6 0.4645 1.40014 +FS_22 Splitter.Fl_O1 127.13 12.425 538.65 128.74 0.0000 153.24 11.166 522.45 719.5 0.3936 1.40014 +FS_23 Duct1.Fl_O 127.13 12.394 538.65 128.74 0.0000 153.63 11.138 522.45 721.3 0.3936 1.40014 +FS_24 LPC.Fl_O 127.13 26.108 687.72 164.60 0.0000 82.40 23.100 664.22 366.0 0.4222 1.39643 +FS_25 Duct2.Fl_O 127.13 26.043 687.72 164.60 0.0000 82.61 23.042 664.22 366.9 0.4222 1.39643 +FS_3 HPC.Fl_O 127.13 135.921 1152.03 279.13 0.0000 20.49 127.441 1132.09 119.9 0.3077 1.37116 +FS_36 Bld3.Fl_O 115.69 135.921 1152.03 279.13 0.0000 18.64 127.441 1132.09 109.1 0.3077 1.37116 +FS_4 Burner.Fl_O 117.51 128.446 2151.83 557.33 0.0157 27.38 127.619 2148.53 483.4 0.0992 1.31206 +FS_45 HPT.Fl_O 128.95 47.135 1666.46 419.72 0.0143 72.06 44.434 1642.10 439.1 0.2986 1.33193 +FS_48 Duct3.Fl_O 128.95 46.899 1666.46 419.72 0.0143 72.43 44.211 1642.10 441.4 0.2986 1.33193 +FS_5 LPT.Fl_O 128.95 10.207 1168.34 286.66 0.0143 278.64 9.417 1143.62 1477.4 0.3459 1.36032 +FS_7 Duct4.Fl_O 128.95 10.105 1168.34 286.66 0.0143 281.46 9.696 1155.60 2018.9 0.2472 1.36032 +FS_9 Core_Nozz.Fl_O 128.95 10.105 1168.34 286.66 0.0143 281.46 6.753 1049.08 862.9 0.7890 1.36032 +FS_15 BypBld.Fl_O 764.16 12.425 538.65 128.74 0.0000 921.09 10.716 516.35 3795.6 0.4645 1.40014 +FS_17 Duct5.Fl_O 764.16 12.332 538.65 128.74 0.0000 928.05 10.636 516.35 3824.3 0.4645 1.40014 +FS_19 Byp_Nozz.Fl_O 764.16 12.332 538.65 128.74 0.0000 928.05 6.753 453.39 2706.3 0.9685 1.40014 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1469.34 1.449 0.9107 3339.159 1.1230 0.9154 -17828.4 40.29 19.87 +LPC 153.63 2.107 0.8550 3151.007 1.2767 0.8694 -6449.8 25.80 16.87 +HPC 82.61 5.219 0.8658 6259.768 1.6751 0.8921 -20601.2 25.89 26.04 +HPT 27.38 2.725 0.9148 155.387 1.2457 0.9046 20601.8 +LPT 72.43 4.595 0.9220 78.661 1.4264 0.9060 24276.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2817.07 1.313 0.9409 0.847 2.0400 0.5215 1.4369 0.9679 3943.9586 +LPC 164.78 1.339 0.8906 0.860 1.6348 0.9323 3.2631 0.9600 3662.6571 +HPC 196.38 20.505 0.8541 0.985 2.1328 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.060 0.9332 101.486 5.0601 1.4085 0.4249 0.9803 1.5311 +LPT 150.49 6.015 0.9208 96.980 6.0146 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5060.94 17241.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 852.74 204.69 42.140 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 852.74 204.69 42.140 +Duct1 0.0025 0.3936 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 852.74 204.69 42.140 +Duct2 0.0025 0.4222 365.99 +Duct3 0.0050 0.2986 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3459 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.4497 1152.03 279.13 135.921 +Duct5 0.0075 0.4645 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.9924 1152.03 279.13 135.921 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 538.65 128.74 12.425 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.0107 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7208.1 15011.4 20601.8 +LP_Shaft 3211.1 39706.7 24276.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2151.83 0.9940 0.0550 1.81452 0.01568 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.826 0.9975 1.0000 0.9975 2706.36 0.968 1008.8 23960.8 +Core_Nozz 1.496 0.9999 1.0000 0.9999 862.88 0.789 1238.2 4962.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 222 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 20000.0 0.00 807.72 7787.8 0.5847 4553.34 6.6962 622.40 12.335 1937.2 1891.5 1491.2 + core size:20.86 Q: 245.29 Maximum Thrust: 19469.4 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 807.72 8.616 479.66 114.61 0.0000 1324.89 6.753 447.35 4586.4 0.6000 1.40110 +FS_2 Inlet.Fl_O 807.72 8.573 479.66 114.61 0.0000 1331.56 7.597 463.35 5943.4 0.4189 1.40110 +FS_21 Fan.Fl_O 807.72 11.385 524.19 125.28 0.0000 1048.16 9.977 504.77 4515.2 0.4383 1.40042 +FS_13 Splitter.Fl_O2 702.77 11.385 524.19 125.28 0.0000 911.97 9.856 503.02 3795.6 0.4584 1.40042 +FS_22 Splitter.Fl_O1 104.95 11.385 524.19 125.28 0.0000 136.19 10.499 512.19 719.5 0.3421 1.40042 +FS_23 Duct1.Fl_O 104.95 11.357 524.19 125.28 0.0000 136.53 10.473 512.19 721.3 0.3421 1.40042 +FS_24 LPC.Fl_O 104.95 21.571 648.67 155.18 0.0000 79.96 19.253 628.01 366.0 0.4064 1.39786 +FS_25 Duct2.Fl_O 104.95 21.517 648.67 155.18 0.0000 80.16 19.205 628.01 366.9 0.4064 1.39786 +FS_3 HPC.Fl_O 104.95 106.280 1071.91 258.94 0.0000 20.86 99.385 1052.41 119.9 0.3135 1.37621 +FS_36 Bld3.Fl_O 95.50 106.280 1071.91 258.94 0.0000 18.98 99.385 1052.41 109.1 0.3135 1.37621 +FS_4 Burner.Fl_O 96.77 100.435 1937.24 494.68 0.0132 27.37 99.789 1934.20 483.4 0.0988 1.32100 +FS_45 HPT.Fl_O 106.22 36.474 1491.20 371.19 0.0121 72.56 34.353 1468.56 439.1 0.2997 1.34229 +FS_48 Duct3.Fl_O 106.22 36.291 1491.20 371.19 0.0121 72.93 34.182 1468.56 441.4 0.2997 1.34229 +FS_5 LPT.Fl_O 106.22 8.882 1068.33 260.50 0.0121 252.22 8.329 1049.98 1477.4 0.3078 1.36821 +FS_7 Duct4.Fl_O 106.22 8.793 1068.33 260.50 0.0121 254.77 8.504 1058.75 2018.9 0.2216 1.36821 +FS_9 Core_Nozz.Fl_O 106.22 8.793 1068.33 260.50 0.0121 254.77 6.753 994.65 862.9 0.6317 1.36821 +FS_15 BypBld.Fl_O 702.77 11.385 524.19 125.28 0.0000 911.97 9.856 503.02 3795.6 0.4584 1.40042 +FS_17 Duct5.Fl_O 702.77 11.300 524.19 125.28 0.0000 918.86 9.783 503.02 3824.3 0.4584 1.40042 +FS_19 Byp_Nozz.Fl_O 702.77 11.300 524.19 125.28 0.0000 918.86 6.753 452.38 2706.4 0.8897 1.40042 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1331.56 1.328 0.9108 2982.725 1.0928 0.9144 -12193.8 47.55 21.19 +LPC 136.53 1.899 0.8462 2853.214 1.2375 0.8593 -4440.9 24.76 13.84 +HPC 80.16 4.939 0.8648 6216.336 1.6525 0.8908 -15406.6 30.16 30.37 +HPT 27.37 2.754 0.9154 157.947 1.2552 0.9049 15406.6 +LPT 72.93 4.086 0.9189 74.279 1.3958 0.9037 16634.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2553.09 1.228 0.9410 0.756 2.0667 0.5215 1.4369 0.9679 3943.9586 +LPC 146.45 1.276 0.8814 0.779 1.5832 0.9323 3.2631 0.9600 3662.6571 +HPC 190.58 19.211 0.8531 0.978 2.1695 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.127 0.9337 103.158 5.1273 1.4085 0.4249 0.9803 1.5311 +LPT 151.54 5.305 0.9178 91.577 5.3049 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4586.39 15625.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 798.70 191.50 33.935 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 798.70 191.50 33.935 +Duct1 0.0025 0.3421 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 798.70 191.50 33.935 +Duct2 0.0025 0.4064 365.99 +Duct3 0.0050 0.2997 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3078 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.6733 1071.91 258.94 106.280 +Duct5 0.0075 0.4584 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.7723 1071.91 258.94 106.280 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 524.19 125.28 11.385 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6962 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6951.9 11639.6 15406.6 +LP_Shaft 2868.4 30459.0 16634.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1937.24 0.9940 0.0550 1.26482 0.01324 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.673 0.9975 1.0000 0.9975 2706.36 0.890 925.7 20220.5 +Core_Nozz 1.302 0.9999 1.0000 0.9999 862.88 0.632 967.1 3192.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 223 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 20000.0 0.00 700.53 3893.8 0.6918 2693.84 7.7696 622.40 8.676 1660.4 1623.2 1267.9 + core size:21.42 Q: 245.29 Maximum Thrust: 19469.4 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 700.53 8.616 479.66 114.61 0.0000 1149.06 6.753 447.35 3977.7 0.6000 1.40110 +FS_2 Inlet.Fl_O 700.53 8.573 479.66 114.61 0.0000 1154.85 7.866 467.99 5943.4 0.3526 1.40110 +FS_21 Fan.Fl_O 700.53 10.223 507.34 121.24 0.0000 995.97 9.101 490.73 4515.2 0.4109 1.40071 +FS_13 Splitter.Fl_O2 620.65 10.223 507.34 121.24 0.0000 882.40 8.954 488.46 3795.6 0.4391 1.40071 +FS_22 Splitter.Fl_O1 79.88 10.223 507.34 121.24 0.0000 113.57 9.686 499.56 719.5 0.2787 1.40071 +FS_23 Duct1.Fl_O 79.88 10.198 507.34 121.24 0.0000 113.86 9.661 499.56 721.3 0.2787 1.40071 +FS_24 LPC.Fl_O 79.88 16.529 597.23 142.81 0.0000 76.21 14.938 580.23 366.0 0.3831 1.39909 +FS_25 Duct2.Fl_O 79.88 16.488 597.23 142.81 0.0000 76.40 14.901 580.23 366.9 0.3831 1.39909 +FS_3 HPC.Fl_O 79.88 74.748 965.10 232.33 0.0000 21.42 69.614 946.25 119.9 0.3222 1.38287 +FS_36 Bld3.Fl_O 72.69 74.748 965.10 232.33 0.0000 19.50 69.614 946.25 109.1 0.3222 1.38287 +FS_4 Burner.Fl_O 73.44 70.637 1660.41 416.37 0.0103 27.34 70.184 1657.73 483.4 0.0982 1.33495 +FS_45 HPT.Fl_O 80.63 25.332 1267.93 311.27 0.0094 73.13 23.836 1247.74 439.1 0.3006 1.35729 +FS_48 Duct3.Fl_O 80.63 25.206 1267.93 311.27 0.0094 73.50 23.717 1247.74 441.4 0.3006 1.35729 +FS_5 LPT.Fl_O 80.63 7.874 958.57 232.29 0.0094 204.59 7.559 947.93 1477.4 0.2439 1.37699 +FS_7 Duct4.Fl_O 80.63 7.795 958.57 232.29 0.0094 206.66 7.628 952.92 2018.9 0.1773 1.37699 +FS_9 Core_Nozz.Fl_O 80.63 7.795 958.57 232.29 0.0094 206.66 6.753 921.58 863.0 0.4605 1.37699 +FS_15 BypBld.Fl_O 620.65 10.223 507.34 121.24 0.0000 882.40 8.954 488.46 3795.6 0.4391 1.40071 +FS_17 Duct5.Fl_O 620.65 10.146 507.34 121.24 0.0000 889.06 8.887 488.46 3824.3 0.4391 1.40071 +FS_19 Byp_Nozz.Fl_O 620.65 10.146 507.34 121.24 0.0000 889.06 6.753 451.53 2706.4 0.7850 1.40071 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1154.85 1.193 0.8954 2478.246 1.0577 0.8980 -6571.9 56.91 22.13 +LPC 113.86 1.621 0.8354 2409.691 1.1772 0.8462 -2438.0 27.48 10.96 +HPC 76.40 4.533 0.8629 6147.398 1.6160 0.8881 -10117.4 36.86 37.33 +HPT 27.34 2.788 0.9162 161.886 1.2686 0.9053 10117.4 +LPT 73.50 3.201 0.9086 66.930 1.3227 0.8943 9010.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2214.26 1.134 0.9251 0.628 2.2130 0.5215 1.4369 0.9679 3943.9586 +LPC 122.13 1.190 0.8701 0.658 1.5867 0.9323 3.2631 0.9600 3662.6571 +HPC 181.63 17.335 0.8513 0.967 2.2330 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.209 0.9346 105.731 5.2092 1.4085 0.4249 0.9803 1.5311 +LPT 152.73 4.071 0.9074 82.516 4.0708 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3977.71 13551.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 727.18 174.14 25.023 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 727.18 174.14 25.023 +Duct1 0.0025 0.2787 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 727.18 174.14 25.023 +Duct2 0.0025 0.3831 365.99 +Duct3 0.0050 0.3006 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2439 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.7959 965.10 232.33 74.748 +Duct5 0.0075 0.4391 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.3935 965.10 232.33 74.748 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 507.34 121.24 10.223 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.7696 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6596.5 8055.4 10117.4 +LP_Shaft 2383.2 19855.9 9010.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1660.41 0.9940 0.0550 0.74829 0.01029 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.502 0.9975 1.0000 0.9975 2706.36 0.785 816.0 15740.9 +Core_Nozz 1.154 0.9999 1.0000 0.9999 862.88 0.460 680.1 1704.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:50 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 224 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 11/ 21/ 1/ 9 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 20000.0 0.00 590.86 973.5 1.3355 1300.10 9.3831 622.40 5.530 1333.2 1306.5 1009.8 + core size:22.38 Q: 245.29 Maximum Thrust: 19469.4 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 590.86 8.616 479.66 114.61 0.0000 969.18 6.753 447.35 3355.0 0.6000 1.40110 +FS_2 Inlet.Fl_O 590.86 8.573 479.66 114.61 0.0000 974.06 8.084 471.67 5943.4 0.2905 1.40110 +FS_21 Fan.Fl_O 590.86 9.236 492.31 117.64 0.0000 916.00 8.397 479.08 4515.2 0.3711 1.40093 +FS_13 Splitter.Fl_O2 533.96 9.236 492.31 117.64 0.0000 827.78 8.248 476.62 3795.6 0.4051 1.40093 +FS_22 Splitter.Fl_O1 56.91 9.236 492.31 117.64 0.0000 88.22 8.950 487.90 719.5 0.2124 1.40093 +FS_23 Duct1.Fl_O 56.91 9.212 492.31 117.64 0.0000 88.44 8.927 487.90 721.3 0.2124 1.40093 +FS_24 LPC.Fl_O 56.91 12.313 544.14 130.06 0.0000 69.57 11.346 531.56 366.0 0.3438 1.40002 +FS_25 Duct2.Fl_O 56.91 12.282 544.14 130.06 0.0000 69.74 11.317 531.56 366.9 0.3438 1.40002 +FS_3 HPC.Fl_O 56.91 47.648 843.07 202.32 0.0000 22.38 44.050 824.69 119.9 0.3379 1.38991 +FS_36 Bld3.Fl_O 51.78 47.648 843.07 202.32 0.0000 20.36 44.050 824.69 109.1 0.3379 1.38991 +FS_4 Burner.Fl_O 52.15 45.027 1333.20 327.63 0.0070 27.29 44.740 1330.96 483.4 0.0973 1.35491 +FS_45 HPT.Fl_O 57.27 15.974 1009.84 244.61 0.0063 73.51 15.021 992.99 439.1 0.3002 1.37575 +FS_48 Duct3.Fl_O 57.27 15.895 1009.84 244.61 0.0063 73.88 14.946 992.99 441.4 0.3002 1.37575 +FS_5 LPT.Fl_O 57.27 7.279 834.30 201.01 0.0063 146.63 7.133 829.61 1477.4 0.1712 1.38624 +FS_7 Duct4.Fl_O 57.27 7.206 834.30 201.01 0.0063 148.11 7.128 831.77 2018.9 0.1255 1.38624 +FS_9 Core_Nozz.Fl_O 57.27 7.206 834.30 201.01 0.0063 148.11 6.753 819.32 862.7 0.3076 1.38624 +FS_15 BypBld.Fl_O 533.96 9.236 492.31 117.64 0.0000 827.78 8.248 476.62 3795.6 0.4051 1.40093 +FS_17 Duct5.Fl_O 533.96 9.166 492.31 117.64 0.0000 834.04 8.186 476.62 3824.3 0.4051 1.40093 +FS_19 Byp_Nozz.Fl_O 533.96 9.166 492.31 117.64 0.0000 834.04 6.753 451.08 2706.4 0.6750 1.40093 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 974.06 1.077 0.8168 1867.881 1.0264 0.8188 -2532.4 83.96 21.56 +LPC 88.44 1.337 0.8219 1843.730 1.1053 0.8291 -1000.2 36.28 9.30 +HPC 69.74 3.879 0.8542 6025.013 1.5494 0.8787 -5818.2 49.33 50.32 +HPT 27.29 2.819 0.9179 169.012 1.2853 0.9066 5818.2 +LPT 73.88 2.184 0.8966 56.526 1.2104 0.8861 3532.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1867.62 1.054 0.8439 0.474 2.5525 0.5215 1.4369 0.9679 3943.9586 +LPC 94.87 1.103 0.8561 0.503 1.6897 0.9323 3.2631 0.9600 3662.6571 +HPC 165.80 14.311 0.8427 0.948 2.3796 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.281 0.9363 110.385 5.2805 1.4085 0.4249 0.9803 1.5311 +LPT 153.52 2.651 0.8954 69.689 2.6510 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3355.01 11430.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 649.37 155.35 17.463 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 649.37 155.35 17.463 +Duct1 0.0025 0.2124 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 649.37 155.35 17.463 +Duct2 0.0025 0.3438 365.99 +Duct3 0.0050 0.3002 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1712 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.9917 843.07 202.32 47.648 +Duct5 0.0075 0.4051 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.1298 843.07 202.32 47.648 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 492.31 117.64 9.236 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.3831 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6171.1 4951.7 5818.2 +LP_Shaft 1796.3 10328.5 3532.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1333.20 0.9940 0.0550 0.36114 0.00697 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.357 0.9975 1.0000 0.9975 2706.36 0.675 701.3 11638.9 +Core_Nozz 1.067 0.9999 1.0000 0.9999 862.88 0.308 429.6 764.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 225 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 4/ 14/ 1/ 2 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 20000.0 0.00 1091.91 20045.5 0.6154 12336.68 5.0400 726.13 22.697 2584.2 2518.7 2023.9 + core size:19.90 Q: 333.87 Maximum Thrust: 20045.5 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1091.91 9.370 491.33 117.40 0.0000 1666.72 6.753 447.35 5314.3 0.7000 1.40095 +FS_2 Inlet.Fl_O 1091.91 9.324 491.33 117.40 0.0000 1675.11 7.443 460.63 5943.4 0.5763 1.40095 +FS_21 Fan.Fl_O 1091.91 15.331 577.87 138.16 0.0000 1104.78 13.180 553.46 4515.2 0.4698 1.39940 +FS_13 Splitter.Fl_O2 911.13 15.331 577.87 138.16 0.0000 921.87 13.218 553.92 3795.6 0.4652 1.39940 +FS_22 Splitter.Fl_O1 180.78 15.331 577.87 138.16 0.0000 182.91 12.968 550.90 719.5 0.4949 1.39940 +FS_23 Duct1.Fl_O 180.78 15.293 577.87 138.16 0.0000 183.37 12.936 550.90 721.3 0.4949 1.39940 +FS_24 LPC.Fl_O 180.78 38.056 774.65 185.65 0.0000 85.32 33.298 745.96 366.0 0.4418 1.39317 +FS_25 Duct2.Fl_O 180.78 37.961 774.65 185.65 0.0000 85.53 33.214 745.96 366.9 0.4418 1.39317 +FS_3 HPC.Fl_O 180.78 212.684 1317.01 321.34 0.0000 19.90 200.205 1296.04 119.9 0.2991 1.36085 +FS_36 Bld3.Fl_O 164.51 212.684 1317.01 321.34 0.0000 18.11 200.205 1296.04 109.1 0.2991 1.36085 +FS_4 Burner.Fl_O 167.94 200.986 2584.16 688.11 0.0208 27.41 199.690 2580.33 483.4 0.0999 1.29767 +FS_45 HPT.Fl_O 184.21 75.431 2023.92 522.55 0.0190 70.89 71.254 1996.52 439.1 0.2954 1.31396 +FS_48 Duct3.Fl_O 184.21 75.054 2023.92 522.55 0.0190 71.25 70.898 1996.52 441.4 0.2954 1.31396 +FS_5 LPT.Fl_O 184.21 15.450 1414.44 352.89 0.0190 289.35 14.148 1382.99 1477.4 0.3640 1.34197 +FS_7 Duct4.Fl_O 184.21 15.296 1414.44 352.89 0.0190 292.27 14.624 1398.35 2018.9 0.2592 1.34197 +FS_9 Core_Nozz.Fl_O 184.21 15.296 1414.44 352.89 0.0190 292.27 8.193 1203.73 862.9 1.0000 1.34197 +FS_15 BypBld.Fl_O 911.13 15.331 577.87 138.16 0.0000 921.87 13.218 553.92 3795.6 0.4652 1.39940 +FS_17 Duct5.Fl_O 911.13 15.216 577.87 138.16 0.0000 928.84 13.119 553.92 3824.3 0.4652 1.39940 +FS_19 Byp_Nozz.Fl_O 911.13 15.216 577.87 138.16 0.0000 928.84 8.036 481.45 2706.4 1.0000 1.39940 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.644 0.8675 3944.235 1.1762 0.8765 -32069.3 24.72 17.46 +LPC 183.37 2.488 0.8683 3636.895 1.3405 0.8839 -12147.5 28.38 23.30 +HPC 85.53 5.603 0.8651 6325.047 1.7001 0.8921 -34707.0 20.19 20.25 +HPT 27.41 2.664 0.9136 152.059 1.2292 0.9039 34706.8 +LPT 71.25 4.858 0.9328 85.331 1.4309 0.9189 44216.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.448 0.8962 1.000 2.3715 0.5215 1.4369 0.9679 3943.9586 +LPC 196.69 1.456 0.9045 0.993 1.7666 0.9323 3.2631 0.9600 3662.6571 +HPC 203.34 22.277 0.8535 0.995 2.0448 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.918 0.9319 99.312 4.9176 1.4085 0.4249 0.9803 1.5311 +LPT 148.05 6.382 0.9316 105.202 6.3816 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5314.31 24643.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 968.40 233.14 63.558 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 968.40 233.14 63.558 +Duct1 0.0025 0.4949 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 968.40 233.14 63.558 +Duct2 0.0025 0.4418 365.99 +Duct3 0.0050 0.2954 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3640 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 6.3273 1317.01 321.34 212.684 +Duct5 0.0075 0.4652 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.9428 1317.01 321.34 212.684 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 577.87 138.16 15.331 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0400 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7729.9 23581.8 34706.8 +LP_Shaft 3838.9 60494.8 44216.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2584.16 0.9940 0.0550 3.42686 0.02083 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.253 0.9972 1.0000 0.9975 2706.36 1.000 1073.4 33868.4 +Core_Nozz 2.265 0.9993 1.0000 0.9999 862.88 1.000 1672.9 10820.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 226 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 20000.0 0.00 1064.17 18040.6 0.6042 10899.75 5.3080 726.13 20.776 2490.9 2428.2 1944.3 + core size:20.00 Q: 333.87 Maximum Thrust: 20045.5 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1064.17 9.370 491.33 117.40 0.0000 1624.38 6.753 447.35 5179.3 0.7000 1.40095 +FS_2 Inlet.Fl_O 1064.17 9.324 491.33 117.40 0.0000 1632.56 7.570 462.87 5943.4 0.5536 1.40095 +FS_21 Fan.Fl_O 1064.17 14.981 571.27 136.57 0.0000 1095.55 12.922 547.64 4515.2 0.4645 1.39951 +FS_13 Splitter.Fl_O2 895.47 14.981 571.27 136.57 0.0000 921.87 12.917 547.58 3795.6 0.4652 1.39951 +FS_22 Splitter.Fl_O1 168.70 14.981 571.27 136.57 0.0000 173.68 12.947 547.95 719.5 0.4613 1.39951 +FS_23 Duct1.Fl_O 168.70 14.944 571.27 136.57 0.0000 174.11 12.915 547.95 721.3 0.4613 1.39951 +FS_24 LPC.Fl_O 168.70 34.832 750.79 179.86 0.0000 85.63 30.439 722.68 366.0 0.4438 1.39423 +FS_25 Duct2.Fl_O 168.70 34.745 750.79 179.86 0.0000 85.85 30.363 722.68 366.9 0.4438 1.39423 +FS_3 HPC.Fl_O 168.70 194.679 1279.34 311.63 0.0000 20.00 183.140 1258.66 119.9 0.3005 1.36317 +FS_36 Bld3.Fl_O 153.52 194.679 1279.34 311.63 0.0000 18.20 183.140 1258.66 109.1 0.3005 1.36317 +FS_4 Burner.Fl_O 156.55 183.972 2490.94 659.44 0.0197 27.40 182.786 2487.22 483.4 0.0998 1.30051 +FS_45 HPT.Fl_O 171.73 68.363 1944.31 499.24 0.0179 71.48 64.511 1917.29 439.1 0.2976 1.31753 +FS_48 Duct3.Fl_O 171.73 68.021 1944.31 499.24 0.0179 71.83 64.188 1917.29 441.4 0.2976 1.31753 +FS_5 LPT.Fl_O 171.73 14.110 1359.74 337.93 0.0179 289.61 12.918 1329.20 1477.4 0.3639 1.34589 +FS_7 Duct4.Fl_O 171.73 13.969 1359.74 337.93 0.0179 292.53 13.355 1344.11 2018.9 0.2591 1.34589 +FS_9 Core_Nozz.Fl_O 171.73 13.969 1359.74 337.93 0.0179 292.53 7.472 1155.28 862.9 1.0000 1.34589 +FS_15 BypBld.Fl_O 895.47 14.981 571.27 136.57 0.0000 921.87 12.917 547.58 3795.6 0.4652 1.39951 +FS_17 Duct5.Fl_O 895.47 14.869 571.27 136.57 0.0000 928.84 12.820 547.58 3824.3 0.4652 1.39951 +FS_19 Byp_Nozz.Fl_O 895.47 14.869 571.27 136.57 0.0000 928.84 7.853 475.93 2706.4 1.0000 1.39951 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1632.56 1.607 0.8926 3740.887 1.1627 0.8996 -28865.0 28.25 17.75 +LPC 174.11 2.331 0.8659 3469.286 1.3143 0.8807 -10332.5 28.79 22.08 +HPC 85.85 5.603 0.8642 6332.789 1.7040 0.8914 -31451.4 20.65 20.68 +HPT 27.40 2.691 0.9141 152.661 1.2338 0.9042 31451.7 +LPT 71.83 4.821 0.9283 82.572 1.4299 0.9136 39195.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3130.02 1.422 0.9222 0.949 2.1741 0.5215 1.4369 0.9679 3943.9586 +LPC 186.76 1.408 0.9020 0.947 1.7494 0.9323 3.2631 0.9600 3662.6571 +HPC 204.09 22.279 0.8526 0.996 2.0721 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.980 0.9324 99.705 4.9802 1.4085 0.4249 0.9803 1.5311 +LPT 149.26 6.330 0.9271 101.801 6.3300 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5179.31 24017.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 939.43 225.98 58.176 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 939.43 225.98 58.176 +Duct1 0.0025 0.4613 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 939.43 225.98 58.176 +Duct2 0.0025 0.4438 365.99 +Duct3 0.0050 0.2976 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3639 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.9045 1279.34 311.63 194.679 +Duct5 0.0075 0.4652 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 9.2786 1279.34 311.63 194.679 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 571.27 136.57 14.981 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3080 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7619.2 21680.5 31451.7 +LP_Shaft 3640.9 56539.5 39195.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2490.94 0.9940 0.0550 3.02771 0.01972 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.202 0.9974 1.0000 0.9975 2706.36 1.000 1067.2 32677.5 +Core_Nozz 2.068 0.9998 1.0000 0.9999 862.88 1.000 1641.2 9380.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 227 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 20000.0 0.00 1032.95 16036.5 0.5993 9610.96 5.5160 726.13 19.129 2395.6 2335.9 1865.6 + core size:20.16 Q: 333.87 Maximum Thrust: 20045.5 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 1032.95 9.370 491.33 117.40 0.0000 1576.72 6.753 447.35 5027.3 0.7000 1.40095 +FS_2 Inlet.Fl_O 1032.95 9.324 491.33 117.40 0.0000 1584.65 7.702 465.17 5943.4 0.5294 1.40095 +FS_21 Fan.Fl_O 1032.95 14.552 565.24 135.12 0.0000 1089.00 12.580 542.21 4515.2 0.4608 1.39962 +FS_13 Splitter.Fl_O2 874.42 14.552 565.24 135.12 0.0000 921.87 12.546 541.80 3795.6 0.4651 1.39962 +FS_22 Splitter.Fl_O1 158.53 14.552 565.24 135.12 0.0000 167.13 12.749 544.29 719.5 0.4388 1.39962 +FS_23 Duct1.Fl_O 158.53 14.515 565.24 135.12 0.0000 167.55 12.717 544.29 721.3 0.4388 1.39962 +FS_24 LPC.Fl_O 158.53 32.769 736.06 176.29 0.0000 84.69 28.743 709.23 366.0 0.4374 1.39480 +FS_25 Duct2.Fl_O 158.53 32.687 736.06 176.29 0.0000 84.91 28.671 709.23 366.9 0.4374 1.39480 +FS_3 HPC.Fl_O 158.53 179.247 1247.31 303.40 0.0000 20.16 168.446 1226.72 119.9 0.3028 1.36517 +FS_36 Bld3.Fl_O 144.26 179.247 1247.31 303.40 0.0000 18.34 168.446 1226.72 109.1 0.3028 1.36517 +FS_4 Burner.Fl_O 146.93 169.388 2395.60 630.32 0.0185 27.40 168.297 2391.99 483.4 0.0996 1.30354 +FS_45 HPT.Fl_O 161.20 62.642 1865.59 476.37 0.0168 71.72 59.087 1839.23 439.1 0.2983 1.32136 +FS_48 Duct3.Fl_O 161.20 62.329 1865.59 476.37 0.0168 72.08 58.792 1839.23 441.4 0.2983 1.32136 +FS_5 LPT.Fl_O 161.20 12.948 1302.14 322.31 0.0168 289.88 11.853 1272.58 1477.4 0.3636 1.35014 +FS_7 Duct4.Fl_O 161.20 12.819 1302.14 322.31 0.0168 292.81 12.254 1287.01 2018.9 0.2589 1.35014 +FS_9 Core_Nozz.Fl_O 161.20 12.819 1302.14 322.31 0.0168 292.81 6.848 1104.40 862.9 1.0000 1.35014 +FS_15 BypBld.Fl_O 874.42 14.552 565.24 135.12 0.0000 921.87 12.546 541.80 3795.6 0.4651 1.39962 +FS_17 Duct5.Fl_O 874.42 14.443 565.24 135.12 0.0000 928.84 12.452 541.80 3824.3 0.4651 1.39962 +FS_19 Byp_Nozz.Fl_O 874.42 14.443 565.24 135.12 0.0000 928.84 7.627 470.89 2706.4 1.0000 1.39962 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1584.65 1.561 0.9025 3611.757 1.1504 0.9084 -25902.9 31.74 18.34 +LPC 167.55 2.258 0.8629 3367.344 1.3022 0.8775 -9233.1 27.88 20.34 +HPC 84.91 5.484 0.8650 6308.850 1.6946 0.8918 -28510.0 22.29 22.38 +HPT 27.40 2.704 0.9145 153.551 1.2373 0.9047 28509.9 +LPT 72.08 4.814 0.9262 81.386 1.4327 0.9109 35136.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3038.39 1.390 0.9323 0.916 2.0955 0.5215 1.4369 0.9679 3943.9586 +LPC 179.72 1.385 0.8988 0.919 1.7116 0.9323 3.2631 0.9600 3662.6571 +HPC 201.85 21.728 0.8534 0.992 2.0966 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.011 0.9329 100.287 5.0107 1.4085 0.4249 0.9803 1.5311 +LPT 149.78 6.320 0.9250 100.339 6.3199 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5027.34 23312.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 918.34 220.78 54.158 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 918.34 220.78 54.158 +Duct1 0.0025 0.4388 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 918.34 220.78 54.158 +Duct2 0.0025 0.4374 365.99 +Duct3 0.0050 0.2983 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.5484 1247.31 303.40 179.247 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.7189 1247.31 303.40 179.247 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 565.24 135.12 14.552 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5160 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7515.5 19923.6 28509.9 +LP_Shaft 3515.3 52496.8 35136.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2395.60 0.9940 0.0550 2.66971 0.01851 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.139 0.9975 1.0000 0.9975 2706.36 1.000 1061.6 31215.9 +Core_Nozz 1.898 0.9999 1.0000 0.9999 862.88 1.000 1607.0 8132.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 228 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 20000.0 0.00 963.30 12027.2 0.6035 7257.99 5.9974 726.13 15.893 2201.1 2147.7 1707.0 + core size:20.50 Q: 333.87 Maximum Thrust: 20045.5 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 963.30 9.370 491.33 117.40 0.0000 1470.40 6.753 447.35 4688.4 0.7000 1.40095 +FS_2 Inlet.Fl_O 963.30 9.324 491.33 117.40 0.0000 1477.81 7.963 469.64 5943.4 0.4798 1.40095 +FS_21 Fan.Fl_O 963.30 13.586 552.68 132.11 0.0000 1075.59 11.799 530.85 4515.2 0.4533 1.39985 +FS_13 Splitter.Fl_O2 825.63 13.586 552.68 132.11 0.0000 921.88 11.714 529.76 3795.6 0.4651 1.39985 +FS_22 Splitter.Fl_O1 137.66 13.586 552.68 132.11 0.0000 153.71 12.200 535.95 719.5 0.3951 1.39985 +FS_23 Duct1.Fl_O 137.66 13.552 552.68 132.11 0.0000 154.10 12.170 535.95 721.3 0.3951 1.39985 +FS_24 LPC.Fl_O 137.66 28.810 707.71 169.43 0.0000 82.03 25.526 683.82 366.0 0.4199 1.39575 +FS_25 Duct2.Fl_O 137.66 28.738 707.71 169.43 0.0000 82.23 25.462 683.82 366.9 0.4199 1.39575 +FS_3 HPC.Fl_O 137.66 148.928 1181.42 286.59 0.0000 20.50 139.620 1161.01 119.9 0.3082 1.36931 +FS_36 Bld3.Fl_O 125.27 148.928 1181.42 286.59 0.0000 18.66 139.620 1161.01 109.1 0.3082 1.36931 +FS_4 Burner.Fl_O 127.29 140.737 2201.06 571.82 0.0161 27.38 139.831 2197.70 483.4 0.0993 1.31037 +FS_45 HPT.Fl_O 139.68 51.716 1706.95 431.05 0.0146 72.01 48.757 1682.16 439.1 0.2986 1.32978 +FS_48 Duct3.Fl_O 139.68 51.457 1706.95 431.05 0.0146 72.37 48.513 1682.16 441.4 0.2986 1.32978 +FS_5 LPT.Fl_O 139.68 10.913 1191.75 292.82 0.0146 285.12 10.024 1165.27 1477.4 0.3555 1.35857 +FS_7 Duct4.Fl_O 139.68 10.804 1191.75 292.82 0.0146 288.00 10.345 1178.15 2018.9 0.2535 1.35857 +FS_9 Core_Nozz.Fl_O 139.68 10.804 1191.75 292.82 0.0146 288.00 6.753 1051.47 862.9 0.8558 1.35857 +FS_15 BypBld.Fl_O 825.63 13.586 552.68 132.11 0.0000 921.88 11.714 529.76 3795.6 0.4651 1.39985 +FS_17 Duct5.Fl_O 825.63 13.485 552.68 132.11 0.0000 928.84 11.626 529.76 3824.3 0.4651 1.39985 +FS_19 Byp_Nozz.Fl_O 825.63 13.485 552.68 132.11 0.0000 928.84 7.121 460.40 2706.3 1.0000 1.39985 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1477.81 1.457 0.9105 3359.914 1.1249 0.9152 -20049.3 39.72 19.77 +LPC 154.10 2.126 0.8543 3167.920 1.2805 0.8689 -7268.9 25.25 16.60 +HPC 82.23 5.182 0.8659 6252.669 1.6694 0.8919 -22819.1 26.34 26.50 +HPT 27.38 2.721 0.9149 155.679 1.2441 0.9047 22819.4 +LPT 72.37 4.715 0.9216 79.151 1.4323 0.9053 27318.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2833.46 1.318 0.9406 0.852 2.0410 0.5215 1.4369 0.9679 3943.9586 +LPC 165.29 1.345 0.8899 0.865 1.6231 0.9323 3.2631 0.9600 3662.6571 +HPC 195.49 20.334 0.8542 0.984 2.1338 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.051 0.9332 101.677 5.0514 1.4085 0.4249 0.9803 1.5311 +LPT 150.37 6.182 0.9204 97.583 6.1824 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4688.37 21740.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 876.22 210.43 46.346 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 876.22 210.43 46.346 +Duct1 0.0025 0.3951 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 876.22 210.43 46.346 +Duct2 0.0025 0.4199 365.99 +Duct3 0.0050 0.2986 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3555 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.8183 1181.42 286.59 148.928 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.5715 1181.42 286.59 148.928 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 552.68 132.11 13.586 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9974 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7303.8 16409.3 22819.4 +LP_Shaft 3270.1 43875.7 27318.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2201.06 0.9940 0.0550 2.01611 0.01609 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.997 0.9976 1.0000 0.9975 2706.36 1.000 1049.7 27931.5 +Core_Nozz 1.600 0.9999 1.0000 0.9999 862.88 0.856 1344.3 5836.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 229 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 20000.0 0.00 881.71 8018.5 0.6342 5085.51 6.7143 726.13 12.506 1984.1 1937.5 1530.1 + core size:20.89 Q: 333.87 Maximum Thrust: 20045.5 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 881.71 9.370 491.33 117.40 0.0000 1345.87 6.753 447.35 4291.3 0.7000 1.40095 +FS_2 Inlet.Fl_O 881.71 9.324 491.33 117.40 0.0000 1352.64 8.223 473.97 5943.4 0.4273 1.40095 +FS_21 Fan.Fl_O 881.71 12.470 538.18 128.63 0.0000 1058.45 10.891 517.75 4515.2 0.4439 1.40015 +FS_13 Splitter.Fl_O2 767.42 12.470 538.18 128.63 0.0000 921.25 10.754 515.88 3795.6 0.4646 1.40015 +FS_22 Splitter.Fl_O1 114.30 12.470 538.18 128.63 0.0000 137.21 11.484 525.65 719.5 0.3451 1.40015 +FS_23 Duct1.Fl_O 114.30 12.439 538.18 128.63 0.0000 137.55 11.455 525.65 721.3 0.3451 1.40015 +FS_24 LPC.Fl_O 114.30 24.081 670.27 160.39 0.0000 79.29 21.543 649.37 366.0 0.4023 1.39707 +FS_25 Duct2.Fl_O 114.30 24.021 670.27 160.39 0.0000 79.49 21.489 649.37 366.9 0.4023 1.39707 +FS_3 HPC.Fl_O 114.30 117.189 1102.13 266.53 0.0000 20.89 109.561 1082.09 119.9 0.3142 1.37431 +FS_36 Bld3.Fl_O 104.01 117.189 1102.13 266.53 0.0000 19.01 109.561 1082.09 109.1 0.3142 1.37431 +FS_4 Burner.Fl_O 105.42 110.743 1984.09 508.11 0.0136 27.36 110.032 1981.00 483.4 0.0989 1.31903 +FS_45 HPT.Fl_O 115.71 40.313 1530.10 381.79 0.0124 72.45 37.977 1507.07 439.1 0.2995 1.34002 +FS_48 Duct3.Fl_O 115.71 40.112 1530.10 381.79 0.0124 72.81 37.787 1507.07 441.4 0.2995 1.34002 +FS_5 LPT.Fl_O 115.71 9.320 1085.09 264.84 0.0124 263.90 8.679 1064.52 1477.4 0.3241 1.36693 +FS_7 Duct4.Fl_O 115.71 9.227 1085.09 264.84 0.0124 266.57 8.893 1074.41 2018.9 0.2326 1.36693 +FS_9 Core_Nozz.Fl_O 115.71 9.227 1085.09 264.84 0.0124 266.57 6.753 997.30 862.8 0.6893 1.36693 +FS_15 BypBld.Fl_O 767.42 12.470 538.18 128.63 0.0000 921.25 10.754 515.88 3795.6 0.4646 1.40015 +FS_17 Duct5.Fl_O 767.42 12.377 538.18 128.63 0.0000 928.21 10.674 515.88 3824.3 0.4646 1.40015 +FS_19 Byp_Nozz.Fl_O 767.42 12.377 538.18 128.63 0.0000 928.21 6.753 452.52 2706.3 0.9716 1.40015 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1352.64 1.337 0.9096 3026.251 1.0954 0.9133 -14010.0 47.64 21.58 +LPC 137.55 1.936 0.8446 2891.515 1.2454 0.8583 -5135.7 23.46 13.34 +HPC 79.49 4.879 0.8648 6205.589 1.6443 0.8905 -17164.6 30.91 31.14 +HPT 27.36 2.747 0.9154 158.373 1.2532 0.9051 17164.6 +LPT 72.81 4.304 0.9177 75.298 1.4101 0.9016 19146.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2593.52 1.235 0.9397 0.767 2.0824 0.5215 1.4369 0.9679 3943.9586 +LPC 147.54 1.287 0.8798 0.789 1.5566 0.9323 3.2631 0.9600 3662.6571 +HPC 188.98 18.930 0.8531 0.976 2.1678 0.4206 0.2163 1.0137 6357.1603 +HPT 30.10 5.112 0.9338 103.436 5.1119 1.4085 0.4249 0.9803 1.5311 +LPT 151.30 5.609 0.9165 92.833 5.6089 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4291.29 19899.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 823.49 197.54 37.670 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 823.49 197.54 37.670 +Duct1 0.0025 0.3451 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 823.49 197.54 37.670 +Duct2 0.0025 0.4023 365.99 +Duct3 0.0050 0.2995 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3241 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.0003 1102.13 266.53 117.189 +Duct5 0.0075 0.4646 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.2863 1102.13 266.53 117.189 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 538.18 128.63 12.470 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.7143 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7054.4 12779.3 17164.6 +LP_Shaft 2945.4 34140.6 19146.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1984.09 0.9940 0.0550 1.41264 0.01358 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.833 0.9975 1.0000 0.9975 2706.36 0.972 1011.2 24118.6 +Core_Nozz 1.366 0.9999 1.0000 0.9999 862.88 0.689 1056.4 3799.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 230 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 20000.0 0.00 778.81 4009.1 0.7559 3030.58 7.8684 726.13 8.887 1703.7 1665.9 1303.8 + core size:21.48 Q: 333.87 Maximum Thrust: 20045.5 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 778.81 9.370 491.33 117.40 0.0000 1188.80 6.753 447.35 3790.5 0.7000 1.40095 +FS_2 Inlet.Fl_O 778.81 9.324 491.33 117.40 0.0000 1194.78 8.494 478.40 5943.4 0.3671 1.40095 +FS_21 Fan.Fl_O 778.81 11.198 521.06 124.52 0.0000 1024.41 9.886 502.80 4515.2 0.4257 1.40047 +FS_13 Splitter.Fl_O2 690.99 11.198 521.06 124.52 0.0000 908.90 9.707 500.19 3795.6 0.4563 1.40047 +FS_22 Splitter.Fl_O1 87.82 11.198 521.06 124.52 0.0000 115.51 10.588 512.77 719.5 0.2840 1.40047 +FS_23 Duct1.Fl_O 87.82 11.170 521.06 124.52 0.0000 115.80 10.561 512.77 721.3 0.2840 1.40047 +FS_24 LPC.Fl_O 87.82 18.725 620.51 148.40 0.0000 75.39 16.965 603.29 366.0 0.3782 1.39866 +FS_25 Duct2.Fl_O 87.82 18.678 620.51 148.40 0.0000 75.58 16.923 603.29 366.9 0.3782 1.39866 +FS_3 HPC.Fl_O 87.82 83.274 996.53 240.12 0.0000 21.48 77.519 977.02 119.9 0.3235 1.38093 +FS_36 Bld3.Fl_O 79.92 83.274 996.53 240.12 0.0000 19.55 77.519 977.02 109.1 0.3235 1.38093 +FS_4 Burner.Fl_O 80.76 78.694 1703.71 428.33 0.0105 27.33 78.189 1700.98 483.4 0.0983 1.33275 +FS_45 HPT.Fl_O 88.66 28.303 1303.84 320.71 0.0096 72.99 26.638 1283.27 439.1 0.3002 1.35490 +FS_48 Duct3.Fl_O 88.66 28.161 1303.84 320.71 0.0096 73.36 26.504 1283.27 441.4 0.3002 1.35490 +FS_5 LPT.Fl_O 88.66 8.109 967.12 234.47 0.0096 219.41 7.734 954.67 1477.4 0.2631 1.37631 +FS_7 Duct4.Fl_O 88.66 8.028 967.12 234.47 0.0096 221.63 7.830 960.54 2018.9 0.1908 1.37631 +FS_9 Core_Nozz.Fl_O 88.66 8.028 967.12 234.47 0.0096 221.63 6.753 922.36 862.9 0.5066 1.37631 +FS_15 BypBld.Fl_O 690.99 11.198 521.06 124.52 0.0000 908.90 9.707 500.19 3795.6 0.4563 1.40047 +FS_17 Duct5.Fl_O 690.99 11.114 521.06 124.52 0.0000 915.77 9.634 500.19 3824.3 0.4563 1.40047 +FS_19 Byp_Nozz.Fl_O 690.99 11.114 521.06 124.52 0.0000 915.77 6.753 451.81 2706.4 0.8742 1.40047 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1194.78 1.201 0.8894 2558.851 1.0605 0.8923 -7850.5 57.73 23.53 +LPC 115.80 1.676 0.8329 2484.773 1.1909 0.8446 -2967.1 24.59 10.24 +HPC 75.58 4.458 0.8628 6131.835 1.6060 0.8878 -11396.2 37.97 38.50 +HPT 27.33 2.780 0.9163 162.487 1.2662 0.9055 11396.2 +LPT 73.36 3.473 0.9105 68.972 1.3482 0.8954 10817.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2290.83 1.140 0.9188 0.649 2.2509 0.5215 1.4369 0.9679 3943.9586 +LPC 124.21 1.207 0.8676 0.678 1.5336 0.9323 3.2631 0.9600 3662.6571 +HPC 179.67 16.988 0.8512 0.965 2.2428 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.190 0.9347 106.123 5.1904 1.4085 0.4249 0.9803 1.5311 +LPT 152.43 4.450 0.9093 85.034 4.4496 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3790.46 17576.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 753.45 180.51 28.141 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 753.45 180.51 28.141 +Duct1 0.0025 0.2840 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 753.45 180.51 28.141 +Duct2 0.0025 0.3782 365.99 +Duct3 0.0050 0.3002 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2631 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.0737 996.53 240.12 83.274 +Duct5 0.0075 0.4563 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.8300 996.53 240.12 83.274 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 521.06 124.52 11.198 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8684 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6706.8 8924.4 11396.2 +LP_Shaft 2490.5 22812.8 10817.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1703.71 0.9940 0.0550 0.84183 0.01053 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.646 0.9975 1.0000 0.9975 2706.36 0.874 909.0 19523.2 +Core_Nozz 1.189 0.9999 1.0000 0.9999 862.88 0.507 748.5 2062.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 231 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 11/ 21/ 1/ 9 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 20000.0 0.00 674.61 1002.3 1.5075 1510.97 9.6377 726.13 5.777 1384.8 1357.2 1051.4 + core size:22.39 Q: 333.87 Maximum Thrust: 20045.5 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 674.61 9.370 491.33 117.40 0.0000 1029.74 6.753 447.35 3283.3 0.7000 1.40095 +FS_2 Inlet.Fl_O 674.61 9.324 491.33 117.40 0.0000 1034.92 8.719 481.98 5943.4 0.3109 1.40095 +FS_21 Fan.Fl_O 674.61 10.106 505.83 120.88 0.0000 968.78 9.065 490.33 4515.2 0.3971 1.40073 +FS_13 Splitter.Fl_O2 611.19 10.106 505.83 120.88 0.0000 877.71 8.867 487.25 3795.6 0.4361 1.40073 +FS_22 Splitter.Fl_O1 63.42 10.106 505.83 120.88 0.0000 91.07 9.772 500.99 719.5 0.2196 1.40073 +FS_23 Duct1.Fl_O 63.42 10.081 505.83 120.88 0.0000 91.30 9.747 500.99 721.3 0.2196 1.40073 +FS_24 LPC.Fl_O 63.42 14.085 567.71 135.72 0.0000 69.23 12.990 554.75 366.0 0.3419 1.39957 +FS_25 Duct2.Fl_O 63.42 14.050 567.71 135.72 0.0000 69.40 12.958 554.75 366.9 0.3419 1.39957 +FS_3 HPC.Fl_O 63.42 54.135 877.23 210.68 0.0000 22.39 50.042 858.13 119.9 0.3383 1.38816 +FS_36 Bld3.Fl_O 57.71 54.135 877.23 210.68 0.0000 20.37 50.042 858.13 109.1 0.3383 1.38816 +FS_4 Burner.Fl_O 58.13 51.158 1384.77 341.26 0.0073 27.28 50.831 1382.46 483.4 0.0974 1.35160 +FS_45 HPT.Fl_O 63.84 18.199 1051.36 255.11 0.0066 73.39 17.117 1033.98 439.1 0.3000 1.37293 +FS_48 Duct3.Fl_O 63.84 18.108 1051.36 255.11 0.0066 73.76 17.031 1033.98 441.4 0.3000 1.37293 +FS_5 LPT.Fl_O 63.84 7.399 844.83 203.64 0.0066 161.83 7.217 839.01 1477.4 0.1897 1.38554 +FS_7 Duct4.Fl_O 63.84 7.325 844.83 203.64 0.0066 163.46 7.228 841.71 2018.9 0.1388 1.38554 +FS_9 Core_Nozz.Fl_O 63.84 7.325 844.83 203.64 0.0066 163.46 6.753 825.94 862.8 0.3443 1.38554 +FS_15 BypBld.Fl_O 611.19 10.106 505.83 120.88 0.0000 877.71 8.867 487.25 3795.6 0.4361 1.40073 +FS_17 Duct5.Fl_O 611.19 10.030 505.83 120.88 0.0000 884.35 8.801 487.25 3824.3 0.4361 1.40073 +FS_19 Byp_Nozz.Fl_O 611.19 10.030 505.83 120.88 0.0000 884.35 6.753 451.68 2706.4 0.7731 1.40073 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1034.92 1.084 0.7901 1986.929 1.0295 0.7926 -3317.0 83.20 24.29 +LPC 91.30 1.397 0.8203 1958.232 1.1223 0.8286 -1331.8 30.72 8.54 +HPC 69.40 3.853 0.8537 6018.740 1.5452 0.8781 -6726.1 49.75 50.75 +HPT 27.28 2.811 0.9179 169.214 1.2824 0.9068 6726.1 +LPT 73.76 2.448 0.8999 59.641 1.2445 0.8881 4648.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1984.32 1.058 0.8162 0.504 2.6183 0.5215 1.4369 0.9679 3943.9586 +LPC 97.93 1.122 0.8544 0.535 1.5963 0.9323 3.2631 0.9600 3662.6571 +HPC 164.99 14.189 0.8422 0.947 2.3806 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.262 0.9363 110.517 5.2623 1.4085 0.4249 0.9803 1.5311 +LPT 153.26 3.019 0.8987 73.530 3.0193 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3283.31 15225.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 676.76 161.96 19.922 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 676.76 161.96 19.922 +Duct1 0.0025 0.2196 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 676.76 161.96 19.922 +Duct2 0.0025 0.3419 365.99 +Duct3 0.0050 0.3000 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1897 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.2196 877.23 210.68 54.135 +Duct5 0.0075 0.4361 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.4879 877.23 210.68 54.135 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 505.83 120.88 10.106 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.6377 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6296.9 5610.1 6726.1 +LP_Shaft 1933.8 12625.4 4648.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1384.77 0.9940 0.0550 0.41971 0.00727 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.485 0.9975 1.0000 0.9975 2706.36 0.773 803.8 15269.7 +Core_Nozz 1.085 0.9999 1.0000 0.9999 862.88 0.344 482.7 957.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 232 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 8/ 18/ 1/ 6 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 25000.0 0.00 786.85 15543.2 0.5173 8039.94 5.0409 508.22 22.720 2388.1 2327.3 1863.6 + core size:19.94 Q: 137.55 Maximum Thrust: 15543.2 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 786.85 6.470 451.07 107.76 0.0000 1666.72 5.453 429.52 6505.8 0.5000 1.40132 +FS_2 Inlet.Fl_O 786.85 6.438 451.07 107.76 0.0000 1675.11 5.139 422.88 5943.4 0.5763 1.40132 +FS_21 Fan.Fl_O 786.85 10.587 530.62 126.82 0.0000 1104.74 9.102 508.17 4515.2 0.4696 1.40030 +FS_13 Splitter.Fl_O2 656.60 10.587 530.62 126.82 0.0000 921.87 9.128 508.59 3795.6 0.4650 1.40030 +FS_22 Splitter.Fl_O1 130.25 10.587 530.62 126.82 0.0000 182.88 8.956 505.83 719.5 0.4946 1.40030 +FS_23 Duct1.Fl_O 130.25 10.561 530.62 126.82 0.0000 183.34 8.934 505.83 721.3 0.4946 1.40030 +FS_24 LPC.Fl_O 130.25 26.279 711.90 170.44 0.0000 85.34 22.992 685.42 366.0 0.4416 1.39561 +FS_25 Duct2.Fl_O 130.25 26.213 711.90 170.44 0.0000 85.55 22.935 685.42 366.9 0.4416 1.39561 +FS_3 HPC.Fl_O 130.25 146.999 1216.38 295.49 0.0000 19.94 138.343 1196.69 119.9 0.2990 1.36711 +FS_36 Bld3.Fl_O 118.53 146.999 1216.38 295.49 0.0000 18.15 138.343 1196.69 109.1 0.2990 1.36711 +FS_4 Burner.Fl_O 120.76 138.914 2388.10 628.36 0.0188 27.41 138.018 2384.50 483.4 0.0997 1.30350 +FS_45 HPT.Fl_O 132.49 52.040 1863.59 475.97 0.0171 70.92 49.156 1837.91 439.1 0.2946 1.32124 +FS_48 Duct3.Fl_O 132.49 51.779 1863.59 475.97 0.0171 71.28 48.911 1837.91 441.4 0.2946 1.32124 +FS_5 LPT.Fl_O 132.49 10.603 1292.70 319.90 0.0171 289.91 9.706 1263.32 1477.4 0.3636 1.35053 +FS_7 Duct4.Fl_O 132.49 10.497 1292.70 319.90 0.0171 292.84 10.034 1277.66 2018.9 0.2589 1.35053 +FS_9 Core_Nozz.Fl_O 132.49 10.497 1292.70 319.90 0.0171 292.84 5.607 1096.23 862.9 1.0000 1.35053 +FS_15 BypBld.Fl_O 656.60 10.587 530.62 126.82 0.0000 921.87 9.128 508.59 3795.6 0.4650 1.40030 +FS_17 Duct5.Fl_O 656.60 10.508 530.62 126.82 0.0000 928.83 9.060 508.59 3824.3 0.4650 1.40030 +FS_19 Byp_Nozz.Fl_O 656.60 10.508 530.62 126.82 0.0000 928.83 5.548 441.98 2706.4 1.0000 1.40030 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.645 0.8675 3944.235 1.1764 0.8766 -21214.5 24.71 17.45 +LPC 183.34 2.488 0.8683 3636.573 1.3416 0.8840 -8040.0 28.37 23.28 +HPC 85.55 5.608 0.8651 6325.655 1.7086 0.8922 -23045.3 20.10 20.15 +HPT 27.41 2.669 0.9133 151.650 1.2335 0.9035 23045.6 +LPT 71.28 4.884 0.9323 85.204 1.4416 0.9180 29253.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8963 1.000 2.3706 0.5215 1.4369 0.9679 3943.9586 +LPC 196.66 1.456 0.9045 0.993 1.7662 0.9323 3.2631 0.9600 3662.6571 +HPC 203.39 22.301 0.8535 0.995 2.0421 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.929 0.9316 99.045 4.9291 1.4085 0.4249 0.9803 1.5311 +LPT 148.11 6.418 0.9311 105.046 6.4175 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6505.78 12429.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 891.61 214.21 43.908 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 891.61 214.21 43.908 +Duct1 0.0025 0.4946 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 891.61 214.21 43.908 +Duct2 0.0025 0.4416 365.99 +Duct3 0.0050 0.2946 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.5589 1216.38 295.49 146.999 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.1640 1216.38 295.49 146.999 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 530.62 126.82 10.587 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0409 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7410.9 16332.5 23045.6 +LP_Shaft 3678.2 41771.4 29253.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2388.10 0.9940 0.0550 2.23332 0.01884 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.927 0.9975 1.0000 0.9975 2706.36 1.000 1028.5 21246.3 +Core_Nozz 1.925 0.9999 1.0000 0.9999 862.88 1.000 1601.2 6726.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 233 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 25000.0 0.00 765.66 13988.7 0.5055 7071.17 5.3153 508.22 20.728 2298.2 2240.0 1786.5 + core size:20.04 Q: 137.55 Maximum Thrust: 15543.2 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 765.66 6.470 451.07 107.76 0.0000 1621.82 5.453 429.52 6330.5 0.5000 1.40132 +FS_2 Inlet.Fl_O 765.66 6.438 451.07 107.76 0.0000 1629.99 5.232 425.05 5943.4 0.5522 1.40132 +FS_21 Fan.Fl_O 765.66 10.328 524.22 125.28 0.0000 1095.24 8.909 502.52 4515.2 0.4642 1.40042 +FS_13 Splitter.Fl_O2 644.42 10.328 524.22 125.28 0.0000 921.81 8.905 502.45 3795.6 0.4650 1.40042 +FS_22 Splitter.Fl_O1 121.24 10.328 524.22 125.28 0.0000 173.43 8.931 502.87 719.5 0.4603 1.40042 +FS_23 Duct1.Fl_O 121.24 10.303 524.22 125.28 0.0000 173.86 8.909 502.87 721.3 0.4603 1.40042 +FS_24 LPC.Fl_O 121.24 23.926 688.62 164.82 0.0000 85.81 20.895 662.62 366.0 0.4446 1.39640 +FS_25 Duct2.Fl_O 121.24 23.866 688.62 164.82 0.0000 86.02 20.843 662.62 366.9 0.4446 1.39640 +FS_3 HPC.Fl_O 121.24 134.113 1179.95 286.21 0.0000 20.04 126.134 1160.56 119.9 0.3004 1.36941 +FS_36 Bld3.Fl_O 110.33 134.113 1179.95 286.21 0.0000 18.23 126.134 1160.56 109.1 0.3004 1.36941 +FS_4 Burner.Fl_O 112.29 126.736 2298.17 601.23 0.0178 27.41 125.919 2294.68 483.4 0.0995 1.30659 +FS_45 HPT.Fl_O 123.20 46.984 1786.50 453.87 0.0162 71.52 44.334 1761.20 439.1 0.2969 1.32514 +FS_48 Duct3.Fl_O 123.20 46.749 1786.50 453.87 0.0162 71.88 44.112 1761.20 441.4 0.2969 1.32514 +FS_5 LPT.Fl_O 123.20 9.677 1241.14 306.09 0.0162 289.42 8.862 1212.83 1477.4 0.3624 1.35440 +FS_7 Duct4.Fl_O 123.20 9.581 1241.14 306.09 0.0162 292.34 9.160 1226.64 2018.9 0.2581 1.35440 +FS_9 Core_Nozz.Fl_O 123.20 9.581 1241.14 306.09 0.0162 292.34 5.453 1069.19 862.9 0.9434 1.35440 +FS_15 BypBld.Fl_O 644.42 10.328 524.22 125.28 0.0000 921.81 8.905 502.45 3795.6 0.4650 1.40042 +FS_17 Duct5.Fl_O 644.42 10.251 524.22 125.28 0.0000 928.78 8.839 502.45 3824.3 0.4650 1.40042 +FS_19 Byp_Nozz.Fl_O 644.42 10.251 524.22 125.28 0.0000 928.78 5.453 437.57 2706.3 0.9936 1.40042 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1629.99 1.604 0.8934 3732.820 1.1622 0.9003 -18980.5 28.44 17.78 +LPC 173.86 2.322 0.8660 3462.597 1.3136 0.8808 -6781.6 28.97 22.17 +HPC 86.02 5.619 0.8639 6337.462 1.7135 0.8915 -20823.5 20.49 20.51 +HPT 27.41 2.697 0.9139 152.324 1.2387 0.9039 20823.6 +LPT 71.88 4.831 0.9278 82.359 1.4394 0.9125 25759.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3125.16 1.421 0.9230 0.946 2.1684 0.5215 1.4369 0.9679 3943.9586 +LPC 186.49 1.405 0.9020 0.945 1.7529 0.9323 3.2631 0.9600 3662.6571 +HPC 204.50 22.355 0.8523 0.997 2.0726 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.995 0.9322 99.485 4.9951 1.4085 0.4249 0.9803 1.5311 +LPT 149.35 6.344 0.9266 101.538 6.3438 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6330.53 12094.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 863.45 207.31 40.017 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 863.45 207.31 40.017 +Duct1 0.0025 0.4603 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 863.45 207.31 40.017 +Duct2 0.0025 0.4446 365.99 +Duct3 0.0050 0.2969 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3624 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.2433 1179.95 286.21 134.113 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.6681 1179.95 286.21 134.113 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 524.22 125.28 10.328 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3153 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7302.3 14977.2 20823.6 +LP_Shaft 3481.1 38865.3 25759.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2298.17 0.9940 0.0550 1.96421 0.01780 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.880 0.9975 1.0000 0.9975 2706.36 0.994 1016.8 20365.4 +Core_Nozz 1.757 0.9999 1.0000 0.9999 862.88 0.943 1493.2 5717.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 234 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 25000.0 0.00 740.64 12434.5 0.4998 6214.17 5.5245 508.22 19.012 2208.5 2153.2 1712.2 + core size:20.18 Q: 137.55 Maximum Thrust: 15543.2 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 740.64 6.470 451.07 107.76 0.0000 1568.82 5.453 429.52 6123.7 0.5000 1.40132 +FS_2 Inlet.Fl_O 740.64 6.438 451.07 107.76 0.0000 1576.72 5.332 427.38 5943.4 0.5255 1.40132 +FS_21 Fan.Fl_O 740.64 10.003 518.17 123.83 0.0000 1087.63 8.651 497.10 4515.2 0.4599 1.40053 +FS_13 Splitter.Fl_O2 627.12 10.003 518.17 123.83 0.0000 920.93 8.628 496.71 3795.6 0.4643 1.40053 +FS_22 Splitter.Fl_O1 113.52 10.003 518.17 123.83 0.0000 166.70 8.771 499.06 719.5 0.4372 1.40053 +FS_23 Duct1.Fl_O 113.52 9.978 518.17 123.83 0.0000 167.12 8.749 499.06 721.3 0.4372 1.40053 +FS_24 LPC.Fl_O 113.52 22.341 673.37 161.14 0.0000 85.08 19.567 648.46 366.0 0.4396 1.39695 +FS_25 Duct2.Fl_O 113.52 22.285 673.37 161.14 0.0000 85.30 19.518 648.46 366.9 0.4396 1.39695 +FS_3 HPC.Fl_O 113.52 123.007 1148.60 278.26 0.0000 20.18 115.576 1129.36 119.9 0.3026 1.37138 +FS_36 Bld3.Fl_O 103.30 123.007 1148.60 278.26 0.0000 18.37 115.576 1129.36 109.1 0.3026 1.37138 +FS_4 Burner.Fl_O 105.03 116.242 2208.49 574.38 0.0167 27.40 115.492 2205.11 483.4 0.0994 1.30975 +FS_45 HPT.Fl_O 115.24 42.861 1712.23 432.76 0.0152 71.79 40.424 1687.56 439.1 0.2977 1.32915 +FS_48 Duct3.Fl_O 115.24 42.647 1712.23 432.76 0.0152 72.15 40.222 1687.56 441.4 0.2977 1.32915 +FS_5 LPT.Fl_O 115.24 8.963 1190.85 292.72 0.0152 286.31 8.226 1164.15 1477.4 0.3573 1.35826 +FS_7 Duct4.Fl_O 115.24 8.873 1190.85 292.72 0.0152 289.20 8.493 1177.15 2018.9 0.2547 1.35826 +FS_9 Core_Nozz.Fl_O 115.24 8.873 1190.85 292.72 0.0152 289.20 5.453 1045.99 862.9 0.8721 1.35826 +FS_15 BypBld.Fl_O 627.12 10.003 518.17 123.83 0.0000 920.93 8.628 496.71 3795.6 0.4643 1.40053 +FS_17 Duct5.Fl_O 627.12 9.928 518.17 123.83 0.0000 927.89 8.563 496.71 3824.3 0.4643 1.40053 +FS_19 Byp_Nozz.Fl_O 627.12 9.928 518.17 123.83 0.0000 927.89 5.453 436.51 2706.3 0.9657 1.40053 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1576.72 1.554 0.9036 3594.031 1.1488 0.9095 -16841.6 32.26 18.40 +LPC 167.12 2.239 0.8632 3353.245 1.2995 0.8778 -5991.5 28.36 20.59 +HPC 85.30 5.520 0.8645 6318.240 1.7057 0.8919 -18811.3 21.95 22.03 +HPT 27.40 2.712 0.9145 153.190 1.2426 0.9043 18811.4 +LPT 72.15 4.758 0.9262 80.998 1.4378 0.9106 22833.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3023.18 1.385 0.9336 0.911 2.0846 0.5215 1.4369 0.9679 3943.9586 +LPC 179.26 1.380 0.8992 0.916 1.7218 0.9323 3.2631 0.9600 3662.6571 +HPC 202.78 21.894 0.8529 0.994 2.0982 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.029 0.9328 100.051 5.0295 1.4085 0.4249 0.9803 1.5311 +LPT 149.93 6.242 0.9250 99.861 6.2425 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6123.66 11699.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 842.29 202.13 37.041 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 842.29 202.13 37.041 +Duct1 0.0025 0.4372 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 842.29 202.13 37.041 +Duct2 0.0025 0.4396 365.99 +Duct3 0.0050 0.2977 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3573 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.9731 1148.60 278.26 123.007 +Duct5 0.0075 0.4643 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.2434 1148.60 278.26 123.007 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 518.17 123.83 10.003 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5245 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7199.1 13723.8 18811.4 +LP_Shaft 3351.6 35780.4 22833.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2208.49 0.9940 0.0550 1.72616 0.01671 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.820 0.9975 1.0000 0.9975 2706.36 0.966 987.1 19239.7 +Core_Nozz 1.627 0.9999 1.0000 0.9999 862.88 0.872 1366.3 4893.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 235 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 25000.0 0.00 681.72 9326.0 0.5005 4667.49 5.9964 508.22 15.619 2029.4 1979.7 1566.2 + core size:20.48 Q: 137.55 Maximum Thrust: 15543.2 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 681.72 6.470 451.07 107.76 0.0000 1444.02 5.453 429.52 5636.5 0.5000 1.40132 +FS_2 Inlet.Fl_O 681.72 6.438 451.07 107.76 0.0000 1451.29 5.539 432.06 5943.4 0.4682 1.40132 +FS_21 Fan.Fl_O 681.72 9.281 505.67 120.84 0.0000 1065.84 8.087 486.13 4515.2 0.4478 1.40073 +FS_13 Splitter.Fl_O2 584.28 9.281 505.67 120.84 0.0000 913.50 8.030 485.15 3795.6 0.4594 1.40073 +FS_22 Splitter.Fl_O1 97.44 9.281 505.67 120.84 0.0000 152.34 8.353 490.66 719.5 0.3907 1.40073 +FS_23 Duct1.Fl_O 97.44 9.258 505.67 120.84 0.0000 152.72 8.332 490.66 721.3 0.3907 1.40073 +FS_24 LPC.Fl_O 97.44 19.201 642.49 153.69 0.0000 83.00 16.952 620.08 366.0 0.4258 1.39806 +FS_25 Duct2.Fl_O 97.44 19.153 642.49 153.69 0.0000 83.21 16.910 620.08 366.9 0.4258 1.39806 +FS_3 HPC.Fl_O 97.44 101.054 1082.91 261.70 0.0000 20.48 94.758 1064.04 119.9 0.3070 1.37552 +FS_36 Bld3.Fl_O 88.67 101.054 1082.91 261.70 0.0000 18.63 94.758 1064.04 109.1 0.3070 1.37552 +FS_4 Burner.Fl_O 89.97 95.496 2029.39 521.59 0.0146 27.39 94.881 2026.24 483.4 0.0991 1.31672 +FS_45 HPT.Fl_O 98.74 34.947 1566.16 391.92 0.0133 72.15 32.939 1542.92 439.1 0.2984 1.33752 +FS_48 Duct3.Fl_O 98.74 34.772 1566.16 391.92 0.0133 72.51 32.775 1542.92 441.4 0.2984 1.33752 +FS_5 LPT.Fl_O 98.74 7.806 1101.38 269.20 0.0133 270.88 7.238 1079.32 1477.4 0.3341 1.36526 +FS_7 Duct4.Fl_O 98.74 7.728 1101.38 269.20 0.0133 273.62 7.433 1089.96 2018.9 0.2393 1.36526 +FS_9 Core_Nozz.Fl_O 98.74 7.728 1101.38 269.20 0.0133 273.62 5.453 1002.58 862.8 0.7305 1.36526 +FS_15 BypBld.Fl_O 584.28 9.281 505.67 120.84 0.0000 913.50 8.030 485.15 3795.6 0.4594 1.40073 +FS_17 Duct5.Fl_O 584.28 9.212 505.67 120.84 0.0000 920.40 7.970 485.15 3824.3 0.4594 1.40073 +FS_19 Byp_Nozz.Fl_O 584.28 9.212 505.67 120.84 0.0000 920.40 5.453 435.20 2706.4 0.8984 1.40073 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1451.29 1.442 0.9119 3304.788 1.1211 0.9164 -12613.0 40.39 19.49 +LPC 152.72 2.074 0.8560 3121.249 1.2706 0.8699 -4529.6 26.68 17.27 +HPC 83.21 5.276 0.8655 6271.576 1.6855 0.8922 -14890.0 25.26 25.39 +HPT 27.39 2.733 0.9148 154.946 1.2498 0.9045 14889.9 +LPT 72.51 4.455 0.9220 77.875 1.4220 0.9063 17142.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2782.67 1.307 0.9421 0.838 2.0160 0.5215 1.4369 0.9679 3943.9586 +LPC 163.82 1.329 0.8916 0.852 1.6534 0.9323 3.2631 0.9600 3662.6571 +HPC 197.82 20.767 0.8538 0.987 2.1335 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.078 0.9331 101.198 5.0779 1.4085 0.4249 0.9803 1.5311 +LPT 150.68 5.819 0.9208 96.011 5.8192 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5636.51 10768.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 798.69 191.50 31.152 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 798.69 191.50 31.152 +Duct1 0.0025 0.3907 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 798.69 191.50 31.152 +Duct2 0.0025 0.4258 365.99 +Duct3 0.0050 0.2984 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3341 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.4103 1082.91 261.70 101.054 +Duct5 0.0075 0.4594 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.3591 1082.91 261.70 101.054 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 505.67 120.84 9.281 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9964 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6980.1 11203.7 14889.9 +LP_Shaft 3081.9 29213.5 17142.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2029.39 0.9940 0.0550 1.29652 0.01462 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.689 0.9975 1.0000 0.9975 2706.36 0.898 916.9 16650.7 +Core_Nozz 1.417 0.9999 1.0000 0.9999 862.88 0.730 1122.2 3443.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 236 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 25000.0 0.00 609.76 6217.3 0.5201 3233.95 6.6294 508.22 12.124 1823.5 1780.1 1398.3 + core size:20.84 Q: 137.55 Maximum Thrust: 15543.2 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 609.76 6.470 451.07 107.76 0.0000 1291.59 5.453 429.52 5041.5 0.5000 1.40132 +FS_2 Inlet.Fl_O 609.76 6.438 451.07 107.76 0.0000 1298.09 5.747 436.64 5943.4 0.4058 1.40132 +FS_21 Fan.Fl_O 609.76 8.495 491.89 117.54 0.0000 1027.27 7.493 474.53 4515.2 0.4271 1.40094 +FS_13 Splitter.Fl_O2 529.84 8.495 491.89 117.54 0.0000 892.63 7.411 473.05 3795.6 0.4456 1.40094 +FS_22 Splitter.Fl_O1 79.92 8.495 491.89 117.54 0.0000 134.65 7.850 480.90 719.5 0.3376 1.40094 +FS_23 Duct1.Fl_O 79.92 8.474 491.89 117.54 0.0000 134.98 7.831 480.90 721.3 0.3376 1.40094 +FS_24 LPC.Fl_O 79.92 15.697 603.69 144.36 0.0000 80.73 13.973 583.98 366.0 0.4111 1.39899 +FS_25 Duct2.Fl_O 79.92 15.657 603.69 144.36 0.0000 80.93 13.938 583.98 366.9 0.4111 1.39899 +FS_3 HPC.Fl_O 79.92 78.441 1004.34 242.06 0.0000 20.84 73.367 985.98 119.9 0.3125 1.38044 +FS_36 Bld3.Fl_O 72.73 78.441 1004.34 242.06 0.0000 18.96 73.367 985.98 109.1 0.3125 1.38044 +FS_4 Burner.Fl_O 73.63 74.127 1823.51 462.33 0.0124 27.37 73.650 1820.62 483.4 0.0987 1.32618 +FS_45 HPT.Fl_O 80.82 26.820 1398.31 346.11 0.0112 72.71 25.254 1376.73 439.1 0.2997 1.34806 +FS_48 Duct3.Fl_O 80.82 26.686 1398.31 346.11 0.0112 73.08 25.128 1376.73 441.4 0.2997 1.34806 +FS_5 LPT.Fl_O 80.82 6.901 1011.10 245.83 0.0112 240.31 6.514 995.36 1477.4 0.2911 1.37242 +FS_7 Duct4.Fl_O 80.82 6.832 1011.10 245.83 0.0112 242.73 6.629 1002.84 2018.9 0.2102 1.37242 +FS_9 Core_Nozz.Fl_O 80.82 6.832 1011.10 245.83 0.0112 242.73 5.453 950.86 862.8 0.5813 1.37242 +FS_15 BypBld.Fl_O 529.84 8.495 491.89 117.54 0.0000 892.63 7.411 473.05 3795.6 0.4456 1.40094 +FS_17 Duct5.Fl_O 529.84 8.431 491.89 117.54 0.0000 899.37 7.356 473.05 3824.3 0.4456 1.40094 +FS_19 Byp_Nozz.Fl_O 529.84 8.431 491.89 117.54 0.0000 899.37 5.453 434.20 2706.4 0.8137 1.40094 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1298.09 1.320 0.9129 2924.972 1.0905 0.9162 -8433.4 46.38 20.14 +LPC 134.98 1.852 0.8477 2800.956 1.2273 0.8603 -3033.3 26.41 14.39 +HPC 80.93 5.010 0.8648 6229.125 1.6637 0.8910 -11048.0 29.29 29.48 +HPT 27.37 2.764 0.9153 157.374 1.2597 0.9044 11048.0 +LPT 73.08 3.867 0.9192 72.945 1.3830 0.9044 11466.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2488.92 1.222 0.9431 0.742 2.0236 0.5215 1.4369 0.9679 3943.9586 +LPC 144.79 1.261 0.8830 0.765 1.6155 0.9323 3.2631 0.9600 3662.6571 +HPC 192.40 19.537 0.8531 0.980 2.1711 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.152 0.9337 102.784 5.1515 1.4085 0.4249 0.9803 1.5311 +LPT 151.85 4.999 0.9180 89.932 4.9994 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5041.53 9631.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 745.41 178.56 24.855 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 745.41 178.56 24.855 +Duct1 0.0025 0.3376 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 745.41 178.56 24.855 +Duct2 0.0025 0.4111 365.99 +Duct3 0.0050 0.2997 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2911 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.7973 1004.34 242.06 78.441 +Duct5 0.0075 0.4456 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.3957 1004.34 242.06 78.441 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 491.89 117.54 8.495 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6294 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6720.3 8634.4 11048.0 +LP_Shaft 2727.7 22078.7 11466.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1823.51 0.9940 0.0550 0.89832 0.01235 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.546 0.9975 1.0000 0.9975 2706.36 0.814 829.5 13660.7 +Core_Nozz 1.253 0.9999 1.0000 0.9999 862.88 0.581 871.2 2188.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 237 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 25000.0 0.00 516.90 3108.6 0.6087 1892.13 7.5924 508.22 8.418 1557.2 1521.9 1184.3 + core size:21.38 Q: 137.55 Maximum Thrust: 15543.2 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 516.90 6.470 451.07 107.76 0.0000 1094.91 5.453 429.52 4273.8 0.5000 1.40132 +FS_2 Inlet.Fl_O 516.90 6.438 451.07 107.76 0.0000 1100.42 5.960 441.22 5943.4 0.3334 1.40132 +FS_21 Fan.Fl_O 516.90 7.629 475.92 113.71 0.0000 953.83 6.870 461.86 4515.2 0.3896 1.40114 +FS_13 Splitter.Fl_O2 456.74 7.629 475.92 113.71 0.0000 842.82 6.778 460.08 3795.6 0.4142 1.40114 +FS_22 Splitter.Fl_O1 60.16 7.629 475.92 113.71 0.0000 111.01 7.247 468.97 719.5 0.2718 1.40114 +FS_23 Duct1.Fl_O 60.16 7.610 475.92 113.71 0.0000 111.29 7.229 468.97 721.3 0.2718 1.40114 +FS_24 LPC.Fl_O 60.16 11.856 552.80 132.14 0.0000 76.98 10.688 536.66 366.0 0.3877 1.39985 +FS_25 Duct2.Fl_O 60.16 11.826 552.80 132.14 0.0000 77.18 10.661 536.66 366.9 0.3877 1.39985 +FS_3 HPC.Fl_O 60.16 54.466 899.46 216.14 0.0000 21.38 50.744 881.86 119.9 0.3209 1.38688 +FS_36 Bld3.Fl_O 54.74 54.466 899.46 216.14 0.0000 19.45 50.744 881.86 109.1 0.3209 1.38688 +FS_4 Burner.Fl_O 55.27 51.470 1557.20 388.06 0.0096 27.34 51.140 1554.65 483.4 0.0980 1.34052 +FS_45 HPT.Fl_O 60.68 18.383 1184.27 289.45 0.0087 73.30 17.292 1165.10 439.1 0.3007 1.36302 +FS_48 Duct3.Fl_O 60.68 18.292 1184.27 289.45 0.0087 73.67 17.206 1165.10 441.4 0.3007 1.36302 +FS_5 LPT.Fl_O 60.68 6.209 911.70 220.49 0.0087 190.41 5.996 902.95 1477.4 0.2256 1.38035 +FS_7 Duct4.Fl_O 60.68 6.147 911.70 220.49 0.0087 192.33 6.034 907.03 2018.9 0.1644 1.38035 +FS_9 Core_Nozz.Fl_O 60.68 6.147 911.70 220.49 0.0087 192.33 5.453 882.08 862.8 0.4195 1.38035 +FS_15 BypBld.Fl_O 456.74 7.629 475.92 113.71 0.0000 842.82 6.778 460.08 3795.6 0.4142 1.40114 +FS_17 Duct5.Fl_O 456.74 7.572 475.92 113.71 0.0000 849.19 6.727 460.08 3824.3 0.4142 1.40114 +FS_19 Byp_Nozz.Fl_O 456.74 7.572 475.92 113.71 0.0000 849.19 5.453 433.24 2706.4 0.7007 1.40114 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1100.42 1.185 0.9038 2381.425 1.0551 0.9062 -4352.2 54.77 19.89 +LPC 111.29 1.558 0.8371 2318.398 1.1615 0.8470 -1568.4 30.95 11.67 +HPC 77.18 4.606 0.8630 6162.165 1.6271 0.8884 -7149.7 35.80 36.20 +HPT 27.34 2.800 0.9162 161.213 1.2733 0.9049 7149.8 +LPT 73.67 2.946 0.9063 64.534 1.2990 0.8925 5920.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2109.90 1.129 0.9338 0.604 2.1432 0.5215 1.4369 0.9679 3943.9586 +LPC 119.37 1.171 0.8720 0.633 1.6476 0.9323 3.2631 0.9600 3662.6571 +HPC 183.48 17.668 0.8514 0.969 2.2241 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.236 0.9346 105.291 5.2360 1.4085 0.4249 0.9803 1.5311 +LPT 153.08 3.714 0.9051 79.562 3.7143 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4273.80 8165.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 675.04 161.54 18.073 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 675.04 161.54 18.073 +Duct1 0.0025 0.2718 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 675.04 161.54 18.073 +Duct2 0.0025 0.3877 365.99 +Duct3 0.0050 0.3007 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2256 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.1055 899.46 216.14 54.466 +Duct5 0.0075 0.4142 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.3087 899.46 216.14 54.466 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 475.92 113.71 7.629 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.5924 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6361.7 5902.8 7149.8 +LP_Shaft 2220.8 14001.8 5920.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1557.20 0.9940 0.0550 0.52559 0.00960 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.388 0.9975 1.0000 0.9975 2706.36 0.701 713.5 10129.1 +Core_Nozz 1.127 0.9999 1.0000 0.9999 862.88 0.420 606.8 1144.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 238 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 11/ 31/ 2/ 8 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 25000.0 0.00 420.01 777.2 1.1361 882.96 8.9287 508.22 5.262 1233.4 1208.6 930.8 + core size:22.39 Q: 137.55 Maximum Thrust: 15543.2 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 420.01 6.470 451.07 107.76 0.0000 889.66 5.453 429.52 3472.6 0.5000 1.40132 +FS_2 Inlet.Fl_O 420.01 6.438 451.07 107.76 0.0000 894.14 6.132 444.83 5943.4 0.2644 1.40132 +FS_21 Fan.Fl_O 420.01 6.897 461.56 110.27 0.0000 844.23 6.374 451.27 4515.2 0.3372 1.40126 +FS_13 Splitter.Fl_O2 377.70 6.897 461.56 110.27 0.0000 759.21 6.290 449.55 3795.6 0.3649 1.40126 +FS_22 Splitter.Fl_O1 42.30 6.897 461.56 110.27 0.0000 85.03 6.699 457.73 719.5 0.2042 1.40126 +FS_23 Duct1.Fl_O 42.30 6.880 461.56 110.27 0.0000 85.24 6.682 457.73 721.3 0.2042 1.40126 +FS_24 LPC.Fl_O 42.30 8.780 502.27 120.02 0.0000 69.68 8.088 490.61 366.0 0.3444 1.40079 +FS_25 Duct2.Fl_O 42.30 8.758 502.27 120.02 0.0000 69.85 8.067 490.61 366.9 0.3444 1.40079 +FS_3 HPC.Fl_O 42.30 34.046 779.70 186.88 0.0000 22.39 31.473 762.59 119.9 0.3377 1.39293 +FS_36 Bld3.Fl_O 38.49 34.046 779.70 186.88 0.0000 20.37 31.473 762.59 109.1 0.3377 1.39293 +FS_4 Burner.Fl_O 38.74 32.174 1233.42 301.52 0.0064 27.29 31.968 1231.32 483.4 0.0971 1.36153 +FS_45 HPT.Fl_O 42.55 11.385 930.85 224.79 0.0058 73.57 10.705 915.14 439.1 0.2999 1.38108 +FS_48 Duct3.Fl_O 42.55 11.329 930.85 224.79 0.0058 73.94 10.651 915.14 441.4 0.2999 1.38108 +FS_5 LPT.Fl_O 42.55 5.805 790.90 190.29 0.0058 133.02 5.709 787.24 1477.4 0.1546 1.38874 +FS_7 Duct4.Fl_O 42.55 5.747 790.90 190.29 0.0058 134.36 5.695 788.92 2018.9 0.1136 1.38874 +FS_9 Core_Nozz.Fl_O 42.55 5.747 790.90 190.29 0.0058 134.36 5.453 779.38 862.9 0.2758 1.38874 +FS_15 BypBld.Fl_O 377.70 6.897 461.56 110.27 0.0000 759.21 6.290 449.55 3795.6 0.3649 1.40126 +FS_17 Duct5.Fl_O 377.70 6.845 461.56 110.27 0.0000 764.94 6.243 449.55 3824.3 0.3649 1.40126 +FS_19 Byp_Nozz.Fl_O 377.70 6.845 461.56 110.27 0.0000 764.94 5.453 432.47 2706.4 0.5789 1.40126 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 894.14 1.071 0.8564 1740.230 1.0233 0.8579 -1493.4 81.92 17.92 +LPC 85.24 1.276 0.8198 1720.326 1.0882 0.8259 -583.4 42.85 9.99 +HPC 69.85 3.888 0.8543 6027.050 1.5523 0.8789 -4001.3 49.22 50.19 +HPT 27.29 2.826 0.9179 168.878 1.2901 0.9064 4001.3 +LPT 73.94 1.952 0.8864 53.191 1.1769 0.8767 2077.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1714.38 1.050 0.8848 0.441 2.4227 0.5215 1.4369 0.9679 3943.9586 +LPC 91.43 1.085 0.8539 0.470 1.7958 0.9323 3.2631 0.9600 3662.6571 +HPC 166.06 14.348 0.8428 0.948 2.3795 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.297 0.9364 110.297 5.2974 1.4085 0.4249 0.9803 1.5311 +LPT 153.64 2.327 0.8853 65.578 2.3275 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3472.64 6634.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 599.78 143.42 12.463 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 599.78 143.42 12.463 +Duct1 0.0025 0.2042 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 599.78 143.42 12.463 +Duct2 0.0025 0.3444 365.99 +Duct3 0.0050 0.2999 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1546 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.4806 779.70 186.88 34.046 +Duct5 0.0075 0.3649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.3266 779.70 186.88 34.046 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 461.56 110.27 6.897 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 8.9287 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 5931.0 3543.3 4001.3 +LP_Shaft 1622.9 6721.8 2077.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1233.42 0.9940 0.0550 0.24527 0.00637 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.255 0.9975 1.0000 0.9975 2706.36 0.579 589.0 6914.5 +Core_Nozz 1.054 0.9999 1.0000 0.9999 862.88 0.276 375.9 497.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 239 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 4/ 14/ 1/ 2 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 25000.0 0.00 837.39 15690.8 0.5588 8768.57 5.0413 609.86 22.713 2434.7 2372.8 1901.8 + core size:19.93 Q: 198.08 Maximum Thrust: 15690.8 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 837.39 6.958 460.55 110.03 0.0000 1666.72 5.453 429.52 5769.7 0.6000 1.40127 +FS_2 Inlet.Fl_O 837.39 6.923 460.55 110.03 0.0000 1675.11 5.526 431.77 5943.4 0.5763 1.40127 +FS_21 Fan.Fl_O 837.39 11.385 541.75 129.49 0.0000 1104.74 9.787 518.84 4515.2 0.4696 1.40007 +FS_13 Splitter.Fl_O2 698.78 11.385 541.75 129.49 0.0000 921.88 9.816 519.27 3795.6 0.4651 1.40007 +FS_22 Splitter.Fl_O1 138.61 11.385 541.75 129.49 0.0000 182.87 9.631 516.46 719.5 0.4946 1.40007 +FS_23 Duct1.Fl_O 138.61 11.356 541.75 129.49 0.0000 183.32 9.607 516.46 721.3 0.4946 1.40007 +FS_24 LPC.Fl_O 138.61 28.265 726.78 174.04 0.0000 85.31 24.733 699.79 366.0 0.4415 1.39513 +FS_25 Duct2.Fl_O 138.61 28.195 726.78 174.04 0.0000 85.52 24.671 699.79 366.9 0.4415 1.39513 +FS_3 HPC.Fl_O 138.61 158.029 1240.23 301.59 0.0000 19.93 148.732 1220.23 119.9 0.2991 1.36562 +FS_36 Bld3.Fl_O 126.14 158.029 1240.23 301.59 0.0000 18.14 148.732 1220.23 109.1 0.2991 1.36562 +FS_4 Burner.Fl_O 128.57 149.338 2434.70 642.47 0.0193 27.41 148.374 2431.05 483.4 0.0997 1.30205 +FS_45 HPT.Fl_O 141.05 55.971 1901.77 486.97 0.0176 70.91 52.870 1875.68 439.1 0.2948 1.31942 +FS_48 Duct3.Fl_O 141.05 55.691 1901.77 486.97 0.0176 71.27 52.605 1875.68 441.4 0.2948 1.31942 +FS_5 LPT.Fl_O 141.05 11.419 1321.59 327.67 0.0176 289.76 10.454 1291.71 1477.4 0.3637 1.34846 +FS_7 Duct4.Fl_O 141.05 11.305 1321.59 327.67 0.0176 292.68 10.807 1306.30 2018.9 0.2590 1.34846 +FS_9 Core_Nozz.Fl_O 141.05 11.305 1321.59 327.67 0.0176 292.68 6.042 1121.67 862.9 1.0000 1.34846 +FS_15 BypBld.Fl_O 698.78 11.385 541.75 129.49 0.0000 921.88 9.816 519.27 3795.6 0.4651 1.40007 +FS_17 Duct5.Fl_O 698.78 11.299 541.75 129.49 0.0000 928.84 9.742 519.27 3824.3 0.4651 1.40007 +FS_19 Byp_Nozz.Fl_O 698.78 11.299 541.75 129.49 0.0000 928.84 5.967 451.27 2706.4 1.0000 1.40007 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.645 0.8675 3944.235 1.1763 0.8766 -23052.7 24.71 17.45 +LPC 183.32 2.489 0.8683 3636.629 1.3415 0.8839 -8737.9 28.34 23.26 +HPC 85.52 5.605 0.8652 6324.913 1.7065 0.8922 -25013.5 20.13 20.19 +HPT 27.41 2.668 0.9134 151.735 1.2324 0.9036 25013.5 +LPT 71.27 4.877 0.9324 85.227 1.4390 0.9182 31790.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8963 1.000 2.3707 0.5215 1.4369 0.9679 3943.9586 +LPC 196.64 1.456 0.9044 0.993 1.7655 0.9323 3.2631 0.9600 3662.6571 +HPC 203.32 22.288 0.8535 0.995 2.0422 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.926 0.9317 99.101 4.9262 1.4085 0.4249 0.9803 1.5311 +LPT 148.10 6.408 0.9312 105.074 6.4083 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5769.68 15872.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 909.82 218.68 47.215 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 909.82 218.68 47.215 +Duct1 0.0025 0.4946 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 909.82 218.68 47.215 +Duct2 0.0025 0.4415 365.99 +Duct3 0.0050 0.2948 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3637 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.8514 1240.23 301.59 158.029 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.6236 1240.23 301.59 158.029 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 541.75 129.49 11.385 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0413 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7487.0 17546.8 25013.5 +LP_Shaft 3716.7 44924.1 31790.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2434.70 0.9940 0.0550 2.43571 0.01931 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.072 0.9976 1.0000 0.9975 2706.36 1.000 1039.3 23960.1 +Core_Nozz 2.073 0.9997 1.0000 0.9999 862.88 1.000 1618.6 7603.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 240 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 25000.0 0.00 815.78 14121.2 0.5476 7732.92 5.3102 609.86 20.771 2344.7 2285.4 1824.7 + core size:20.03 Q: 198.08 Maximum Thrust: 15690.8 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 815.78 6.958 460.55 110.03 0.0000 1623.72 5.453 429.52 5620.8 0.6000 1.40127 +FS_2 Inlet.Fl_O 815.78 6.923 460.55 110.03 0.0000 1631.89 5.622 433.90 5943.4 0.5532 1.40127 +FS_21 Fan.Fl_O 815.78 11.119 535.46 127.98 0.0000 1095.48 9.591 513.29 4515.2 0.4644 1.40020 +FS_13 Splitter.Fl_O2 686.50 11.119 535.46 127.98 0.0000 921.88 9.587 513.23 3795.6 0.4650 1.40020 +FS_22 Splitter.Fl_O1 129.28 11.119 535.46 127.98 0.0000 173.61 9.611 513.60 719.5 0.4610 1.40020 +FS_23 Duct1.Fl_O 129.28 11.092 535.46 127.98 0.0000 174.04 9.587 513.60 721.3 0.4610 1.40020 +FS_24 LPC.Fl_O 129.28 25.824 703.86 168.50 0.0000 85.70 22.562 677.39 366.0 0.4440 1.39588 +FS_25 Duct2.Fl_O 129.28 25.760 703.86 168.50 0.0000 85.92 22.506 677.39 366.9 0.4440 1.39588 +FS_3 HPC.Fl_O 129.28 144.515 1204.07 292.35 0.0000 20.03 135.923 1184.36 119.9 0.3004 1.36789 +FS_36 Bld3.Fl_O 117.65 144.515 1204.07 292.35 0.0000 18.23 135.923 1184.36 109.1 0.3004 1.36789 +FS_4 Burner.Fl_O 119.79 136.567 2344.65 615.16 0.0183 27.41 135.686 2341.11 483.4 0.0996 1.30502 +FS_45 HPT.Fl_O 131.43 50.670 1824.67 464.76 0.0166 71.50 47.813 1798.96 439.1 0.2971 1.32322 +FS_48 Duct3.Fl_O 131.43 50.416 1824.67 464.76 0.0166 71.86 47.574 1798.96 441.4 0.2971 1.32322 +FS_5 LPT.Fl_O 131.43 10.415 1268.98 313.51 0.0166 290.08 9.533 1240.00 1477.4 0.3636 1.35237 +FS_7 Duct4.Fl_O 131.43 10.311 1268.98 313.51 0.0166 293.01 9.856 1254.14 2018.9 0.2589 1.35237 +FS_9 Core_Nozz.Fl_O 131.43 10.311 1268.98 313.51 0.0166 293.01 5.505 1075.31 862.9 1.0000 1.35237 +FS_15 BypBld.Fl_O 686.50 11.119 535.46 127.98 0.0000 921.88 9.587 513.23 3795.6 0.4650 1.40020 +FS_17 Duct5.Fl_O 686.50 11.036 535.46 127.98 0.0000 928.85 9.515 513.23 3824.3 0.4650 1.40020 +FS_19 Byp_Nozz.Fl_O 686.50 11.036 535.46 127.98 0.0000 928.85 5.827 446.02 2706.4 1.0000 1.40020 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1631.89 1.606 0.8929 3738.660 1.1627 0.8998 -20715.0 28.29 17.75 +LPC 174.04 2.328 0.8659 3467.292 1.3145 0.8808 -7411.9 28.84 22.11 +HPC 85.92 5.610 0.8641 6334.635 1.7107 0.8915 -22654.0 20.57 20.60 +HPT 27.41 2.695 0.9139 152.398 1.2373 0.9040 22654.1 +LPT 71.86 4.841 0.9279 82.474 1.4379 0.9126 28124.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3128.66 1.422 0.9224 0.948 2.1722 0.5215 1.4369 0.9679 3943.9586 +LPC 186.68 1.407 0.9020 0.947 1.7505 0.9323 3.2631 0.9600 3662.6571 +HPC 204.25 22.311 0.8525 0.996 2.0718 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.990 0.9322 99.534 4.9899 1.4085 0.4249 0.9803 1.5311 +LPT 149.30 6.358 0.9267 101.680 6.3578 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5620.82 15463.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 881.98 211.85 43.158 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 881.98 211.85 43.158 +Duct1 0.0025 0.4610 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 881.98 211.85 43.158 +Duct2 0.0025 0.4440 365.99 +Duct3 0.0050 0.2971 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.5248 1204.07 292.35 144.515 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.1104 1204.07 292.35 144.515 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 535.46 127.98 11.119 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3102 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7379.4 16123.6 22654.1 +LP_Shaft 3523.0 41929.1 28124.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2344.65 0.9940 0.0550 2.14803 0.01826 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.024 0.9976 1.0000 0.9975 2706.36 1.000 1033.2 23057.8 +Core_Nozz 1.891 0.9999 1.0000 0.9999 862.88 1.000 1586.9 6526.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 241 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 25000.0 0.00 791.13 12552.7 0.5425 6809.75 5.5180 609.86 19.105 2253.6 2197.3 1749.3 + core size:20.18 Q: 198.08 Maximum Thrust: 15690.8 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 791.13 6.958 460.55 110.03 0.0000 1574.64 5.453 429.52 5450.9 0.6000 1.40127 +FS_2 Inlet.Fl_O 791.13 6.923 460.55 110.03 0.0000 1582.57 5.723 436.11 5943.4 0.5284 1.40127 +FS_21 Fan.Fl_O 791.13 10.789 529.62 126.58 0.0000 1088.92 9.327 508.03 4515.2 0.4607 1.40031 +FS_13 Splitter.Fl_O2 669.75 10.789 529.62 126.58 0.0000 921.86 9.302 507.64 3795.6 0.4650 1.40031 +FS_22 Splitter.Fl_O1 121.38 10.789 529.62 126.58 0.0000 167.06 9.454 509.99 719.5 0.4384 1.40031 +FS_23 Duct1.Fl_O 121.38 10.762 529.62 126.58 0.0000 167.48 9.430 509.99 721.3 0.4384 1.40031 +FS_24 LPC.Fl_O 121.38 24.228 689.37 165.00 0.0000 84.88 21.237 664.04 366.0 0.4384 1.39638 +FS_25 Duct2.Fl_O 121.38 24.167 689.37 165.00 0.0000 85.09 21.184 664.04 366.9 0.4384 1.39638 +FS_3 HPC.Fl_O 121.38 132.921 1173.24 284.51 0.0000 20.18 124.890 1153.64 119.9 0.3028 1.36983 +FS_36 Bld3.Fl_O 110.45 132.921 1173.24 284.51 0.0000 18.37 124.890 1153.64 109.1 0.3028 1.36983 +FS_4 Burner.Fl_O 112.34 125.611 2253.61 587.77 0.0171 27.40 124.801 2250.18 483.4 0.0994 1.30825 +FS_45 HPT.Fl_O 123.27 46.369 1749.31 443.22 0.0156 71.75 43.736 1724.25 439.1 0.2977 1.32720 +FS_48 Duct3.Fl_O 123.27 46.137 1749.31 443.22 0.0156 72.11 43.517 1724.25 441.4 0.2977 1.32720 +FS_5 LPT.Fl_O 123.27 9.583 1215.30 299.18 0.0156 289.35 8.777 1187.49 1477.4 0.3620 1.35645 +FS_7 Duct4.Fl_O 123.27 9.488 1215.30 299.18 0.0156 292.27 9.072 1201.05 2018.9 0.2578 1.35645 +FS_9 Core_Nozz.Fl_O 123.27 9.488 1215.30 299.18 0.0156 292.27 5.453 1048.99 862.9 0.9343 1.35645 +FS_15 BypBld.Fl_O 669.75 10.789 529.62 126.58 0.0000 921.86 9.302 507.64 3795.6 0.4650 1.40031 +FS_17 Duct5.Fl_O 669.75 10.708 529.62 126.58 0.0000 928.82 9.233 507.64 3824.3 0.4650 1.40031 +FS_19 Byp_Nozz.Fl_O 669.75 10.708 529.62 126.58 0.0000 928.82 5.654 441.15 2706.4 1.0000 1.40031 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1582.57 1.559 0.9027 3606.732 1.1500 0.9087 -18522.5 31.91 18.38 +LPC 167.48 2.251 0.8631 3363.315 1.3016 0.8777 -6597.8 28.09 20.47 +HPC 85.09 5.500 0.8648 6313.228 1.7019 0.8919 -20523.2 22.15 22.23 +HPT 27.40 2.709 0.9145 153.318 1.2412 0.9045 20523.0 +LPT 72.11 4.814 0.9260 81.259 1.4394 0.9103 25120.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3034.37 1.389 0.9326 0.914 2.0937 0.5215 1.4369 0.9679 3943.9586 +LPC 179.65 1.383 0.8990 0.918 1.7163 0.9323 3.2631 0.9600 3662.6571 +HPC 202.29 21.803 0.8531 0.993 2.0980 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.022 0.9328 100.134 5.0222 1.4085 0.4249 0.9803 1.5311 +LPT 149.83 6.321 0.9248 100.182 6.3207 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5450.93 14995.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 861.49 206.83 40.100 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 861.49 206.83 40.100 +Duct1 0.0025 0.4384 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 861.49 206.83 40.100 +Duct2 0.0025 0.4384 365.99 +Duct3 0.0050 0.2977 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3620 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.2481 1173.24 284.51 132.921 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.6756 1173.24 284.51 132.921 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 529.62 126.58 10.789 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5180 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7278.3 14809.6 20523.0 +LP_Shaft 3398.6 38820.2 25120.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2253.61 0.9940 0.0550 1.89160 0.01713 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.964 0.9976 1.0000 0.9975 2706.36 1.000 1027.5 21933.2 +Core_Nozz 1.740 0.9999 1.0000 0.9999 862.88 0.934 1465.7 5615.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 242 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 25000.0 0.00 734.46 9413.8 0.5455 5134.94 6.0089 609.86 15.787 2071.5 2021.0 1601.2 + core size:20.50 Q: 198.08 Maximum Thrust: 15690.8 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 734.46 6.958 460.55 110.03 0.0000 1461.85 5.453 429.52 5060.5 0.6000 1.40127 +FS_2 Inlet.Fl_O 734.46 6.923 460.55 110.03 0.0000 1469.21 5.927 440.52 5943.4 0.4760 1.40127 +FS_21 Fan.Fl_O 734.46 10.032 517.20 123.60 0.0000 1074.35 8.716 496.80 4515.2 0.4526 1.40054 +FS_13 Splitter.Fl_O2 629.67 10.032 517.20 123.60 0.0000 921.07 8.653 495.76 3795.6 0.4644 1.40054 +FS_22 Splitter.Fl_O1 104.79 10.032 517.20 123.60 0.0000 153.28 9.015 501.62 719.5 0.3936 1.40054 +FS_23 Duct1.Fl_O 104.79 10.007 517.20 123.60 0.0000 153.67 8.993 501.62 721.3 0.3936 1.40054 +FS_24 LPC.Fl_O 104.79 21.070 660.37 158.00 0.0000 82.47 18.638 637.72 366.0 0.4225 1.39744 +FS_25 Duct2.Fl_O 104.79 21.017 660.37 158.00 0.0000 82.68 18.592 637.72 366.9 0.4225 1.39744 +FS_3 HPC.Fl_O 104.79 109.837 1108.55 268.15 0.0000 20.50 102.977 1089.24 119.9 0.3076 1.37391 +FS_36 Bld3.Fl_O 95.36 109.837 1108.55 268.15 0.0000 18.65 102.977 1089.24 109.1 0.3076 1.37391 +FS_4 Burner.Fl_O 96.78 103.796 2071.54 533.82 0.0150 27.39 103.128 2068.34 483.4 0.0991 1.31507 +FS_45 HPT.Fl_O 106.22 38.055 1601.15 401.56 0.0136 72.07 35.874 1577.55 439.1 0.2982 1.33555 +FS_48 Duct3.Fl_O 106.22 37.864 1601.15 401.56 0.0136 72.43 35.694 1577.55 441.4 0.2982 1.33555 +FS_5 LPT.Fl_O 106.22 8.227 1119.06 273.81 0.0136 278.68 7.590 1095.22 1477.4 0.3454 1.36392 +FS_7 Duct4.Fl_O 106.22 8.145 1119.06 273.81 0.0136 281.50 7.815 1106.77 2018.9 0.2469 1.36392 +FS_9 Core_Nozz.Fl_O 106.22 8.145 1119.06 273.81 0.0136 281.50 5.453 1004.51 863.0 0.7866 1.36392 +FS_15 BypBld.Fl_O 629.67 10.032 517.20 123.60 0.0000 921.07 8.653 495.76 3795.6 0.4644 1.40054 +FS_17 Duct5.Fl_O 629.67 9.957 517.20 123.60 0.0000 928.03 8.588 495.76 3824.3 0.4644 1.40054 +FS_19 Byp_Nozz.Fl_O 629.67 9.957 517.20 123.60 0.0000 928.03 5.453 435.32 2706.4 0.9683 1.40054 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1469.21 1.449 0.9107 3338.816 1.1230 0.9154 -14099.7 40.30 19.87 +LPC 153.67 2.105 0.8552 3150.666 1.2768 0.8694 -5100.6 25.88 16.92 +HPC 82.68 5.226 0.8657 6261.052 1.6787 0.8923 -16330.8 25.81 25.95 +HPT 27.39 2.728 0.9148 155.220 1.2480 0.9045 16331.3 +LPT 72.43 4.602 0.9218 78.626 1.4308 0.9058 19199.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2816.83 1.313 0.9409 0.847 2.0401 0.5215 1.4369 0.9679 3943.9586 +LPC 164.83 1.339 0.8908 0.860 1.6366 0.9323 3.2631 0.9600 3662.6571 +HPC 196.54 20.536 0.8541 0.985 2.1324 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.066 0.9332 101.377 5.0660 1.4085 0.4249 0.9803 1.5311 +LPT 150.50 6.025 0.9206 96.936 6.0250 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5060.49 13921.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 819.44 196.55 34.029 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 819.44 196.55 34.029 +Duct1 0.0025 0.3936 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 819.44 196.55 34.029 +Duct2 0.0025 0.4225 365.99 +Duct3 0.0050 0.2982 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3454 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.6676 1108.55 268.15 109.837 +Duct5 0.0075 0.4644 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.7634 1108.55 268.15 109.837 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 517.20 123.60 10.032 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.0089 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7064.7 12141.2 16331.3 +LP_Shaft 3146.2 32050.0 19199.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2071.54 0.9940 0.0550 1.42637 0.01496 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.826 0.9975 1.0000 0.9975 2706.36 0.968 988.4 19343.3 +Core_Nozz 1.494 0.9999 1.0000 0.9999 862.88 0.787 1209.3 3992.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 243 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 25000.0 0.00 665.55 6276.4 0.5706 3581.48 6.6932 609.86 12.345 1864.6 1820.4 1432.4 + core size:20.87 Q: 198.08 Maximum Thrust: 15690.8 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 665.55 6.958 460.55 110.03 0.0000 1324.70 5.453 429.52 4585.7 0.6000 1.40127 +FS_2 Inlet.Fl_O 665.55 6.923 460.55 110.03 0.0000 1331.37 6.135 444.89 5943.4 0.4188 1.40127 +FS_21 Fan.Fl_O 665.55 9.192 503.30 120.27 0.0000 1048.16 8.055 484.63 4515.2 0.4383 1.40077 +FS_13 Splitter.Fl_O2 579.04 9.192 503.30 120.27 0.0000 911.92 7.958 482.96 3795.6 0.4583 1.40077 +FS_22 Splitter.Fl_O1 86.51 9.192 503.30 120.27 0.0000 136.25 8.476 491.75 719.5 0.3422 1.40077 +FS_23 Duct1.Fl_O 86.51 9.169 503.30 120.27 0.0000 136.59 8.455 491.75 721.3 0.3422 1.40077 +FS_24 LPC.Fl_O 86.51 17.406 622.79 148.95 0.0000 80.04 15.532 602.89 366.0 0.4068 1.39860 +FS_25 Duct2.Fl_O 86.51 17.362 622.79 148.95 0.0000 80.24 15.493 602.89 366.9 0.4068 1.39860 +FS_3 HPC.Fl_O 86.51 85.893 1031.10 248.73 0.0000 20.87 80.317 1012.24 119.9 0.3133 1.37877 +FS_36 Bld3.Fl_O 78.73 85.893 1031.10 248.73 0.0000 18.99 80.317 1012.24 109.1 0.3133 1.37877 +FS_4 Burner.Fl_O 79.72 81.169 1864.57 473.94 0.0126 27.37 80.647 1861.62 483.4 0.0987 1.32427 +FS_45 HPT.Fl_O 87.51 29.449 1432.38 355.26 0.0115 72.57 27.737 1410.47 439.1 0.2993 1.34592 +FS_48 Duct3.Fl_O 87.51 29.302 1432.38 355.26 0.0115 72.93 27.599 1410.47 441.4 0.2993 1.34592 +FS_5 LPT.Fl_O 87.51 7.168 1023.56 249.03 0.0115 252.04 6.722 1005.90 1477.4 0.3072 1.37145 +FS_7 Duct4.Fl_O 87.51 7.096 1023.56 249.03 0.0115 254.59 6.863 1014.34 2018.9 0.2211 1.37145 +FS_9 Core_Nozz.Fl_O 87.51 7.096 1023.56 249.03 0.0115 254.59 5.453 952.75 862.9 0.6301 1.37145 +FS_15 BypBld.Fl_O 579.04 9.192 503.30 120.27 0.0000 911.92 7.958 482.96 3795.6 0.4583 1.40077 +FS_17 Duct5.Fl_O 579.04 9.123 503.30 120.27 0.0000 918.81 7.899 482.96 3824.3 0.4583 1.40077 +FS_19 Byp_Nozz.Fl_O 579.04 9.123 503.30 120.27 0.0000 918.81 5.453 434.35 2706.4 0.8895 1.40077 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1331.37 1.328 0.9108 2982.148 1.0928 0.9143 -9640.7 47.56 21.19 +LPC 136.59 1.898 0.8463 2852.684 1.2374 0.8595 -3511.1 24.86 13.90 +HPC 80.24 4.947 0.8648 6217.606 1.6556 0.8909 -12213.0 30.05 30.26 +HPT 27.37 2.756 0.9153 157.783 1.2577 0.9046 12213.0 +LPT 72.93 4.088 0.9188 74.249 1.3994 0.9034 13151.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2552.72 1.228 0.9410 0.756 2.0669 0.5215 1.4369 0.9679 3943.9586 +LPC 146.51 1.275 0.8816 0.779 1.5855 0.9323 3.2631 0.9600 3662.6571 +HPC 190.76 19.247 0.8532 0.978 2.1692 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.133 0.9337 103.051 5.1335 1.4085 0.4249 0.9803 1.5311 +LPT 151.55 5.308 0.9176 91.540 5.3078 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4585.72 12615.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 767.34 183.88 27.402 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 767.34 183.88 27.402 +Duct1 0.0025 0.3422 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 767.34 183.88 27.402 +Duct2 0.0025 0.4068 365.99 +Duct3 0.0050 0.2993 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3072 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.0279 1031.10 248.73 85.893 +Duct5 0.0075 0.4583 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.7581 1031.10 248.73 85.893 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 503.30 120.27 9.192 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6932 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6813.2 9414.7 12213.0 +LP_Shaft 2810.1 24581.2 13151.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1864.57 0.9940 0.0550 0.99486 0.01264 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.673 0.9975 1.0000 0.9975 2706.36 0.889 906.9 16321.6 +Core_Nozz 1.301 0.9999 1.0000 0.9999 862.88 0.630 945.1 2570.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 244 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 25000.0 0.00 577.21 3138.1 0.6760 2121.28 7.7669 609.86 8.682 1597.9 1562.0 1217.8 + core size:21.43 Q: 198.08 Maximum Thrust: 15690.8 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 577.21 6.958 460.55 110.03 0.0000 1148.87 5.453 429.52 3977.0 0.6000 1.40127 +FS_2 Inlet.Fl_O 577.21 6.923 460.55 110.03 0.0000 1154.65 6.352 449.34 5943.4 0.3526 1.40127 +FS_21 Fan.Fl_O 577.21 8.254 487.11 116.39 0.0000 995.94 7.348 471.16 4515.2 0.4108 1.40100 +FS_13 Splitter.Fl_O2 511.37 8.254 487.11 116.39 0.0000 882.33 7.230 468.98 3795.6 0.4390 1.40100 +FS_22 Splitter.Fl_O1 65.84 8.254 487.11 116.39 0.0000 113.60 7.820 479.64 719.5 0.2788 1.40100 +FS_23 Duct1.Fl_O 65.84 8.234 487.11 116.39 0.0000 113.89 7.800 479.64 721.3 0.2788 1.40100 +FS_24 LPC.Fl_O 65.84 13.339 573.37 137.08 0.0000 76.27 12.053 557.00 366.0 0.3834 1.39947 +FS_25 Duct2.Fl_O 65.84 13.306 573.37 137.08 0.0000 76.46 12.023 557.00 366.9 0.3834 1.39947 +FS_3 HPC.Fl_O 65.84 60.408 927.99 223.16 0.0000 21.43 56.258 909.79 119.9 0.3220 1.38515 +FS_36 Bld3.Fl_O 59.91 60.408 927.99 223.16 0.0000 19.50 56.258 909.79 109.1 0.3220 1.38515 +FS_4 Burner.Fl_O 60.50 57.085 1597.88 399.16 0.0098 27.34 56.719 1595.28 483.4 0.0981 1.33831 +FS_45 HPT.Fl_O 66.43 20.453 1217.76 298.14 0.0089 73.14 19.245 1198.23 439.1 0.3002 1.36075 +FS_48 Duct3.Fl_O 66.43 20.351 1217.76 298.14 0.0089 73.50 19.149 1198.23 441.4 0.3002 1.36075 +FS_5 LPT.Fl_O 66.43 6.357 919.10 222.37 0.0089 204.43 6.104 908.86 1477.4 0.2434 1.37975 +FS_7 Duct4.Fl_O 66.43 6.293 919.10 222.37 0.0089 206.50 6.159 913.66 2018.9 0.1770 1.37975 +FS_9 Core_Nozz.Fl_O 66.43 6.293 919.10 222.37 0.0089 206.50 5.453 883.53 863.0 0.4596 1.37975 +FS_15 BypBld.Fl_O 511.37 8.254 487.11 116.39 0.0000 882.33 7.230 468.98 3795.6 0.4390 1.40100 +FS_17 Duct5.Fl_O 511.37 8.192 487.11 116.39 0.0000 889.00 7.176 468.98 3824.3 0.4390 1.40100 +FS_19 Byp_Nozz.Fl_O 511.37 8.192 487.11 116.39 0.0000 889.00 5.453 433.54 2706.4 0.7848 1.40100 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1154.65 1.192 0.8954 2477.541 1.0577 0.8980 -5195.0 56.93 22.14 +LPC 113.89 1.620 0.8355 2409.032 1.1771 0.8463 -1926.8 27.57 10.99 +HPC 76.46 4.540 0.8630 6148.450 1.6185 0.8881 -8019.0 36.74 37.21 +HPT 27.34 2.791 0.9162 161.720 1.2710 0.9051 8019.1 +LPT 73.50 3.201 0.9085 66.901 1.3249 0.8940 7121.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2213.89 1.134 0.9250 0.628 2.2135 0.5215 1.4369 0.9679 3943.9586 +LPC 122.16 1.190 0.8703 0.658 1.5886 0.9323 3.2631 0.9600 3662.6571 +HPC 181.77 17.364 0.8513 0.967 2.2314 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.215 0.9346 105.622 5.2154 1.4085 0.4249 0.9803 1.5311 +LPT 152.73 4.071 0.9073 82.480 4.0708 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3977.05 10941.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 698.50 167.20 20.206 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 698.50 167.20 20.206 +Duct1 0.0025 0.2788 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 698.50 167.20 20.206 +Duct2 0.0025 0.3834 365.99 +Duct3 0.0050 0.3002 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2434 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.3044 927.99 223.16 60.408 +Duct5 0.0075 0.4390 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.6212 927.99 223.16 60.408 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 487.11 116.39 8.254 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.7669 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6464.5 6515.1 8019.1 +LP_Shaft 2334.6 16021.9 7121.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1597.88 0.9940 0.0550 0.58925 0.00983 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.502 0.9975 1.0000 0.9975 2706.36 0.785 799.4 12705.8 +Core_Nozz 1.154 0.9999 1.0000 0.9999 862.88 0.460 665.2 1373.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 245 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 10/ 20/ 1/ 8 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 25000.0 0.00 486.93 784.5 1.3066 1025.01 9.3776 609.86 5.536 1282.1 1256.4 969.4 + core size:22.38 Q: 198.08 Maximum Thrust: 15690.8 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 486.93 6.958 460.55 110.03 0.0000 969.17 5.453 429.52 3355.0 0.6000 1.40127 +FS_2 Inlet.Fl_O 486.93 6.923 460.55 110.03 0.0000 974.05 6.528 452.88 5943.4 0.2905 1.40127 +FS_21 Fan.Fl_O 486.93 7.458 472.69 112.94 0.0000 916.03 6.781 459.98 4515.2 0.3711 1.40117 +FS_13 Splitter.Fl_O2 440.01 7.458 472.69 112.94 0.0000 827.76 6.660 457.63 3795.6 0.4051 1.40117 +FS_22 Splitter.Fl_O1 46.92 7.458 472.69 112.94 0.0000 88.27 7.226 468.45 719.5 0.2125 1.40117 +FS_23 Duct1.Fl_O 46.92 7.439 472.69 112.94 0.0000 88.49 7.208 468.45 721.3 0.2125 1.40117 +FS_24 LPC.Fl_O 46.92 9.941 522.43 124.85 0.0000 69.62 9.158 510.33 366.0 0.3441 1.40045 +FS_25 Duct2.Fl_O 46.92 9.916 522.43 124.85 0.0000 69.79 9.136 510.33 366.9 0.3441 1.40045 +FS_3 HPC.Fl_O 46.92 38.514 810.27 194.32 0.0000 22.38 35.606 792.56 119.9 0.3377 1.39145 +FS_36 Bld3.Fl_O 42.70 38.514 810.27 194.32 0.0000 20.36 35.606 792.56 109.1 0.3377 1.39145 +FS_4 Burner.Fl_O 42.98 36.396 1282.13 314.22 0.0067 27.29 36.163 1279.97 483.4 0.0972 1.35827 +FS_45 HPT.Fl_O 47.21 12.902 969.43 234.45 0.0061 73.51 12.132 953.18 439.1 0.2999 1.37849 +FS_48 Duct3.Fl_O 47.21 12.837 969.43 234.45 0.0061 73.88 12.071 953.18 441.4 0.2999 1.37849 +FS_5 LPT.Fl_O 47.21 5.878 800.22 192.61 0.0061 146.61 5.760 795.71 1477.4 0.1710 1.38810 +FS_7 Duct4.Fl_O 47.21 5.819 800.22 192.61 0.0061 148.09 5.756 797.79 2018.9 0.1254 1.38810 +FS_9 Core_Nozz.Fl_O 47.21 5.819 800.22 192.61 0.0061 148.09 5.453 785.82 863.1 0.3072 1.38810 +FS_15 BypBld.Fl_O 440.01 7.458 472.69 112.94 0.0000 827.76 6.660 457.63 3795.6 0.4051 1.40117 +FS_17 Duct5.Fl_O 440.01 7.402 472.69 112.94 0.0000 834.01 6.610 457.63 3824.3 0.4051 1.40117 +FS_19 Byp_Nozz.Fl_O 440.01 7.402 472.69 112.94 0.0000 834.01 5.453 433.10 2706.4 0.6749 1.40117 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 974.05 1.077 0.8167 1867.755 1.0264 0.8187 -2003.2 83.98 21.56 +LPC 88.49 1.336 0.8220 1843.604 1.1052 0.8292 -791.0 36.37 9.33 +HPC 69.79 3.884 0.8543 6025.943 1.5510 0.8789 -4611.5 49.23 50.21 +HPT 27.29 2.821 0.9179 168.899 1.2876 0.9065 4611.5 +LPT 73.88 2.184 0.8966 56.527 1.2115 0.8860 2794.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1867.61 1.054 0.8438 0.474 2.5527 0.5215 1.4369 0.9679 3943.9586 +LPC 94.92 1.103 0.8562 0.503 1.6914 0.9323 3.2631 0.9600 3662.6571 +HPC 165.92 14.333 0.8428 0.948 2.3788 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.286 0.9363 110.311 5.2860 1.4085 0.4249 0.9803 1.5311 +LPT 153.52 2.652 0.8954 69.690 2.6517 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3354.99 9229.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 623.67 149.17 14.105 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 623.67 149.17 14.105 +Duct1 0.0025 0.2125 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 623.67 149.17 14.105 +Duct2 0.0025 0.3441 365.99 +Duct3 0.0050 0.2999 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1710 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.6422 810.27 194.32 38.514 +Duct5 0.0075 0.4051 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.5807 810.27 194.32 38.514 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 472.69 112.94 7.458 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.3776 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6047.7 4004.8 4611.5 +LP_Shaft 1760.0 8339.1 2794.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1282.13 0.9940 0.0550 0.28473 0.00667 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.357 0.9975 1.0000 0.9975 2706.36 0.675 687.2 9397.5 +Core_Nozz 1.067 0.9999 1.0000 0.9999 862.88 0.307 420.4 616.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 246 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 4/ 14/ 1/ 2 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 25000.0 0.00 899.84 16153.0 0.6000 9691.89 5.0412 711.51 22.706 2489.3 2426.1 1946.4 + core size:19.92 Q: 269.61 Maximum Thrust: 16153.0 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 899.84 7.567 471.75 112.71 0.0000 1666.72 5.453 429.52 5314.3 0.7000 1.40118 +FS_2 Inlet.Fl_O 899.84 7.529 471.75 112.71 0.0000 1675.11 6.010 442.28 5943.4 0.5763 1.40118 +FS_21 Fan.Fl_O 899.84 12.381 554.91 132.64 0.0000 1104.75 10.644 531.45 4515.2 0.4697 1.39981 +FS_13 Splitter.Fl_O2 750.89 12.381 554.91 132.64 0.0000 921.88 10.675 531.89 3795.6 0.4651 1.39981 +FS_22 Splitter.Fl_O1 148.95 12.381 554.91 132.64 0.0000 182.87 10.474 529.01 719.5 0.4947 1.39981 +FS_23 Duct1.Fl_O 148.95 12.350 554.91 132.64 0.0000 183.33 10.448 529.01 721.3 0.4947 1.39981 +FS_24 LPC.Fl_O 148.95 30.741 744.27 178.28 0.0000 85.30 26.899 716.66 366.0 0.4415 1.39449 +FS_25 Duct2.Fl_O 148.95 30.664 744.27 178.28 0.0000 85.51 26.832 716.66 366.9 0.4415 1.39449 +FS_3 HPC.Fl_O 148.95 171.813 1268.29 308.79 0.0000 19.92 161.715 1247.93 119.9 0.2991 1.36386 +FS_36 Bld3.Fl_O 135.54 171.813 1268.29 308.79 0.0000 18.13 161.715 1247.93 109.1 0.2991 1.36386 +FS_4 Burner.Fl_O 138.24 162.364 2489.32 659.07 0.0199 27.41 161.316 2485.60 483.4 0.0998 1.30045 +FS_45 HPT.Fl_O 151.64 60.884 1946.43 499.92 0.0181 70.91 57.511 1919.86 439.1 0.2950 1.31736 +FS_48 Duct3.Fl_O 151.64 60.580 1946.43 499.92 0.0181 71.26 57.224 1919.86 441.4 0.2950 1.31736 +FS_5 LPT.Fl_O 151.64 12.440 1355.45 336.82 0.0181 289.60 11.389 1324.99 1477.4 0.3638 1.34606 +FS_7 Duct4.Fl_O 151.64 12.315 1355.45 336.82 0.0181 292.53 11.774 1339.86 2018.9 0.2591 1.34606 +FS_9 Core_Nozz.Fl_O 151.64 12.315 1355.45 336.82 0.0181 292.53 6.587 1151.55 862.9 1.0000 1.34606 +FS_15 BypBld.Fl_O 750.89 12.381 554.91 132.64 0.0000 921.88 10.675 531.89 3795.6 0.4651 1.39981 +FS_17 Duct5.Fl_O 750.89 12.288 554.91 132.64 0.0000 928.85 10.595 531.89 3824.3 0.4651 1.39981 +FS_19 Byp_Nozz.Fl_O 750.89 12.288 554.91 132.64 0.0000 928.85 6.489 462.26 2706.4 1.0000 1.39981 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.644 0.8675 3944.235 1.1763 0.8765 -25375.4 24.71 17.45 +LPC 183.33 2.489 0.8683 3636.715 1.3412 0.8839 -9617.2 28.34 23.26 +HPC 85.51 5.603 0.8652 6324.646 1.7041 0.8922 -27503.6 20.16 20.22 +HPT 27.41 2.667 0.9135 151.850 1.2311 0.9036 27503.4 +LPT 71.26 4.870 0.9326 85.262 1.4360 0.9185 34992.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8962 1.000 2.3709 0.5215 1.4369 0.9679 3943.9586 +LPC 196.65 1.456 0.9044 0.993 1.7655 0.9323 3.2631 0.9600 3662.6571 +HPC 203.30 22.279 0.8535 0.995 2.0430 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.923 0.9318 99.176 4.9229 1.4085 0.4249 0.9803 1.5311 +LPT 148.08 6.398 0.9314 105.117 6.3984 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5314.27 19899.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 931.23 223.96 51.342 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 931.23 223.96 51.342 +Duct1 0.0025 0.4947 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 931.23 223.96 51.342 +Duct2 0.0025 0.4415 365.99 +Duct3 0.0050 0.2950 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3638 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.2133 1268.29 308.79 171.813 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.1923 1268.29 308.79 171.813 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 554.91 132.64 12.381 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0412 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7576.3 19066.3 27503.4 +LP_Shaft 3761.6 48858.1 34992.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2489.32 0.9940 0.0550 2.69219 0.01986 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.253 0.9972 1.0000 0.9975 2706.36 1.000 1051.8 27350.8 +Core_Nozz 2.258 0.9992 1.0000 0.9999 862.88 1.000 1638.6 8701.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 247 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 25000.0 0.00 876.99 14537.4 0.5891 8564.20 5.3078 711.51 20.789 2399.1 2338.5 1869.3 + core size:20.02 Q: 269.61 Maximum Thrust: 16153.0 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 876.99 7.567 471.75 112.71 0.0000 1624.39 5.453 429.52 5179.3 0.7000 1.40118 +FS_2 Inlet.Fl_O 876.99 7.529 471.75 112.71 0.0000 1632.57 6.113 444.42 5943.4 0.5536 1.40118 +FS_21 Fan.Fl_O 876.99 12.098 548.55 131.12 0.0000 1095.57 10.435 525.85 4515.2 0.4645 1.39993 +FS_13 Splitter.Fl_O2 737.96 12.098 548.55 131.12 0.0000 921.88 10.431 525.79 3795.6 0.4651 1.39993 +FS_22 Splitter.Fl_O1 139.03 12.098 548.55 131.12 0.0000 173.68 10.455 526.15 719.5 0.4613 1.39993 +FS_23 Duct1.Fl_O 139.03 12.068 548.55 131.12 0.0000 174.12 10.429 526.15 721.3 0.4613 1.39993 +FS_24 LPC.Fl_O 139.03 28.124 721.16 172.68 0.0000 85.67 24.575 694.09 366.0 0.4438 1.39531 +FS_25 Duct2.Fl_O 139.03 28.054 721.16 172.68 0.0000 85.88 24.513 694.09 366.9 0.4438 1.39531 +FS_3 HPC.Fl_O 139.03 157.304 1231.88 299.45 0.0000 20.02 147.964 1211.81 119.9 0.3004 1.36614 +FS_36 Bld3.Fl_O 126.52 157.304 1231.88 299.45 0.0000 18.22 147.964 1211.81 109.1 0.3004 1.36614 +FS_4 Burner.Fl_O 128.90 148.652 2399.12 631.58 0.0188 27.41 147.693 2395.51 483.4 0.0997 1.30325 +FS_45 HPT.Fl_O 141.41 55.189 1869.28 477.55 0.0171 71.49 52.079 1843.08 439.1 0.2973 1.32103 +FS_48 Duct3.Fl_O 141.41 54.913 1869.28 477.55 0.0171 71.85 51.818 1843.08 441.4 0.2973 1.32103 +FS_5 LPT.Fl_O 141.41 11.362 1302.73 322.55 0.0171 289.87 10.401 1273.17 1477.4 0.3637 1.34993 +FS_7 Duct4.Fl_O 141.41 11.249 1302.73 322.55 0.0171 292.80 10.753 1287.60 2018.9 0.2589 1.34993 +FS_9 Core_Nozz.Fl_O 141.41 11.249 1302.73 322.55 0.0171 292.80 6.009 1105.00 862.9 1.0000 1.34993 +FS_15 BypBld.Fl_O 737.96 12.098 548.55 131.12 0.0000 921.88 10.431 525.79 3795.6 0.4651 1.39993 +FS_17 Duct5.Fl_O 737.96 12.007 548.55 131.12 0.0000 928.85 10.353 525.79 3824.3 0.4651 1.39993 +FS_19 Byp_Nozz.Fl_O 737.96 12.007 548.55 131.12 0.0000 928.85 6.341 456.95 2706.4 1.0000 1.39993 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1632.57 1.607 0.8927 3740.948 1.1628 0.8996 -22839.0 28.24 17.74 +LPC 174.12 2.331 0.8659 3469.196 1.3147 0.8808 -8176.2 28.81 22.09 +HPC 85.88 5.607 0.8642 6333.665 1.7082 0.8914 -24936.7 20.59 20.62 +HPT 27.41 2.693 0.9140 152.475 1.2359 0.9041 24936.8 +LPT 71.85 4.833 0.9280 82.519 1.4349 0.9130 31013.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3130.04 1.422 0.9222 0.949 2.1740 0.5215 1.4369 0.9679 3943.9586 +LPC 186.77 1.408 0.9020 0.947 1.7498 0.9323 3.2631 0.9600 3662.6571 +HPC 204.16 22.298 0.8525 0.996 2.0712 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.986 0.9323 99.584 4.9858 1.4085 0.4249 0.9803 1.5311 +LPT 149.28 6.347 0.9268 101.736 6.3469 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5179.31 19394.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 903.17 217.05 46.989 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 903.17 217.05 46.989 +Duct1 0.0025 0.4613 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 903.17 217.05 46.989 +Duct2 0.0025 0.4438 365.99 +Duct3 0.0050 0.2973 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3637 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.8661 1231.88 299.45 157.304 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.6468 1231.88 299.45 157.304 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 548.55 131.12 12.098 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3078 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7468.4 17536.8 24936.8 +LP_Shaft 3567.7 45655.5 31013.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2399.12 0.9940 0.0550 2.37894 0.01880 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.202 0.9974 1.0000 0.9975 2706.36 1.000 1045.8 26387.3 +Core_Nozz 2.063 0.9997 1.0000 0.9999 862.88 1.000 1607.3 7544.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 248 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 25000.0 0.00 851.31 12922.4 0.5843 7550.78 5.5135 711.51 19.147 2306.5 2248.9 1792.7 + core size:20.17 Q: 269.61 Maximum Thrust: 16153.0 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 851.31 7.567 471.75 112.71 0.0000 1576.82 5.453 429.52 5027.6 0.7000 1.40118 +FS_2 Inlet.Fl_O 851.31 7.529 471.75 112.71 0.0000 1584.76 6.219 446.63 5943.4 0.5295 1.40118 +FS_21 Fan.Fl_O 851.31 11.751 542.76 129.73 0.0000 1089.08 10.159 520.63 4515.2 0.4608 1.40005 +FS_13 Splitter.Fl_O2 720.61 11.751 542.76 129.73 0.0000 921.87 10.132 520.24 3795.6 0.4651 1.40005 +FS_22 Splitter.Fl_O1 130.70 11.751 542.76 129.73 0.0000 167.20 10.294 522.61 719.5 0.4389 1.40005 +FS_23 Duct1.Fl_O 130.70 11.722 542.76 129.73 0.0000 167.62 10.268 522.61 721.3 0.4389 1.40005 +FS_24 LPC.Fl_O 130.70 26.449 706.87 169.23 0.0000 84.78 23.192 681.00 366.0 0.4378 1.39578 +FS_25 Duct2.Fl_O 130.70 26.382 706.87 169.23 0.0000 84.99 23.134 681.00 366.9 0.4378 1.39578 +FS_3 HPC.Fl_O 130.70 144.878 1200.94 291.55 0.0000 20.17 136.133 1180.97 119.9 0.3028 1.36808 +FS_36 Bld3.Fl_O 118.93 144.878 1200.94 291.55 0.0000 18.36 136.133 1180.97 109.1 0.3028 1.36808 +FS_4 Burner.Fl_O 121.03 136.910 2306.52 603.55 0.0176 27.40 136.028 2303.03 483.4 0.0995 1.30648 +FS_45 HPT.Fl_O 132.80 50.583 1792.67 455.52 0.0160 71.73 47.712 1767.13 439.1 0.2979 1.32497 +FS_48 Duct3.Fl_O 132.80 50.330 1792.67 455.52 0.0160 72.09 47.474 1767.13 441.4 0.2979 1.32497 +FS_5 LPT.Fl_O 132.80 10.426 1246.86 307.55 0.0160 290.23 9.542 1218.25 1477.4 0.3636 1.35414 +FS_7 Duct4.Fl_O 132.80 10.321 1246.86 307.55 0.0160 293.16 9.866 1232.21 2018.9 0.2589 1.35414 +FS_9 Core_Nozz.Fl_O 132.80 10.321 1246.86 307.55 0.0160 293.16 5.508 1055.81 862.9 1.0000 1.35414 +FS_15 BypBld.Fl_O 720.61 11.751 542.76 129.73 0.0000 921.87 10.132 520.24 3795.6 0.4651 1.40005 +FS_17 Duct5.Fl_O 720.61 11.663 542.76 129.73 0.0000 928.84 10.056 520.24 3824.3 0.4651 1.40005 +FS_19 Byp_Nozz.Fl_O 720.61 11.663 542.76 129.73 0.0000 928.84 6.159 452.12 2706.4 1.0000 1.40005 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1584.76 1.561 0.9024 3611.972 1.1505 0.9084 -20497.1 31.73 18.34 +LPC 167.62 2.256 0.8630 3367.405 1.3024 0.8777 -7304.0 27.97 20.41 +HPC 84.99 5.491 0.8649 6310.885 1.6989 0.8918 -22620.4 22.22 22.31 +HPT 27.40 2.707 0.9145 153.404 1.2397 0.9046 22620.2 +LPT 72.09 4.828 0.9260 81.359 1.4377 0.9104 27801.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3038.58 1.390 0.9323 0.916 2.0957 0.5215 1.4369 0.9679 3943.9586 +LPC 179.80 1.385 0.8989 0.919 1.7138 0.9323 3.2631 0.9600 3662.6571 +HPC 202.06 21.763 0.8533 0.993 2.0971 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.017 0.9329 100.191 5.0167 1.4085 0.4249 0.9803 1.5311 +LPT 149.79 6.339 0.9248 100.305 6.3394 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5027.63 18826.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 882.77 212.04 43.742 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 882.77 212.04 43.742 +Duct1 0.0025 0.4389 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 882.77 212.04 43.742 +Duct2 0.0025 0.4378 365.99 +Duct3 0.0050 0.2979 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.5744 1200.94 291.55 144.878 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.1884 1200.94 291.55 144.878 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 542.76 129.73 11.751 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5135 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7367.4 16125.6 22620.2 +LP_Shaft 3444.7 42388.2 27801.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2306.52 0.9940 0.0550 2.09744 0.01764 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.139 0.9975 1.0000 0.9975 2706.36 1.000 1040.2 25207.1 +Core_Nozz 1.893 0.9999 1.0000 0.9999 862.88 1.000 1573.4 6541.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 249 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 25000.0 0.00 793.82 9691.8 0.5887 5705.16 5.9967 711.51 15.904 2119.2 2067.7 1640.4 + core size:20.51 Q: 269.61 Maximum Thrust: 16153.0 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 793.82 7.567 471.75 112.71 0.0000 1470.35 5.453 429.52 4688.2 0.7000 1.40118 +FS_2 Inlet.Fl_O 793.82 7.529 471.75 112.71 0.0000 1477.75 6.431 450.92 5943.4 0.4798 1.40118 +FS_21 Fan.Fl_O 793.82 10.971 530.69 126.83 0.0000 1075.59 9.528 509.71 4515.2 0.4533 1.40029 +FS_13 Splitter.Fl_O2 680.37 10.971 530.69 126.83 0.0000 921.86 9.459 508.66 3795.6 0.4650 1.40029 +FS_22 Splitter.Fl_O1 113.46 10.971 530.69 126.83 0.0000 153.73 9.852 514.60 719.5 0.3951 1.40029 +FS_23 Duct1.Fl_O 113.46 10.944 530.69 126.83 0.0000 154.11 9.827 514.60 721.3 0.3951 1.40029 +FS_24 LPC.Fl_O 113.46 23.259 679.67 162.66 0.0000 82.06 20.606 656.67 366.0 0.4199 1.39672 +FS_25 Duct2.Fl_O 113.46 23.201 679.67 162.66 0.0000 82.27 20.554 656.67 366.9 0.4199 1.39672 +FS_3 HPC.Fl_O 113.46 120.343 1136.98 275.32 0.0000 20.51 112.814 1117.21 119.9 0.3081 1.37211 +FS_36 Bld3.Fl_O 103.25 120.343 1136.98 275.32 0.0000 18.67 112.814 1117.21 109.1 0.3081 1.37211 +FS_4 Burner.Fl_O 104.83 113.725 2119.21 547.73 0.0153 27.38 112.993 2115.95 483.4 0.0992 1.31328 +FS_45 HPT.Fl_O 115.04 41.753 1640.40 412.44 0.0140 72.01 39.364 1616.38 439.1 0.2982 1.33339 +FS_48 Duct3.Fl_O 115.04 41.544 1640.40 412.44 0.0140 72.37 39.167 1616.38 441.4 0.2982 1.33339 +FS_5 LPT.Fl_O 115.04 8.792 1141.54 279.67 0.0140 285.27 8.075 1115.96 1477.4 0.3552 1.36224 +FS_7 Duct4.Fl_O 115.04 8.704 1141.54 279.67 0.0140 288.15 8.334 1128.40 2018.9 0.2533 1.36224 +FS_9 Core_Nozz.Fl_O 115.04 8.704 1141.54 279.67 0.0140 288.15 5.453 1006.80 862.9 0.8531 1.36224 +FS_15 BypBld.Fl_O 680.37 10.971 530.69 126.83 0.0000 921.86 9.459 508.66 3795.6 0.4650 1.40029 +FS_17 Duct5.Fl_O 680.37 10.889 530.69 126.83 0.0000 928.82 9.388 508.66 3824.3 0.4650 1.40029 +FS_19 Byp_Nozz.Fl_O 680.37 10.889 530.69 126.83 0.0000 928.82 5.750 442.04 2706.3 1.0000 1.40029 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1477.75 1.457 0.9105 3359.813 1.1249 0.9152 -15860.3 39.72 19.77 +LPC 154.11 2.125 0.8544 3167.754 1.2807 0.8690 -5750.7 25.28 16.62 +HPC 82.27 5.187 0.8659 6253.343 1.6728 0.8922 -18085.5 26.26 26.42 +HPT 27.38 2.724 0.9149 155.500 1.2464 0.9046 18085.7 +LPT 72.37 4.725 0.9214 79.113 1.4370 0.9050 21611.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2833.35 1.318 0.9406 0.852 2.0410 0.5215 1.4369 0.9679 3943.9586 +LPC 165.30 1.345 0.8900 0.865 1.6238 0.9323 3.2631 0.9600 3662.6571 +HPC 195.57 20.356 0.8542 0.984 2.1328 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.057 0.9332 101.560 5.0570 1.4085 0.4249 0.9803 1.5311 +LPT 150.38 6.196 0.9202 97.537 6.1963 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4688.16 17554.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 842.12 202.09 37.432 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 842.12 202.09 37.432 +Duct1 0.0025 0.3951 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 842.12 202.09 37.432 +Duct2 0.0025 0.4199 365.99 +Duct3 0.0050 0.2982 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3552 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.9710 1136.98 275.32 120.343 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.2402 1136.98 275.32 120.343 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 530.69 126.83 10.971 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9967 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7158.4 13269.4 18085.7 +LP_Shaft 3204.2 35423.1 21611.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2119.21 0.9940 0.0550 1.58477 0.01535 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.997 0.9976 1.0000 0.9975 2706.36 1.000 1028.6 22552.4 +Core_Nozz 1.596 0.9999 1.0000 0.9999 862.88 0.853 1312.9 4694.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 250 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 25000.0 0.00 726.57 6461.3 0.6190 3999.35 6.7097 711.51 12.519 1909.6 1864.7 1469.6 + core size:20.90 Q: 269.61 Maximum Thrust: 16153.0 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 726.57 7.567 471.75 112.71 0.0000 1345.79 5.453 429.52 4291.0 0.7000 1.40118 +FS_2 Inlet.Fl_O 726.57 7.529 471.75 112.71 0.0000 1352.56 6.640 455.08 5943.4 0.4272 1.40118 +FS_21 Fan.Fl_O 726.57 10.069 516.74 123.49 0.0000 1058.51 8.794 497.11 4515.2 0.4439 1.40055 +FS_13 Splitter.Fl_O2 632.33 10.069 516.74 123.49 0.0000 921.21 8.684 495.32 3795.6 0.4645 1.40055 +FS_22 Splitter.Fl_O1 94.24 10.069 516.74 123.49 0.0000 137.30 9.271 504.68 719.5 0.3453 1.40055 +FS_23 Duct1.Fl_O 94.24 10.044 516.74 123.49 0.0000 137.64 9.248 504.68 721.3 0.3453 1.40055 +FS_24 LPC.Fl_O 94.24 19.432 643.55 153.95 0.0000 79.39 17.378 623.39 366.0 0.4028 1.39803 +FS_25 Duct2.Fl_O 94.24 19.383 643.55 153.95 0.0000 79.59 17.334 623.39 366.9 0.4028 1.39803 +FS_3 HPC.Fl_O 94.24 94.731 1060.38 256.05 0.0000 20.90 88.559 1040.98 119.9 0.3141 1.37693 +FS_36 Bld3.Fl_O 85.76 94.731 1060.38 256.05 0.0000 19.02 88.559 1040.98 109.1 0.3141 1.37693 +FS_4 Burner.Fl_O 86.87 89.520 1909.60 486.74 0.0130 27.36 88.945 1906.60 483.4 0.0988 1.32226 +FS_45 HPT.Fl_O 95.35 32.556 1469.61 365.31 0.0118 72.45 30.670 1447.32 439.1 0.2991 1.34364 +FS_48 Duct3.Fl_O 95.35 32.393 1469.61 365.31 0.0118 72.82 30.516 1447.32 441.4 0.2991 1.34364 +FS_5 LPT.Fl_O 95.35 7.520 1039.34 253.08 0.0118 263.79 7.004 1019.54 1477.4 0.3235 1.37025 +FS_7 Duct4.Fl_O 95.35 7.444 1039.34 253.08 0.0118 266.46 7.176 1029.05 2018.9 0.2322 1.37025 +FS_9 Core_Nozz.Fl_O 95.35 7.444 1039.34 253.08 0.0118 266.46 5.453 955.00 862.9 0.6874 1.37025 +FS_15 BypBld.Fl_O 632.33 10.069 516.74 123.49 0.0000 921.21 8.684 495.32 3795.6 0.4645 1.40055 +FS_17 Duct5.Fl_O 632.33 9.993 516.74 123.49 0.0000 928.17 8.619 495.32 3824.3 0.4645 1.40055 +FS_19 Byp_Nozz.Fl_O 632.33 9.993 516.74 123.49 0.0000 928.17 5.453 434.48 2706.3 0.9715 1.40055 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1352.56 1.337 0.9096 3025.910 1.0954 0.9133 -11078.5 47.66 21.58 +LPC 137.64 1.935 0.8449 2891.192 1.2454 0.8585 -4061.4 23.58 13.41 +HPC 79.59 4.887 0.8648 6207.126 1.6477 0.8907 -13613.9 30.80 31.03 +HPT 27.36 2.750 0.9154 158.221 1.2557 0.9049 13613.9 +LPT 72.82 4.308 0.9175 75.278 1.4140 0.9013 15140.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2593.36 1.235 0.9397 0.767 2.0827 0.5215 1.4369 0.9679 3943.9586 +LPC 147.63 1.286 0.8800 0.789 1.5594 0.9323 3.2631 0.9600 3662.6571 +HPC 189.21 18.970 0.8531 0.976 2.1681 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.118 0.9338 103.337 5.1182 1.4085 0.4249 0.9803 1.5311 +LPT 151.30 5.614 0.9164 92.808 5.6143 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4290.99 16067.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 791.24 189.68 30.421 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 791.24 189.68 30.421 +Duct1 0.0025 0.3453 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 791.24 189.68 30.421 +Duct2 0.0025 0.4028 365.99 +Duct3 0.0050 0.2991 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3235 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.2984 1060.38 256.05 94.731 +Duct5 0.0075 0.4645 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.1833 1060.38 256.05 94.731 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 516.74 123.49 10.069 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.7097 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6914.1 10341.5 13613.9 +LP_Shaft 2885.8 27555.4 15140.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1909.60 0.9940 0.0550 1.11093 0.01295 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.832 0.9975 1.0000 0.9975 2706.36 0.971 990.7 19470.0 +Core_Nozz 1.365 0.9999 1.0000 0.9999 862.88 0.687 1032.2 3059.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 251 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 25000.0 0.00 641.76 3230.6 0.7385 2385.94 7.8632 711.51 8.897 1639.5 1603.0 1252.1 + core size:21.49 Q: 269.61 Maximum Thrust: 16153.0 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 641.76 7.567 471.75 112.71 0.0000 1188.69 5.453 429.52 3790.1 0.7000 1.40118 +FS_2 Inlet.Fl_O 641.76 7.529 471.75 112.71 0.0000 1194.68 6.859 459.34 5943.4 0.3670 1.40118 +FS_21 Fan.Fl_O 641.76 9.042 500.29 119.55 0.0000 1024.44 7.982 482.75 4515.2 0.4256 1.40082 +FS_13 Splitter.Fl_O2 569.35 9.042 500.29 119.55 0.0000 908.85 7.838 480.24 3795.6 0.4563 1.40082 +FS_22 Splitter.Fl_O1 72.41 9.042 500.29 119.55 0.0000 115.58 8.548 492.32 719.5 0.2842 1.40082 +FS_23 Duct1.Fl_O 72.41 9.019 500.29 119.55 0.0000 115.87 8.527 492.32 721.3 0.2842 1.40082 +FS_24 LPC.Fl_O 72.41 15.111 595.72 142.45 0.0000 75.47 13.688 579.15 366.0 0.3786 1.39911 +FS_25 Duct2.Fl_O 72.41 15.073 595.72 142.45 0.0000 75.66 13.654 579.15 366.9 0.3786 1.39911 +FS_3 HPC.Fl_O 72.41 67.319 958.41 230.67 0.0000 21.49 62.665 939.55 119.9 0.3233 1.38329 +FS_36 Bld3.Fl_O 65.89 67.319 958.41 230.67 0.0000 19.55 62.665 939.55 109.1 0.3233 1.38329 +FS_4 Burner.Fl_O 66.55 63.616 1639.49 410.56 0.0101 27.33 63.208 1636.84 483.4 0.0982 1.33612 +FS_45 HPT.Fl_O 73.07 22.858 1252.10 307.10 0.0092 72.99 21.513 1232.20 439.1 0.2998 1.35844 +FS_48 Duct3.Fl_O 73.07 22.744 1252.10 307.10 0.0092 73.36 21.406 1232.20 441.4 0.2998 1.35844 +FS_5 LPT.Fl_O 73.07 6.547 927.00 224.37 0.0092 219.28 6.245 915.02 1477.4 0.2626 1.37912 +FS_7 Duct4.Fl_O 73.07 6.481 927.00 224.37 0.0092 221.49 6.322 920.66 2018.9 0.1904 1.37912 +FS_9 Core_Nozz.Fl_O 73.07 6.481 927.00 224.37 0.0092 221.49 5.453 883.95 862.9 0.5057 1.37912 +FS_15 BypBld.Fl_O 569.35 9.042 500.29 119.55 0.0000 908.85 7.838 480.24 3795.6 0.4563 1.40082 +FS_17 Duct5.Fl_O 569.35 8.974 500.29 119.55 0.0000 915.72 7.779 480.24 3824.3 0.4563 1.40082 +FS_19 Byp_Nozz.Fl_O 569.35 8.974 500.29 119.55 0.0000 915.72 5.453 433.80 2706.4 0.8740 1.40082 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1194.68 1.201 0.8893 2558.381 1.0605 0.8922 -6206.6 57.75 23.53 +LPC 115.87 1.675 0.8332 2484.334 1.1908 0.8448 -2345.9 24.71 10.29 +HPC 75.66 4.466 0.8628 6133.355 1.6088 0.8878 -9038.1 37.84 38.37 +HPT 27.33 2.783 0.9163 162.338 1.2688 0.9053 9038.1 +LPT 73.36 3.474 0.9104 68.954 1.3507 0.8951 8552.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2290.63 1.140 0.9187 0.649 2.2513 0.5215 1.4369 0.9679 3943.9586 +LPC 124.29 1.207 0.8679 0.678 1.5361 0.9323 3.2631 0.9600 3662.6571 +HPC 179.87 17.023 0.8512 0.965 2.2416 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.197 0.9347 106.026 5.1968 1.4085 0.4249 0.9803 1.5311 +LPT 152.43 4.451 0.9092 85.011 4.4510 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3790.10 14192.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 723.81 173.32 22.727 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 723.81 173.32 22.727 +Duct1 0.0025 0.2842 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 723.81 173.32 22.727 +Duct2 0.0025 0.3786 365.99 +Duct3 0.0050 0.2998 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2626 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.5342 958.41 230.67 67.319 +Duct5 0.0075 0.4563 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.9824 958.41 230.67 67.319 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 500.29 119.55 9.042 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8632 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6573.2 7221.6 9038.1 +LP_Shaft 2439.9 18410.0 8552.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1639.49 0.9940 0.0550 0.66276 0.01006 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.646 0.9975 1.0000 0.9975 2706.36 0.874 890.6 15760.0 +Core_Nozz 1.189 0.9999 1.0000 0.9999 862.88 0.506 732.1 1662.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:51 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 252 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 11/ 21/ 1/ 9 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 25000.0 0.00 555.96 807.7 1.4745 1190.88 9.6309 711.51 5.784 1331.8 1305.2 1009.3 + core size:22.39 Q: 269.61 Maximum Thrust: 16153.0 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 555.96 7.567 471.75 112.71 0.0000 1029.77 5.453 429.52 3283.4 0.7000 1.40118 +FS_2 Inlet.Fl_O 555.96 7.529 471.75 112.71 0.0000 1034.96 7.040 462.77 5943.4 0.3109 1.40118 +FS_21 Fan.Fl_O 555.96 8.161 485.68 116.05 0.0000 968.83 7.320 470.79 4515.2 0.3971 1.40102 +FS_13 Splitter.Fl_O2 503.67 8.161 485.68 116.05 0.0000 877.70 7.160 467.84 3795.6 0.4360 1.40102 +FS_22 Splitter.Fl_O1 52.30 8.161 485.68 116.05 0.0000 91.13 7.890 481.02 719.5 0.2198 1.40102 +FS_23 Duct1.Fl_O 52.30 8.140 485.68 116.05 0.0000 91.36 7.871 481.02 721.3 0.2198 1.40102 +FS_24 LPC.Fl_O 52.30 11.371 545.08 130.29 0.0000 69.29 10.486 532.60 366.0 0.3422 1.40000 +FS_25 Duct2.Fl_O 52.30 11.343 545.08 130.29 0.0000 69.46 10.459 532.60 366.9 0.3422 1.40000 +FS_3 HPC.Fl_O 52.30 43.765 843.22 202.36 0.0000 22.39 40.456 824.81 119.9 0.3381 1.38990 +FS_36 Bld3.Fl_O 47.59 43.765 843.22 202.36 0.0000 20.38 40.456 824.81 109.1 0.3381 1.38990 +FS_4 Burner.Fl_O 47.92 41.358 1331.79 327.25 0.0070 27.29 41.094 1329.56 483.4 0.0973 1.35501 +FS_45 HPT.Fl_O 52.63 14.700 1009.26 244.46 0.0063 73.39 13.826 992.48 439.1 0.2997 1.37580 +FS_48 Duct3.Fl_O 52.63 14.627 1009.26 244.46 0.0063 73.76 13.757 992.48 441.4 0.2997 1.37580 +FS_5 LPT.Fl_O 52.63 5.974 810.14 195.07 0.0063 161.80 5.827 804.53 1477.4 0.1895 1.38744 +FS_7 Duct4.Fl_O 52.63 5.914 810.14 195.07 0.0063 163.44 5.836 807.13 2018.9 0.1387 1.38744 +FS_9 Core_Nozz.Fl_O 52.63 5.914 810.14 195.07 0.0063 163.44 5.453 791.96 862.8 0.3440 1.38744 +FS_15 BypBld.Fl_O 503.67 8.161 485.68 116.05 0.0000 877.70 7.160 467.84 3795.6 0.4360 1.40102 +FS_17 Duct5.Fl_O 503.67 8.099 485.68 116.05 0.0000 884.33 7.107 467.84 3824.3 0.4360 1.40102 +FS_19 Byp_Nozz.Fl_O 503.67 8.099 485.68 116.05 0.0000 884.33 5.453 433.67 2706.4 0.7731 1.40102 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1034.96 1.084 0.7900 1986.934 1.0295 0.7925 -2624.2 83.21 24.29 +LPC 91.36 1.397 0.8204 1958.229 1.1223 0.8288 -1053.4 30.82 8.57 +HPC 69.46 3.858 0.8538 6019.883 1.5470 0.8784 -5332.7 49.65 50.65 +HPT 27.29 2.813 0.9179 169.104 1.2848 0.9066 5332.7 +LPT 73.76 2.448 0.8999 59.648 1.2458 0.8881 3677.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1984.39 1.058 0.8162 0.504 2.6184 0.5215 1.4369 0.9679 3943.9586 +LPC 98.00 1.122 0.8546 0.535 1.5983 0.9323 3.2631 0.9600 3662.6571 +HPC 165.14 14.214 0.8423 0.947 2.3800 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.268 0.9363 110.445 5.2680 1.4085 0.4249 0.9803 1.5311 +LPT 153.26 3.021 0.8987 73.538 3.0206 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3283.39 12294.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 650.03 155.51 16.093 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 650.03 155.51 16.093 +Duct1 0.0025 0.2198 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 650.03 155.51 16.093 +Duct2 0.0025 0.3422 365.99 +Duct3 0.0050 0.2997 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1895 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.8304 843.22 202.36 43.765 +Duct5 0.0075 0.4360 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.8763 843.22 202.36 43.765 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 485.68 116.05 8.161 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.6309 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6171.2 4538.5 5332.7 +LP_Shaft 1894.9 10193.2 3677.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1331.79 0.9940 0.0550 0.33080 0.00695 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.485 0.9975 1.0000 0.9975 2706.36 0.773 787.6 12329.6 +Core_Nozz 1.085 0.9999 1.0000 0.9999 862.88 0.344 472.5 772.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 253 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 25000.0 0.00 935.98 16497.6 0.6206 10238.08 5.0407 762.33 22.703 2519.6 2455.7 1971.2 + core size:19.92 Q: 309.50 Maximum Thrust: 16497.6 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 935.98 7.923 478.00 114.21 0.0000 1666.72 5.453 429.52 5159.2 0.7500 1.40112 +FS_2 Inlet.Fl_O 935.98 7.883 478.00 114.21 0.0000 1675.11 6.293 448.13 5943.4 0.5763 1.40112 +FS_21 Fan.Fl_O 935.98 12.963 562.24 134.40 0.0000 1104.76 11.144 538.47 4515.2 0.4697 1.39967 +FS_13 Splitter.Fl_O2 781.04 12.963 562.24 134.40 0.0000 921.88 11.177 538.92 3795.6 0.4651 1.39967 +FS_22 Splitter.Fl_O1 154.94 12.963 562.24 134.40 0.0000 182.88 10.966 536.00 719.5 0.4947 1.39967 +FS_23 Duct1.Fl_O 154.94 12.931 562.24 134.40 0.0000 183.34 10.938 536.00 721.3 0.4947 1.39967 +FS_24 LPC.Fl_O 154.94 32.183 753.98 180.63 0.0000 85.31 28.161 726.02 366.0 0.4416 1.39410 +FS_25 Duct2.Fl_O 154.94 32.103 753.98 180.63 0.0000 85.52 28.090 726.02 366.9 0.4416 1.39410 +FS_3 HPC.Fl_O 154.94 179.864 1283.87 312.79 0.0000 19.92 169.297 1263.31 119.9 0.2991 1.36289 +FS_36 Bld3.Fl_O 141.00 179.864 1283.87 312.79 0.0000 18.13 169.297 1263.31 109.1 0.2991 1.36289 +FS_4 Burner.Fl_O 143.84 169.972 2519.61 668.32 0.0202 27.41 168.875 2515.86 483.4 0.0998 1.29957 +FS_45 HPT.Fl_O 157.79 63.755 1971.17 507.12 0.0184 70.91 60.223 1944.33 439.1 0.2951 1.31625 +FS_48 Duct3.Fl_O 157.79 63.436 1971.17 507.12 0.0184 71.26 59.922 1944.33 441.4 0.2951 1.31625 +FS_5 LPT.Fl_O 157.79 13.037 1374.25 341.93 0.0184 289.53 11.936 1343.48 1477.4 0.3639 1.34474 +FS_7 Duct4.Fl_O 157.79 12.906 1374.25 341.93 0.0184 292.46 12.339 1358.50 2018.9 0.2591 1.34474 +FS_9 Core_Nozz.Fl_O 157.79 12.906 1374.25 341.93 0.0184 292.46 6.906 1168.17 862.9 1.0000 1.34474 +FS_15 BypBld.Fl_O 781.04 12.963 562.24 134.40 0.0000 921.88 11.177 538.92 3795.6 0.4651 1.39967 +FS_17 Duct5.Fl_O 781.04 12.866 562.24 134.40 0.0000 928.84 11.093 538.92 3824.3 0.4651 1.39967 +FS_19 Byp_Nozz.Fl_O 781.04 12.866 562.24 134.40 0.0000 928.84 6.794 468.38 2706.3 1.0000 1.39967 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.644 0.8675 3944.235 1.1762 0.8765 -26744.1 24.72 17.46 +LPC 183.34 2.489 0.8683 3636.770 1.3410 0.8838 -10134.5 28.35 23.27 +HPC 85.52 5.603 0.8652 6324.696 1.7028 0.8922 -28972.9 20.17 20.23 +HPT 27.41 2.666 0.9135 151.917 1.2305 0.9037 28973.3 +LPT 71.26 4.866 0.9326 85.284 1.4344 0.9187 36878.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8962 1.000 2.3711 0.5215 1.4369 0.9679 3943.9586 +LPC 196.66 1.456 0.9045 0.993 1.7658 0.9323 3.2631 0.9600 3662.6571 +HPC 203.30 22.278 0.8535 0.995 2.0435 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.921 0.9318 99.220 4.9212 1.4085 0.4249 0.9803 1.5311 +LPT 148.07 6.393 0.9314 105.145 6.3930 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5159.19 22177.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 943.11 226.89 53.750 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 943.11 226.89 53.750 +Duct1 0.0025 0.4947 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 943.11 226.89 53.750 +Duct2 0.0025 0.4416 365.99 +Duct3 0.0050 0.2951 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3639 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.4231 1283.87 312.79 179.864 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.5219 1283.87 312.79 179.864 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 562.24 134.40 12.963 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0407 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7625.6 19955.4 28973.3 +LP_Shaft 3786.4 51153.9 36878.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2519.61 0.9940 0.0550 2.84391 0.02017 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.359 0.9968 1.0000 0.9975 2706.36 1.000 1058.7 29330.5 +Core_Nozz 2.367 0.9986 1.0000 0.9999 862.88 1.000 1649.7 9344.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 254 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 25000.0 0.00 912.33 14847.5 0.6097 9052.61 5.3070 762.33 20.793 2429.0 2367.7 1893.8 + core size:20.01 Q: 309.50 Maximum Thrust: 16497.6 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 912.33 7.923 478.00 114.21 0.0000 1624.61 5.453 429.52 5028.9 0.7500 1.40112 +FS_2 Inlet.Fl_O 912.33 7.883 478.00 114.21 0.0000 1632.79 6.399 450.30 5943.4 0.5537 1.40112 +FS_21 Fan.Fl_O 912.33 12.669 555.83 132.87 0.0000 1095.60 10.927 532.83 4515.2 0.4645 1.39979 +FS_13 Splitter.Fl_O2 767.68 12.669 555.83 132.87 0.0000 921.89 10.923 532.77 3795.6 0.4651 1.39979 +FS_22 Splitter.Fl_O1 144.65 12.669 555.83 132.87 0.0000 173.71 10.948 533.13 719.5 0.4614 1.39979 +FS_23 Duct1.Fl_O 144.65 12.637 555.83 132.87 0.0000 174.15 10.920 533.13 721.3 0.4614 1.39979 +FS_24 LPC.Fl_O 144.65 29.460 730.73 175.00 0.0000 85.65 25.743 703.33 366.0 0.4438 1.39499 +FS_25 Duct2.Fl_O 144.65 29.386 730.73 175.00 0.0000 85.87 25.679 703.33 366.9 0.4438 1.39499 +FS_3 HPC.Fl_O 144.65 164.735 1247.23 303.38 0.0000 20.01 154.960 1226.96 119.9 0.3004 1.36518 +FS_36 Bld3.Fl_O 131.64 164.735 1247.23 303.38 0.0000 18.21 154.960 1226.96 109.1 0.3004 1.36518 +FS_4 Burner.Fl_O 134.15 155.674 2429.04 640.63 0.0191 27.41 154.671 2425.39 483.4 0.0997 1.30233 +FS_45 HPT.Fl_O 147.17 57.815 1893.76 484.61 0.0174 71.48 54.557 1867.30 439.1 0.2974 1.31986 +FS_48 Duct3.Fl_O 147.17 57.526 1893.76 484.61 0.0174 71.84 54.284 1867.30 441.4 0.2974 1.31986 +FS_5 LPT.Fl_O 147.17 11.913 1321.30 327.54 0.0174 289.77 10.906 1291.42 1477.4 0.3637 1.34860 +FS_7 Duct4.Fl_O 147.17 11.794 1321.30 327.54 0.0174 292.70 11.275 1306.00 2018.9 0.2590 1.34860 +FS_9 Core_Nozz.Fl_O 147.17 11.794 1321.30 327.54 0.0174 292.70 6.303 1121.36 862.9 1.0000 1.34860 +FS_15 BypBld.Fl_O 767.68 12.669 555.83 132.87 0.0000 921.89 10.923 532.77 3795.6 0.4651 1.39979 +FS_17 Duct5.Fl_O 767.68 12.574 555.83 132.87 0.0000 928.85 10.841 532.77 3824.3 0.4651 1.39979 +FS_19 Byp_Nozz.Fl_O 767.68 12.574 555.83 132.87 0.0000 928.85 6.640 463.03 2706.4 1.0000 1.39979 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1632.79 1.607 0.8926 3741.691 1.1628 0.8996 -24083.8 28.23 17.74 +LPC 174.15 2.331 0.8659 3469.837 1.3147 0.8808 -8623.2 28.79 22.09 +HPC 85.87 5.606 0.8642 6333.274 1.7068 0.8914 -26275.4 20.60 20.64 +HPT 27.41 2.693 0.9140 152.526 1.2352 0.9042 26275.5 +LPT 71.84 4.829 0.9281 82.542 1.4333 0.9132 32705.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3130.49 1.422 0.9221 0.949 2.1746 0.5215 1.4369 0.9679 3943.9586 +LPC 186.79 1.408 0.9020 0.947 1.7496 0.9323 3.2631 0.9600 3662.6571 +HPC 204.13 22.292 0.8526 0.996 2.0711 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.984 0.9323 99.617 4.9838 1.4085 0.4249 0.9803 1.5311 +LPT 149.27 6.341 0.9269 101.763 6.3413 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5028.85 21616.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 914.90 219.93 49.215 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 914.90 219.93 49.215 +Duct1 0.0025 0.4614 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 914.90 219.93 49.215 +Duct2 0.0025 0.4438 365.99 +Duct3 0.0050 0.2974 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3637 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.0629 1247.23 303.38 164.735 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.9560 1247.23 303.38 164.735 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 555.83 132.87 12.669 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3070 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7517.3 18358.0 26275.5 +LP_Shaft 3592.0 47821.3 32705.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2429.04 0.9940 0.0550 2.51461 0.01910 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.306 0.9971 1.0000 0.9975 2706.36 1.000 1052.7 28328.3 +Core_Nozz 2.163 0.9995 1.0000 0.9999 862.88 1.000 1618.4 8136.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 255 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 25000.0 0.00 885.69 13198.1 0.6050 7984.50 5.5128 762.33 19.153 2335.8 2277.5 1816.6 + core size:20.17 Q: 309.50 Maximum Thrust: 16497.6 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 885.69 7.923 478.00 114.21 0.0000 1577.16 5.453 429.52 4882.0 0.7500 1.40112 +FS_2 Inlet.Fl_O 885.69 7.883 478.00 114.21 0.0000 1585.10 6.511 452.53 5943.4 0.5296 1.40112 +FS_21 Fan.Fl_O 885.69 12.307 549.98 131.46 0.0000 1089.10 10.639 527.56 4515.2 0.4608 1.39991 +FS_13 Splitter.Fl_O2 749.70 12.307 549.98 131.46 0.0000 921.88 10.611 527.16 3795.6 0.4651 1.39991 +FS_22 Splitter.Fl_O1 135.99 12.307 549.98 131.46 0.0000 167.22 10.780 529.56 719.5 0.4390 1.39991 +FS_23 Duct1.Fl_O 135.99 12.276 549.98 131.46 0.0000 167.64 10.753 529.56 721.3 0.4390 1.39991 +FS_24 LPC.Fl_O 135.99 27.709 716.30 171.51 0.0000 84.76 24.299 690.10 366.0 0.4378 1.39547 +FS_25 Duct2.Fl_O 135.99 27.639 716.30 171.51 0.0000 84.97 24.238 690.10 366.9 0.4378 1.39547 +FS_3 HPC.Fl_O 135.99 151.743 1216.02 295.40 0.0000 20.17 142.590 1195.85 119.9 0.3028 1.36714 +FS_36 Bld3.Fl_O 123.75 151.743 1216.02 295.40 0.0000 18.35 142.590 1195.85 109.1 0.3028 1.36714 +FS_4 Burner.Fl_O 125.97 143.397 2335.79 612.32 0.0179 27.40 142.473 2332.26 483.4 0.0995 1.30549 +FS_45 HPT.Fl_O 138.21 52.998 1816.62 462.35 0.0163 71.72 49.990 1790.81 439.1 0.2980 1.32376 +FS_48 Duct3.Fl_O 138.21 52.733 1816.62 462.35 0.0163 72.08 49.740 1790.81 441.4 0.2980 1.32376 +FS_5 LPT.Fl_O 138.21 10.934 1264.99 312.38 0.0163 290.11 10.008 1236.07 1477.4 0.3636 1.35282 +FS_7 Duct4.Fl_O 138.21 10.825 1264.99 312.38 0.0163 293.04 10.347 1250.19 2018.9 0.2589 1.35282 +FS_9 Core_Nozz.Fl_O 138.21 10.825 1264.99 312.38 0.0163 293.04 5.778 1071.73 862.9 1.0000 1.35282 +FS_15 BypBld.Fl_O 749.70 12.307 549.98 131.46 0.0000 921.88 10.611 527.16 3795.6 0.4651 1.39991 +FS_17 Duct5.Fl_O 749.70 12.214 549.98 131.46 0.0000 928.84 10.531 527.16 3824.3 0.4651 1.39991 +FS_19 Byp_Nozz.Fl_O 749.70 12.214 549.98 131.46 0.0000 928.84 6.450 458.14 2706.4 1.0000 1.39991 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1585.10 1.561 0.9024 3612.782 1.1506 0.9084 -21620.8 31.71 18.33 +LPC 167.64 2.257 0.8630 3368.066 1.3024 0.8777 -7704.9 27.95 20.40 +HPC 84.97 5.490 0.8649 6310.434 1.6977 0.8918 -23838.1 22.23 22.32 +HPT 27.40 2.706 0.9145 153.442 1.2389 0.9046 23837.9 +LPT 72.08 4.823 0.9261 81.372 1.4361 0.9106 29326.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3039.24 1.391 0.9323 0.916 2.0961 0.5215 1.4369 0.9679 3943.9586 +LPC 179.82 1.385 0.8989 0.920 1.7134 0.9323 3.2631 0.9600 3662.6571 +HPC 202.01 21.757 0.8533 0.993 2.0967 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.015 0.9329 100.215 5.0146 1.4085 0.4249 0.9803 1.5311 +LPT 149.78 6.333 0.9249 100.322 6.3328 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4881.97 20985.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 894.29 214.87 45.821 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 894.29 214.87 45.821 +Duct1 0.0025 0.4390 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 894.29 214.87 45.821 +Duct2 0.0025 0.4378 365.99 +Duct3 0.0050 0.2980 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.7597 1216.02 295.40 151.743 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.4795 1216.02 295.40 151.743 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 549.98 131.46 12.307 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5128 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7415.8 16882.7 23837.9 +LP_Shaft 3468.2 44409.7 29326.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2335.79 0.9940 0.0550 2.21792 0.01792 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.240 0.9973 1.0000 0.9975 2706.36 1.000 1047.1 27096.5 +Core_Nozz 1.985 0.9998 1.0000 0.9999 862.88 1.000 1584.5 7087.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 256 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 25000.0 0.00 827.20 9898.5 0.6095 6032.97 5.9923 762.33 15.939 2145.0 2093.0 1661.6 + core size:20.52 Q: 309.50 Maximum Thrust: 16497.6 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 827.20 7.923 478.00 114.21 0.0000 1473.02 5.453 429.52 4559.6 0.7500 1.40112 +FS_2 Inlet.Fl_O 827.20 7.883 478.00 114.21 0.0000 1480.43 6.728 456.80 5943.4 0.4810 1.40112 +FS_21 Fan.Fl_O 827.20 11.510 538.04 128.60 0.0000 1075.71 9.996 516.78 4515.2 0.4534 1.40015 +FS_13 Splitter.Fl_O2 708.90 11.510 538.04 128.60 0.0000 921.87 9.924 515.71 3795.6 0.4650 1.40015 +FS_22 Splitter.Fl_O1 118.30 11.510 538.04 128.60 0.0000 153.84 10.333 521.71 719.5 0.3955 1.40015 +FS_23 Duct1.Fl_O 118.30 11.481 538.04 128.60 0.0000 154.23 10.308 521.71 721.3 0.3955 1.40015 +FS_24 LPC.Fl_O 118.30 24.479 689.78 165.10 0.0000 81.91 21.698 666.56 366.0 0.4190 1.39636 +FS_25 Duct2.Fl_O 118.30 24.417 689.78 165.10 0.0000 82.11 21.644 666.56 366.9 0.4190 1.39636 +FS_3 HPC.Fl_O 118.30 126.276 1152.11 279.15 0.0000 20.52 118.369 1132.10 119.9 0.3083 1.37116 +FS_36 Bld3.Fl_O 107.66 126.276 1152.11 279.15 0.0000 18.67 118.369 1132.10 109.1 0.3083 1.37116 +FS_4 Burner.Fl_O 109.33 119.331 2145.04 555.30 0.0156 27.38 118.563 2141.74 483.4 0.0992 1.31234 +FS_45 HPT.Fl_O 119.98 43.836 1661.57 418.33 0.0142 71.99 41.329 1637.31 439.1 0.2983 1.33224 +FS_48 Duct3.Fl_O 119.98 43.617 1661.57 418.33 0.0142 72.35 41.123 1637.31 441.4 0.2983 1.33224 +FS_5 LPT.Fl_O 119.98 9.142 1154.78 283.13 0.0142 287.78 8.382 1128.44 1477.4 0.3590 1.36126 +FS_7 Duct4.Fl_O 119.98 9.051 1154.78 283.13 0.0142 290.69 8.658 1141.27 2018.9 0.2558 1.36126 +FS_9 Core_Nozz.Fl_O 119.98 9.051 1154.78 283.13 0.0142 290.69 5.453 1008.05 862.9 0.8903 1.36126 +FS_15 BypBld.Fl_O 708.90 11.510 538.04 128.60 0.0000 921.87 9.924 515.71 3795.6 0.4650 1.40015 +FS_17 Duct5.Fl_O 708.90 11.424 538.04 128.60 0.0000 928.83 9.850 515.71 3824.3 0.4650 1.40015 +FS_19 Byp_Nozz.Fl_O 708.90 11.424 538.04 128.60 0.0000 928.83 6.032 448.18 2706.3 1.0000 1.40015 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1480.43 1.460 0.9105 3366.593 1.1256 0.9152 -16841.2 39.47 19.72 +LPC 154.23 2.132 0.8541 3173.179 1.2820 0.8687 -6109.5 25.07 16.50 +HPC 82.11 5.172 0.8659 6250.436 1.6703 0.8921 -19090.2 26.45 26.61 +HPT 27.38 2.722 0.9149 155.634 1.2456 0.9046 19090.5 +LPT 72.35 4.771 0.9212 79.287 1.4389 0.9047 22950.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2838.46 1.320 0.9406 0.854 2.0401 0.5215 1.4369 0.9679 3943.9586 +LPC 165.43 1.347 0.8896 0.866 1.6190 0.9323 3.2631 0.9600 3662.6571 +HPC 195.20 20.284 0.8542 0.983 2.1332 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.053 0.9332 101.647 5.0534 1.4085 0.4249 0.9803 1.5311 +LPT 150.34 6.261 0.9200 97.750 6.2605 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4559.60 19599.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 854.10 205.02 39.340 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 854.10 205.02 39.340 +Duct1 0.0025 0.3955 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 854.10 205.02 39.340 +Duct2 0.0025 0.4190 365.99 +Duct3 0.0050 0.2983 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3590 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.1406 1152.11 279.15 126.276 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.5067 1152.11 279.15 126.276 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 538.04 128.60 11.510 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9923 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7208.1 13910.1 19090.5 +LP_Shaft 3231.9 37296.7 22950.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2145.04 0.9940 0.0550 1.67582 0.01557 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.095 0.9976 1.0000 0.9975 2706.36 1.000 1035.7 24386.1 +Core_Nozz 1.660 0.9999 1.0000 0.9999 862.88 0.890 1370.9 5112.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 257 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 25000.0 0.00 758.87 6599.1 0.6417 4234.47 6.7024 762.33 12.580 1933.0 1887.7 1489.0 + core size:20.92 Q: 309.50 Maximum Thrust: 16497.6 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 758.87 7.923 478.00 114.21 0.0000 1351.33 5.453 429.52 4182.9 0.7500 1.40112 +FS_2 Inlet.Fl_O 758.87 7.883 478.00 114.21 0.0000 1358.13 6.943 460.94 5943.4 0.4295 1.40112 +FS_21 Fan.Fl_O 758.87 10.583 524.20 125.28 0.0000 1059.39 9.240 504.25 4515.2 0.4444 1.40042 +FS_13 Splitter.Fl_O2 660.34 10.583 524.20 125.28 0.0000 921.85 9.125 502.43 3795.6 0.4650 1.40042 +FS_22 Splitter.Fl_O1 98.52 10.583 524.20 125.28 0.0000 137.54 9.741 511.92 719.5 0.3460 1.40042 +FS_23 Duct1.Fl_O 98.52 10.557 524.20 125.28 0.0000 137.89 9.717 511.92 721.3 0.3460 1.40042 +FS_24 LPC.Fl_O 98.52 20.565 654.38 156.56 0.0000 79.08 18.411 634.08 366.0 0.4009 1.39766 +FS_25 Duct2.Fl_O 98.52 20.514 654.38 156.56 0.0000 79.28 18.365 634.08 366.9 0.4009 1.39766 +FS_3 HPC.Fl_O 98.52 99.666 1075.67 259.88 0.0000 20.92 93.160 1055.99 119.9 0.3145 1.37597 +FS_36 Bld3.Fl_O 89.66 99.666 1075.67 259.88 0.0000 19.04 93.160 1055.99 109.1 0.3145 1.37597 +FS_4 Burner.Fl_O 90.83 94.184 1933.05 493.43 0.0131 27.36 93.579 1930.02 483.4 0.0988 1.32124 +FS_45 HPT.Fl_O 99.70 34.285 1488.95 370.55 0.0119 72.41 32.301 1466.45 439.1 0.2990 1.34249 +FS_48 Duct3.Fl_O 99.70 34.113 1488.95 370.55 0.0119 72.77 32.139 1466.45 441.4 0.2990 1.34249 +FS_5 LPT.Fl_O 99.70 7.734 1048.32 255.39 0.0119 269.34 7.178 1027.42 1477.4 0.3314 1.36957 +FS_7 Duct4.Fl_O 99.70 7.656 1048.32 255.39 0.0119 272.06 7.368 1037.50 2018.9 0.2375 1.36957 +FS_9 Core_Nozz.Fl_O 99.70 7.656 1048.32 255.39 0.0119 272.06 5.453 956.00 862.9 0.7192 1.36957 +FS_15 BypBld.Fl_O 660.34 10.583 524.20 125.28 0.0000 921.85 9.125 502.43 3795.6 0.4650 1.40042 +FS_17 Duct5.Fl_O 660.34 10.504 524.20 125.28 0.0000 928.82 9.056 502.43 3824.3 0.4650 1.40042 +FS_19 Byp_Nozz.Fl_O 660.34 10.504 524.20 125.28 0.0000 928.82 5.546 436.62 2706.3 1.0000 1.40042 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1358.13 1.343 0.9098 3041.229 1.0966 0.9136 -11884.1 47.32 21.51 +LPC 137.89 1.948 0.8441 2904.127 1.2483 0.8579 -4360.4 23.04 13.17 +HPC 79.28 4.858 0.8647 6202.244 1.6438 0.8905 -14403.4 31.18 31.42 +HPT 27.36 2.747 0.9154 158.451 1.2548 0.9050 14403.4 +LPT 72.77 4.411 0.9168 75.662 1.4203 0.9002 16244.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2604.03 1.238 0.9400 0.771 2.0793 0.5215 1.4369 0.9679 3943.9586 +LPC 147.90 1.291 0.8792 0.793 1.5479 0.9323 3.2631 0.9600 3662.6571 +HPC 188.48 18.837 0.8531 0.976 2.1679 0.4206 0.2163 1.0137 6357.1603 +HPT 30.10 5.112 0.9338 103.487 5.1120 1.4085 0.4249 0.9803 1.5311 +LPT 151.21 5.758 0.9156 93.281 5.7582 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4182.93 17980.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 803.72 192.72 32.110 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 803.72 192.72 32.110 +Duct1 0.0025 0.3460 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 803.72 192.72 32.110 +Duct2 0.0025 0.4009 365.99 +Duct3 0.0050 0.2990 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3314 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.4483 1075.67 259.88 99.666 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.4188 1075.67 259.88 99.666 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 524.20 125.28 10.583 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.7024 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6966.5 10858.8 14403.4 +LP_Shaft 2919.6 29223.5 16244.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1933.05 0.9940 0.0550 1.17624 0.01312 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.926 0.9975 1.0000 0.9975 2706.36 1.000 1022.3 21231.7 +Core_Nozz 1.404 0.9999 1.0000 0.9999 862.88 0.719 1080.4 3348.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 258 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 25000.0 0.00 675.38 3299.7 0.7672 2531.44 7.8854 762.33 8.978 1660.4 1623.6 1269.3 + core size:21.52 Q: 309.50 Maximum Thrust: 16497.6 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 675.38 7.923 478.00 114.21 0.0000 1202.66 5.453 429.52 3722.7 0.7500 1.40112 +FS_2 Inlet.Fl_O 675.38 7.883 478.00 114.21 0.0000 1208.72 7.163 465.08 5943.4 0.3721 1.40112 +FS_21 Fan.Fl_O 675.38 9.505 507.61 121.30 0.0000 1033.01 8.369 489.45 4515.2 0.4302 1.40070 +FS_13 Splitter.Fl_O2 599.37 9.505 507.61 121.30 0.0000 916.75 8.213 486.82 3795.6 0.4615 1.40070 +FS_22 Splitter.Fl_O1 76.01 9.505 507.61 121.30 0.0000 116.26 8.980 499.42 719.5 0.2860 1.40070 +FS_23 Duct1.Fl_O 76.01 9.481 507.61 121.30 0.0000 116.55 8.958 499.42 721.3 0.2860 1.40070 +FS_24 LPC.Fl_O 76.01 16.105 607.36 145.24 0.0000 75.05 14.607 590.67 366.0 0.3762 1.39892 +FS_25 Duct2.Fl_O 76.01 16.065 607.36 145.24 0.0000 75.24 14.571 590.67 366.9 0.3762 1.39892 +FS_3 HPC.Fl_O 76.01 71.131 974.05 234.54 0.0000 21.52 66.197 954.85 119.9 0.3240 1.38232 +FS_36 Bld3.Fl_O 69.17 71.131 974.05 234.54 0.0000 19.58 66.197 954.85 109.1 0.3240 1.38232 +FS_4 Burner.Fl_O 69.87 67.219 1660.36 416.30 0.0102 27.33 66.788 1657.68 483.4 0.0982 1.33504 +FS_45 HPT.Fl_O 76.71 24.182 1269.35 311.61 0.0093 72.93 22.761 1249.26 439.1 0.2997 1.35728 +FS_48 Duct3.Fl_O 76.71 24.061 1269.35 311.61 0.0093 73.30 22.648 1249.26 441.4 0.2997 1.35728 +FS_5 LPT.Fl_O 76.71 6.661 931.23 225.44 0.0093 226.79 6.330 918.30 1477.4 0.2725 1.37879 +FS_7 Duct4.Fl_O 76.71 6.594 931.23 225.44 0.0093 229.09 6.420 924.41 2018.9 0.1973 1.37879 +FS_9 Core_Nozz.Fl_O 76.71 6.594 931.23 225.44 0.0093 229.09 5.453 883.80 862.8 0.5310 1.37879 +FS_15 BypBld.Fl_O 599.37 9.505 507.61 121.30 0.0000 916.75 8.213 486.82 3795.6 0.4615 1.40070 +FS_17 Duct5.Fl_O 599.37 9.434 507.61 121.30 0.0000 923.68 8.151 486.82 3824.3 0.4615 1.40070 +FS_19 Byp_Nozz.Fl_O 599.37 9.434 507.61 121.30 0.0000 923.68 5.453 433.90 2706.3 0.9202 1.40070 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1208.72 1.206 0.8880 2590.805 1.0619 0.8910 -6777.9 57.69 23.89 +LPC 116.55 1.699 0.8317 2514.101 1.1965 0.8438 -2574.7 23.48 9.94 +HPC 75.24 4.428 0.8627 6125.577 1.6038 0.8875 -9603.9 38.44 38.99 +HPT 27.33 2.780 0.9163 162.676 1.2677 0.9055 9604.1 +LPT 73.30 3.612 0.9112 69.809 1.3631 0.8955 9352.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2317.55 1.143 0.9174 0.657 2.2573 0.5215 1.4369 0.9679 3943.9586 +LPC 125.02 1.214 0.8664 0.686 1.5129 0.9323 3.2631 0.9600 3662.6571 +HPC 178.88 16.846 0.8511 0.964 2.2475 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.189 0.9347 106.246 5.1889 1.4085 0.4249 0.9803 1.5311 +LPT 152.31 4.644 0.9100 86.066 4.6441 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3722.74 16002.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 736.92 176.50 24.132 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 736.92 176.50 24.132 +Duct1 0.0025 0.2860 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 736.92 176.50 24.132 +Duct2 0.0025 0.3762 365.99 +Duct3 0.0050 0.2997 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2725 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.6604 974.05 234.54 71.131 +Duct5 0.0075 0.4615 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.1806 974.05 234.54 71.131 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 507.61 121.30 9.505 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8854 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6628.6 7609.7 9604.1 +LP_Shaft 2487.2 19749.6 9352.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1660.36 0.9940 0.0550 0.70318 0.01017 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.730 0.9975 1.0000 0.9975 2706.36 0.920 937.8 17469.5 +Core_Nozz 1.209 0.9999 1.0000 0.9999 862.88 0.531 768.6 1832.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 259 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 12/ 32/ 2/ 9 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 25000.0 0.00 591.24 824.9 1.5466 1275.77 9.7085 762.33 5.881 1353.9 1327.0 1027.0 + core size:22.42 Q: 309.50 Maximum Thrust: 16497.6 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 591.24 7.923 478.00 114.21 0.0000 1052.82 5.453 429.52 3258.9 0.7500 1.40112 +FS_2 Inlet.Fl_O 591.24 7.883 478.00 114.21 0.0000 1058.12 7.346 468.45 5943.4 0.3188 1.40112 +FS_21 Fan.Fl_O 591.24 8.574 492.81 117.76 0.0000 987.79 7.650 476.99 4515.2 0.4067 1.40092 +FS_13 Splitter.Fl_O2 536.02 8.574 492.81 117.76 0.0000 895.54 7.472 473.78 3795.6 0.4475 1.40092 +FS_22 Splitter.Fl_O1 55.21 8.574 492.81 117.76 0.0000 92.24 8.283 487.96 719.5 0.2226 1.40092 +FS_23 Duct1.Fl_O 55.21 8.553 492.81 117.76 0.0000 92.47 8.262 487.96 721.3 0.2226 1.40092 +FS_24 LPC.Fl_O 55.21 12.181 556.85 133.11 0.0000 69.02 11.241 544.22 366.0 0.3407 1.39977 +FS_25 Duct2.Fl_O 55.21 12.151 556.85 133.11 0.0000 69.19 11.213 544.22 366.9 0.3407 1.39977 +FS_3 HPC.Fl_O 55.21 46.595 859.65 206.38 0.0000 22.42 43.061 840.86 119.9 0.3387 1.38910 +FS_36 Bld3.Fl_O 50.24 46.595 859.65 206.38 0.0000 20.40 43.061 840.86 109.1 0.3387 1.38910 +FS_4 Burner.Fl_O 50.60 44.032 1353.88 333.07 0.0071 27.28 43.751 1351.61 483.4 0.0973 1.35360 +FS_45 HPT.Fl_O 55.57 15.662 1027.02 248.94 0.0064 73.37 14.731 1009.99 439.1 0.2997 1.37461 +FS_48 Duct3.Fl_O 55.57 15.584 1027.02 248.94 0.0064 73.74 14.657 1009.99 441.4 0.2997 1.37461 +FS_5 LPT.Fl_O 55.57 6.030 813.63 195.94 0.0064 169.61 5.867 807.42 1477.4 0.1991 1.38721 +FS_7 Duct4.Fl_O 55.57 5.970 813.63 195.94 0.0064 171.33 5.883 810.30 2018.9 0.1456 1.38721 +FS_9 Core_Nozz.Fl_O 55.57 5.970 813.63 195.94 0.0064 171.33 5.453 793.31 862.9 0.3635 1.38721 +FS_15 BypBld.Fl_O 536.02 8.574 492.81 117.76 0.0000 895.54 7.472 473.78 3795.6 0.4475 1.40092 +FS_17 Duct5.Fl_O 536.02 8.510 492.81 117.76 0.0000 902.31 7.416 473.78 3824.3 0.4475 1.40092 +FS_19 Byp_Nozz.Fl_O 536.02 8.510 492.81 117.76 0.0000 902.31 5.453 433.86 2706.4 0.8229 1.40092 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1058.12 1.088 0.7857 2037.365 1.0310 0.7883 -2967.3 82.18 25.24 +LPC 92.47 1.424 0.8190 2006.515 1.1300 0.8278 -1199.5 28.49 8.18 +HPC 69.19 3.835 0.8532 6014.912 1.5438 0.8777 -5723.2 50.13 51.14 +HPT 27.28 2.811 0.9179 169.381 1.2837 0.9068 5723.2 +LPT 73.74 2.584 0.9011 61.031 1.2623 0.8887 4166.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2028.81 1.061 0.8117 0.517 2.6304 0.5215 1.4369 0.9679 3943.9586 +LPC 99.19 1.130 0.8531 0.548 1.5581 0.9323 3.2631 0.9600 3662.6571 +HPC 164.49 14.104 0.8417 0.946 2.3828 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.263 0.9363 110.626 5.2633 1.4085 0.4249 0.9803 1.5311 +LPT 153.22 3.210 0.9000 75.243 3.2101 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3258.93 14008.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 663.49 158.75 17.197 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 663.49 158.75 17.197 +Duct1 0.0025 0.2226 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 663.49 158.75 17.197 +Duct2 0.0025 0.3407 365.99 +Duct3 0.0050 0.2997 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1991 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.9324 859.65 206.38 46.595 +Duct5 0.0075 0.4475 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.0366 859.65 206.38 46.595 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 492.81 117.76 8.574 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.7085 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6232.4 4823.0 5723.2 +LP_Shaft 1955.9 11189.2 4166.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1353.88 0.9940 0.0550 0.35438 0.00705 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.560 0.9975 1.0000 0.9975 2706.36 0.823 838.6 13970.6 +Core_Nozz 1.095 0.9999 1.0000 0.9999 862.88 0.363 499.7 863.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 260 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 25000.0 0.00 975.67 16916.0 0.6413 10847.63 5.0403 813.15 22.700 2551.9 2487.2 1997.6 + core size:19.91 Q: 352.14 Maximum Thrust: 16916.0 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 975.67 8.316 484.68 115.81 0.0000 1666.72 5.453 429.52 5041.8 0.8000 1.40103 +FS_2 Inlet.Fl_O 975.67 8.274 484.68 115.81 0.0000 1675.11 6.605 454.40 5943.4 0.5763 1.40103 +FS_21 Fan.Fl_O 975.67 13.607 570.07 136.28 0.0000 1104.77 11.697 545.98 4515.2 0.4698 1.39953 +FS_13 Splitter.Fl_O2 814.14 13.607 570.07 136.28 0.0000 921.87 11.731 546.43 3795.6 0.4652 1.39953 +FS_22 Splitter.Fl_O1 161.53 13.607 570.07 136.28 0.0000 182.90 11.510 543.46 719.5 0.4948 1.39953 +FS_23 Duct1.Fl_O 161.53 13.573 570.07 136.28 0.0000 183.36 11.481 543.46 721.3 0.4948 1.39953 +FS_24 LPC.Fl_O 161.53 33.777 764.34 183.15 0.0000 85.31 29.554 736.01 366.0 0.4417 1.39365 +FS_25 Duct2.Fl_O 161.53 33.693 764.34 183.15 0.0000 85.53 29.480 736.01 366.9 0.4417 1.39365 +FS_3 HPC.Fl_O 161.53 188.771 1300.50 317.08 0.0000 19.91 177.688 1279.73 119.9 0.2991 1.36186 +FS_36 Bld3.Fl_O 146.99 188.771 1300.50 317.08 0.0000 18.12 177.688 1279.73 109.1 0.2991 1.36186 +FS_4 Burner.Fl_O 150.00 178.389 2551.94 678.22 0.0205 27.41 177.238 2548.15 483.4 0.0999 1.29862 +FS_45 HPT.Fl_O 164.54 66.931 1997.57 514.83 0.0187 70.90 63.224 1970.45 439.1 0.2953 1.31509 +FS_48 Duct3.Fl_O 164.54 66.597 1997.57 514.83 0.0187 71.26 62.908 1970.45 441.4 0.2953 1.31509 +FS_5 LPT.Fl_O 164.54 13.698 1394.35 347.40 0.0187 289.45 12.542 1363.24 1477.4 0.3640 1.34335 +FS_7 Duct4.Fl_O 164.54 13.561 1394.35 347.40 0.0187 292.37 12.965 1378.43 2018.9 0.2592 1.34335 +FS_9 Core_Nozz.Fl_O 164.54 13.561 1394.35 347.40 0.0187 292.37 7.260 1185.94 862.9 1.0000 1.34335 +FS_15 BypBld.Fl_O 814.14 13.607 570.07 136.28 0.0000 921.87 11.731 546.43 3795.6 0.4652 1.39953 +FS_17 Duct5.Fl_O 814.14 13.504 570.07 136.28 0.0000 928.84 11.643 546.43 3824.3 0.4652 1.39953 +FS_19 Byp_Nozz.Fl_O 814.14 13.504 570.07 136.28 0.0000 928.84 7.132 474.93 2706.3 1.0000 1.39953 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.644 0.8675 3944.235 1.1762 0.8765 -28267.6 24.72 17.46 +LPC 183.36 2.489 0.8683 3636.832 1.3408 0.8839 -10709.6 28.37 23.28 +HPC 85.53 5.603 0.8652 6324.883 1.7015 0.8922 -30608.4 20.18 20.24 +HPT 27.41 2.665 0.9136 151.990 1.2299 0.9038 30608.9 +LPT 71.26 4.862 0.9327 85.308 1.4326 0.9188 38977.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.448 0.8962 1.000 2.3713 0.5215 1.4369 0.9679 3943.9586 +LPC 196.68 1.456 0.9045 0.993 1.7663 0.9323 3.2631 0.9600 3662.6571 +HPC 203.32 22.278 0.8535 0.995 2.0442 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.919 0.9319 99.267 4.9194 1.4085 0.4249 0.9803 1.5311 +LPT 148.06 6.387 0.9315 105.175 6.3873 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5041.83 24658.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 955.79 230.02 56.412 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 955.79 230.02 56.412 +Duct1 0.0025 0.4948 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 955.79 230.02 56.412 +Duct2 0.0025 0.4417 365.99 +Duct3 0.0050 0.2953 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3640 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.6534 1300.50 317.08 188.771 +Duct5 0.0075 0.4652 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.8840 1300.50 317.08 188.771 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 570.07 136.28 13.607 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0403 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7678.0 20937.9 30608.9 +LP_Shaft 3812.8 53691.0 38977.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2551.94 0.9940 0.0550 3.01323 0.02050 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.476 0.9962 1.0000 0.9975 2706.36 1.000 1066.1 31519.3 +Core_Nozz 2.487 0.9979 1.0000 0.9999 862.88 1.000 1661.3 10055.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 261 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 25000.0 0.00 951.12 15224.0 0.6303 9595.80 5.3062 813.15 20.795 2460.7 2398.7 1919.7 + core size:20.00 Q: 352.14 Maximum Thrust: 16916.0 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 951.12 8.316 484.68 115.81 0.0000 1624.78 5.453 429.52 4915.0 0.8000 1.40103 +FS_2 Inlet.Fl_O 951.12 8.274 484.68 115.81 0.0000 1632.96 6.717 456.58 5943.4 0.5538 1.40103 +FS_21 Fan.Fl_O 951.12 13.299 563.60 134.73 0.0000 1095.62 11.470 540.28 4515.2 0.4646 1.39965 +FS_13 Splitter.Fl_O2 800.30 13.299 563.60 134.73 0.0000 921.88 11.466 540.23 3795.6 0.4651 1.39965 +FS_22 Splitter.Fl_O1 150.82 13.299 563.60 134.73 0.0000 173.74 11.492 540.58 719.5 0.4615 1.39965 +FS_23 Duct1.Fl_O 150.82 13.266 563.60 134.73 0.0000 174.17 11.463 540.58 721.3 0.4615 1.39965 +FS_24 LPC.Fl_O 150.82 30.932 740.90 177.46 0.0000 85.64 27.030 713.14 366.0 0.4438 1.39462 +FS_25 Duct2.Fl_O 150.82 30.855 740.90 177.46 0.0000 85.86 26.963 713.14 366.9 0.4438 1.39462 +FS_3 HPC.Fl_O 150.82 172.934 1263.55 307.57 0.0000 20.00 162.679 1243.08 119.9 0.3004 1.36416 +FS_36 Bld3.Fl_O 137.25 172.934 1263.55 307.57 0.0000 18.20 162.679 1243.08 109.1 0.3004 1.36416 +FS_4 Burner.Fl_O 139.91 163.423 2460.73 650.25 0.0194 27.41 162.369 2457.05 483.4 0.0997 1.30139 +FS_45 HPT.Fl_O 153.49 60.713 1919.66 492.10 0.0177 71.48 57.291 1892.91 439.1 0.2975 1.31865 +FS_48 Duct3.Fl_O 153.49 60.409 1919.66 492.10 0.0177 71.84 57.005 1892.91 441.4 0.2975 1.31865 +FS_5 LPT.Fl_O 153.49 12.520 1340.97 332.85 0.0177 289.68 11.463 1310.75 1477.4 0.3638 1.34721 +FS_7 Duct4.Fl_O 153.49 12.395 1340.97 332.85 0.0177 292.61 11.850 1325.50 2018.9 0.2590 1.34721 +FS_9 Core_Nozz.Fl_O 153.49 12.395 1340.97 332.85 0.0177 292.61 6.627 1138.71 862.9 1.0000 1.34721 +FS_15 BypBld.Fl_O 800.30 13.299 563.60 134.73 0.0000 921.88 11.466 540.23 3795.6 0.4651 1.39965 +FS_17 Duct5.Fl_O 800.30 13.199 563.60 134.73 0.0000 928.85 11.380 540.23 3824.3 0.4651 1.39965 +FS_19 Byp_Nozz.Fl_O 800.30 13.199 563.60 134.73 0.0000 928.85 6.970 469.52 2706.4 1.0000 1.39965 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1632.96 1.607 0.8925 3742.235 1.1628 0.8995 -25465.9 28.22 17.74 +LPC 174.17 2.332 0.8659 3470.323 1.3146 0.8807 -9118.5 28.79 22.09 +HPC 85.86 5.605 0.8642 6333.051 1.7054 0.8914 -27763.8 20.62 20.65 +HPT 27.41 2.692 0.9140 152.586 1.2344 0.9042 27763.9 +LPT 71.84 4.825 0.9282 82.565 1.4316 0.9134 34583.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3130.82 1.423 0.9221 0.949 2.1751 0.5215 1.4369 0.9679 3943.9586 +LPC 186.82 1.408 0.9020 0.947 1.7496 0.9323 3.2631 0.9600 3662.6571 +HPC 204.11 22.287 0.8526 0.996 2.0713 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.982 0.9324 99.657 4.9817 1.4085 0.4249 0.9803 1.5311 +LPT 149.26 6.336 0.9270 101.793 6.3356 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4914.97 24038.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 927.35 223.00 51.669 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 927.35 223.00 51.669 +Duct1 0.0025 0.4615 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 927.35 223.00 51.669 +Duct2 0.0025 0.4438 365.99 +Duct3 0.0050 0.2975 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3638 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 5.2788 1263.55 307.57 172.934 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 8.2952 1263.55 307.57 172.934 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 563.60 134.73 13.299 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3062 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7569.1 19264.9 27763.9 +LP_Shaft 3617.5 50210.1 34583.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2460.73 0.9940 0.0550 2.66550 0.01942 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.420 0.9965 1.0000 0.9975 2706.36 1.000 1060.0 30472.6 +Core_Nozz 2.273 0.9991 1.0000 0.9999 862.88 1.000 1630.1 8789.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 262 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 25000.0 0.00 923.36 13532.8 0.6255 8465.36 5.5127 813.15 19.155 2366.7 2307.6 1841.9 + core size:20.16 Q: 352.14 Maximum Thrust: 16916.0 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 923.36 8.316 484.68 115.81 0.0000 1577.37 5.453 429.52 4771.5 0.8000 1.40103 +FS_2 Inlet.Fl_O 923.36 8.274 484.68 115.81 0.0000 1585.31 6.834 458.84 5943.4 0.5298 1.40103 +FS_21 Fan.Fl_O 923.36 12.920 557.68 133.31 0.0000 1089.11 11.168 534.95 4515.2 0.4609 1.39976 +FS_13 Splitter.Fl_O2 781.59 12.920 557.68 133.31 0.0000 921.88 11.139 534.55 3795.6 0.4651 1.39976 +FS_22 Splitter.Fl_O1 141.78 12.920 557.68 133.31 0.0000 167.23 11.317 536.97 719.5 0.4391 1.39976 +FS_23 Duct1.Fl_O 141.78 12.887 557.68 133.31 0.0000 167.65 11.289 536.97 721.3 0.4391 1.39976 +FS_24 LPC.Fl_O 141.78 29.098 726.32 173.93 0.0000 84.74 25.519 699.79 366.0 0.4377 1.39514 +FS_25 Duct2.Fl_O 141.78 29.025 726.32 173.93 0.0000 84.95 25.455 699.79 366.9 0.4377 1.39514 +FS_3 HPC.Fl_O 141.78 159.294 1231.99 299.48 0.0000 20.16 149.692 1211.61 119.9 0.3028 1.36613 +FS_36 Bld3.Fl_O 129.02 159.294 1231.99 299.48 0.0000 18.34 149.692 1211.61 109.1 0.3028 1.36613 +FS_4 Burner.Fl_O 131.37 150.533 2366.66 621.60 0.0182 27.40 149.563 2363.09 483.4 0.0996 1.30447 +FS_45 HPT.Fl_O 144.13 55.654 1841.90 469.58 0.0166 71.72 52.496 1815.81 439.1 0.2982 1.32251 +FS_48 Duct3.Fl_O 144.13 55.376 1841.90 469.58 0.0166 72.08 52.233 1815.81 441.4 0.2982 1.32251 +FS_5 LPT.Fl_O 144.13 11.493 1284.15 317.49 0.0166 289.98 10.520 1254.89 1477.4 0.3636 1.35143 +FS_7 Duct4.Fl_O 144.13 11.378 1284.15 317.49 0.0166 292.91 10.877 1269.17 2018.9 0.2589 1.35143 +FS_9 Core_Nozz.Fl_O 144.13 11.378 1284.15 317.49 0.0166 292.91 6.076 1088.57 862.9 1.0000 1.35143 +FS_15 BypBld.Fl_O 781.59 12.920 557.68 133.31 0.0000 921.88 11.139 534.55 3795.6 0.4651 1.39976 +FS_17 Duct5.Fl_O 781.59 12.823 557.68 133.31 0.0000 928.84 11.056 534.55 3824.3 0.4651 1.39976 +FS_19 Byp_Nozz.Fl_O 781.59 12.823 557.68 133.31 0.0000 928.84 6.771 464.57 2706.4 1.0000 1.39976 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1585.31 1.561 0.9024 3613.283 1.1506 0.9083 -22864.9 31.69 18.33 +LPC 167.65 2.258 0.8629 3368.492 1.3024 0.8776 -8148.7 27.92 20.38 +HPC 84.95 5.488 0.8650 6309.870 1.6962 0.8918 -25185.0 22.24 22.33 +HPT 27.40 2.705 0.9145 153.486 1.2381 0.9047 25184.8 +LPT 72.08 4.818 0.9262 81.386 1.4343 0.9108 31013.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3039.64 1.391 0.9322 0.916 2.0963 0.5215 1.4369 0.9679 3943.9586 +LPC 179.83 1.385 0.8989 0.920 1.7128 0.9323 3.2631 0.9600 3662.6571 +HPC 201.95 21.748 0.8533 0.993 2.0964 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.012 0.9329 100.245 5.0124 1.4085 0.4249 0.9803 1.5311 +LPT 149.78 6.326 0.9250 100.339 6.3262 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4771.55 23336.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 906.51 217.87 48.109 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 906.51 217.87 48.109 +Duct1 0.0025 0.4391 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 906.51 217.87 48.109 +Duct2 0.0025 0.4377 365.99 +Duct3 0.0050 0.2982 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.9623 1231.99 299.48 159.294 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.7979 1231.99 299.48 159.294 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 557.68 133.31 12.920 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5127 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7466.9 17714.8 25184.8 +LP_Shaft 3492.9 46634.6 31013.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2366.66 0.9940 0.0550 2.35149 0.01823 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.351 0.9969 1.0000 0.9975 2706.36 1.000 1054.4 29181.9 +Core_Nozz 2.086 0.9997 1.0000 0.9999 862.88 1.000 1596.2 7687.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 263 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 25000.0 0.00 863.33 10149.6 0.6300 6394.04 5.9897 813.15 15.959 2172.4 2119.8 1684.0 + core size:20.52 Q: 352.14 Maximum Thrust: 16916.0 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 863.33 8.316 484.68 115.81 0.0000 1474.81 5.453 429.52 4461.3 0.8000 1.40103 +FS_2 Inlet.Fl_O 863.33 8.274 484.68 115.81 0.0000 1482.23 7.058 463.11 5943.4 0.4818 1.40103 +FS_21 Fan.Fl_O 863.33 12.098 545.78 130.45 0.0000 1075.78 10.506 524.21 4515.2 0.4534 1.39999 +FS_13 Splitter.Fl_O2 739.82 12.098 545.78 130.45 0.0000 921.88 10.431 523.13 3795.6 0.4651 1.39999 +FS_22 Splitter.Fl_O1 123.51 12.098 545.78 130.45 0.0000 153.91 10.860 529.20 719.5 0.3957 1.39999 +FS_23 Duct1.Fl_O 123.51 12.068 545.78 130.45 0.0000 154.29 10.833 529.20 721.3 0.3957 1.39999 +FS_24 LPC.Fl_O 123.51 25.785 700.17 167.61 0.0000 81.79 22.866 676.69 366.0 0.4183 1.39600 +FS_25 Duct2.Fl_O 123.51 25.721 700.17 167.61 0.0000 81.99 22.809 676.69 366.9 0.4183 1.39600 +FS_3 HPC.Fl_O 123.51 132.713 1167.88 283.15 0.0000 20.52 124.400 1147.62 119.9 0.3085 1.37017 +FS_36 Bld3.Fl_O 112.40 132.713 1167.88 283.15 0.0000 18.68 124.400 1147.62 109.1 0.3085 1.37017 +FS_4 Burner.Fl_O 114.17 125.413 2172.43 563.35 0.0158 27.38 124.606 2169.10 483.4 0.0993 1.31138 +FS_45 HPT.Fl_O 125.29 46.094 1683.95 424.58 0.0144 71.98 43.459 1659.45 439.1 0.2983 1.33103 +FS_48 Duct3.Fl_O 125.29 45.863 1683.95 424.58 0.0144 72.34 43.242 1659.45 441.4 0.2983 1.33103 +FS_5 LPT.Fl_O 125.29 9.548 1169.68 287.03 0.0144 289.59 8.743 1142.66 1477.4 0.3618 1.36016 +FS_7 Duct4.Fl_O 125.29 9.453 1169.68 287.03 0.0144 292.52 9.037 1155.83 2018.9 0.2577 1.36016 +FS_9 Core_Nozz.Fl_O 125.29 9.453 1169.68 287.03 0.0144 292.52 5.453 1009.44 862.9 0.9304 1.36016 +FS_15 BypBld.Fl_O 739.82 12.098 545.78 130.45 0.0000 921.88 10.431 523.13 3795.6 0.4651 1.39999 +FS_17 Duct5.Fl_O 739.82 12.007 545.78 130.45 0.0000 928.84 10.353 523.13 3824.3 0.4651 1.39999 +FS_19 Byp_Nozz.Fl_O 739.82 12.007 545.78 130.45 0.0000 928.84 6.340 454.64 2706.4 1.0000 1.39999 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1482.23 1.462 0.9105 3371.179 1.1261 0.9152 -17890.9 39.31 19.68 +LPC 154.29 2.137 0.8538 3176.857 1.2829 0.8686 -6492.9 24.91 16.41 +HPC 81.99 5.160 0.8659 6248.277 1.6680 0.8920 -20190.9 26.60 26.76 +HPT 27.38 2.721 0.9149 155.756 1.2448 0.9047 20191.1 +LPT 72.34 4.803 0.9211 79.414 1.4397 0.9045 24383.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2841.92 1.322 0.9406 0.855 2.0395 0.5215 1.4369 0.9679 3943.9586 +LPC 165.50 1.348 0.8894 0.867 1.6155 0.9323 3.2631 0.9600 3662.6571 +HPC 194.92 20.229 0.8542 0.983 2.1338 0.4206 0.2163 1.0137 6357.1603 +HPT 30.12 5.050 0.9332 101.727 5.0502 1.4085 0.4249 0.9803 1.5311 +LPT 150.31 6.306 0.9200 97.908 6.3057 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4461.31 21819.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 866.48 208.05 41.395 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 866.48 208.05 41.395 +Duct1 0.0025 0.3957 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 866.48 208.05 41.395 +Duct2 0.0025 0.4183 365.99 +Duct3 0.0050 0.2983 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3618 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.3230 1167.88 283.15 132.713 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.7933 1167.88 283.15 132.713 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 545.78 130.45 12.098 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9897 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7259.7 14607.5 20191.1 +LP_Shaft 3258.8 39298.0 24383.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2172.43 0.9940 0.0550 1.77612 0.01580 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.202 0.9974 1.0000 0.9975 2706.36 1.000 1043.1 26386.5 +Core_Nozz 1.733 0.9999 1.0000 0.9999 862.88 0.930 1433.6 5582.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 264 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 25000.0 0.00 793.45 6766.3 0.6634 4489.09 6.6960 813.15 12.622 1957.2 1911.4 1508.9 + core size:20.94 Q: 352.14 Maximum Thrust: 16916.0 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 793.45 8.316 484.68 115.81 0.0000 1355.44 5.453 429.52 4100.2 0.8000 1.40103 +FS_2 Inlet.Fl_O 793.45 8.274 484.68 115.81 0.0000 1362.26 7.281 467.25 5943.4 0.4311 1.40103 +FS_21 Fan.Fl_O 793.45 11.147 532.06 127.16 0.0000 1059.53 9.732 511.81 4515.2 0.4445 1.40027 +FS_13 Splitter.Fl_O2 690.35 11.147 532.06 127.16 0.0000 921.86 9.611 509.98 3795.6 0.4650 1.40027 +FS_22 Splitter.Fl_O1 103.10 11.147 532.06 127.16 0.0000 137.67 10.258 519.57 719.5 0.3464 1.40027 +FS_23 Duct1.Fl_O 103.10 11.119 532.06 127.16 0.0000 138.02 10.232 519.57 721.3 0.3464 1.40027 +FS_24 LPC.Fl_O 103.10 21.786 665.52 159.24 0.0000 78.78 19.524 645.09 366.0 0.3991 1.39724 +FS_25 Duct2.Fl_O 103.10 21.731 665.52 159.24 0.0000 78.98 19.475 645.09 366.9 0.3991 1.39724 +FS_3 HPC.Fl_O 103.10 104.963 1091.40 263.83 0.0000 20.94 98.098 1071.43 119.9 0.3149 1.37499 +FS_36 Bld3.Fl_O 93.82 104.963 1091.40 263.83 0.0000 19.05 98.098 1071.43 109.1 0.3149 1.37499 +FS_4 Burner.Fl_O 95.07 99.190 1957.21 500.34 0.0133 27.36 98.552 1954.15 483.4 0.0989 1.32022 +FS_45 HPT.Fl_O 104.35 36.139 1508.89 375.97 0.0121 72.37 34.049 1486.16 439.1 0.2990 1.34132 +FS_48 Duct3.Fl_O 104.35 35.958 1508.89 375.97 0.0121 72.74 33.879 1486.16 441.4 0.2990 1.34132 +FS_5 LPT.Fl_O 104.35 7.978 1058.16 257.92 0.0121 274.55 7.380 1036.16 1477.4 0.3389 1.36884 +FS_7 Duct4.Fl_O 104.35 7.898 1058.16 257.92 0.0121 277.32 7.588 1046.79 2018.9 0.2425 1.36884 +FS_9 Core_Nozz.Fl_O 104.35 7.898 1058.16 257.92 0.0121 277.32 5.453 956.93 862.9 0.7531 1.36884 +FS_15 BypBld.Fl_O 690.35 11.147 532.06 127.16 0.0000 921.86 9.611 509.98 3795.6 0.4650 1.40027 +FS_17 Duct5.Fl_O 690.35 11.063 532.06 127.16 0.0000 928.82 9.538 509.98 3824.3 0.4650 1.40027 +FS_19 Byp_Nozz.Fl_O 690.35 11.063 532.06 127.16 0.0000 928.82 5.841 443.18 2706.3 1.0000 1.40027 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1362.26 1.347 0.9101 3053.590 1.0978 0.9139 -12748.1 46.97 21.40 +LPC 138.02 1.959 0.8432 2914.441 1.2508 0.8573 -4679.7 22.54 12.93 +HPC 78.98 4.830 0.8647 6197.389 1.6399 0.8903 -15256.5 31.56 31.81 +HPT 27.36 2.745 0.9154 158.682 1.2538 0.9051 15256.8 +LPT 72.74 4.507 0.9161 75.991 1.4260 0.8992 17428.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2611.95 1.242 0.9403 0.774 2.0747 0.5215 1.4369 0.9679 3943.9586 +LPC 148.04 1.294 0.8783 0.796 1.5370 0.9323 3.2631 0.9600 3662.6571 +HPC 187.76 18.705 0.8530 0.975 2.1684 0.4206 0.2163 1.0137 6357.1603 +HPT 30.10 5.106 0.9338 103.638 5.1063 1.4085 0.4249 0.9803 1.5311 +LPT 151.13 5.892 0.9150 93.687 5.8924 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4100.20 20053.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 816.56 195.85 33.925 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 816.56 195.85 33.925 +Duct1 0.0025 0.3464 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 816.56 195.85 33.925 +Duct2 0.0025 0.3991 365.99 +Duct3 0.0050 0.2990 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3389 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.6085 1091.40 263.83 104.963 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.6705 1091.40 263.83 104.963 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 532.06 127.16 11.147 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6960 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7020.1 11414.4 15256.8 +LP_Shaft 2951.8 31009.4 17428.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1957.21 0.9940 0.0550 1.24697 0.01329 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.029 0.9976 1.0000 0.9975 2706.36 1.000 1029.9 23148.9 +Core_Nozz 1.448 0.9999 1.0000 0.9999 862.88 0.753 1131.8 3670.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 265 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 25000.0 0.00 709.81 3383.3 0.7937 2685.51 7.8918 813.15 9.041 1681.1 1644.0 1286.5 + core size:21.56 Q: 352.14 Maximum Thrust: 16916.0 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 709.81 8.316 484.68 115.81 0.0000 1212.56 5.453 429.52 3668.0 0.8000 1.40103 +FS_2 Inlet.Fl_O 709.81 8.274 484.68 115.81 0.0000 1218.66 7.505 471.32 5943.4 0.3758 1.40103 +FS_21 Fan.Fl_O 709.81 10.021 515.40 123.17 0.0000 1037.71 8.810 496.76 4515.2 0.4327 1.40057 +FS_13 Splitter.Fl_O2 629.98 10.021 515.40 123.17 0.0000 921.01 8.643 494.05 3795.6 0.4644 1.40057 +FS_22 Splitter.Fl_O1 79.83 10.021 515.40 123.17 0.0000 116.70 9.462 507.02 719.5 0.2873 1.40057 +FS_23 Duct1.Fl_O 79.83 9.996 515.40 123.17 0.0000 117.00 9.439 507.02 721.3 0.2873 1.40057 +FS_24 LPC.Fl_O 79.83 17.173 619.19 148.09 0.0000 74.64 15.596 602.41 366.0 0.3737 1.39869 +FS_25 Duct2.Fl_O 79.83 17.130 619.19 148.09 0.0000 74.83 15.557 602.41 366.9 0.3737 1.39869 +FS_3 HPC.Fl_O 79.83 75.183 989.86 238.47 0.0000 21.56 69.948 970.32 119.9 0.3247 1.38134 +FS_36 Bld3.Fl_O 72.64 75.183 989.86 238.47 0.0000 19.62 69.948 970.32 109.1 0.3247 1.38134 +FS_4 Burner.Fl_O 73.39 71.048 1681.06 422.01 0.0103 27.33 70.592 1678.35 483.4 0.0982 1.33399 +FS_45 HPT.Fl_O 80.57 25.586 1286.46 316.10 0.0093 72.89 24.086 1266.18 439.1 0.2996 1.35615 +FS_48 Duct3.Fl_O 80.57 25.458 1286.46 316.10 0.0093 73.25 23.965 1266.18 441.4 0.2996 1.35615 +FS_5 LPT.Fl_O 80.57 6.788 935.65 226.56 0.0093 234.30 6.427 921.71 1477.4 0.2825 1.37845 +FS_7 Duct4.Fl_O 80.57 6.720 935.65 226.56 0.0093 236.66 6.530 928.32 2018.9 0.2042 1.37845 +FS_9 Core_Nozz.Fl_O 80.57 6.720 935.65 226.56 0.0093 236.66 5.453 883.40 862.9 0.5575 1.37845 +FS_15 BypBld.Fl_O 629.98 10.021 515.40 123.17 0.0000 921.01 8.643 494.05 3795.6 0.4644 1.40057 +FS_17 Duct5.Fl_O 629.98 9.945 515.40 123.17 0.0000 927.97 8.578 494.05 3824.3 0.4644 1.40057 +FS_19 Byp_Nozz.Fl_O 629.98 9.945 515.40 123.17 0.0000 927.97 5.453 433.95 2706.3 0.9673 1.40057 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1218.66 1.211 0.8883 2617.230 1.0634 0.8914 -7393.0 57.33 24.00 +LPC 117.00 1.718 0.8302 2538.016 1.2014 0.8426 -2814.4 22.40 9.60 +HPC 74.83 4.389 0.8625 6117.776 1.5986 0.8873 -10207.9 39.06 39.64 +HPT 27.33 2.777 0.9164 163.030 1.2667 0.9056 10208.1 +LPT 73.25 3.751 0.9117 70.538 1.3749 0.8957 10207.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2336.62 1.147 0.9177 0.664 2.2545 0.5215 1.4369 0.9679 3943.9586 +LPC 125.49 1.220 0.8648 0.693 1.4917 0.9323 3.2631 0.9600 3662.6571 +HPC 177.89 16.666 0.8509 0.962 2.2540 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.182 0.9348 106.478 5.1819 1.4085 0.4249 0.9803 1.5311 +LPT 152.21 4.837 0.9105 86.965 4.8369 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3668.00 17939.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 750.21 179.72 25.635 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 750.21 179.72 25.635 +Duct1 0.0025 0.2873 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 750.21 179.72 25.635 +Duct2 0.0025 0.3737 365.99 +Duct3 0.0050 0.2996 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2825 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.7940 989.86 238.47 75.183 +Duct5 0.0075 0.4644 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.3905 989.86 238.47 75.183 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 515.40 123.17 10.021 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8918 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6684.4 8020.9 10208.1 +LP_Shaft 2530.0 21189.8 10207.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1681.06 0.9940 0.0550 0.74597 0.01027 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.824 0.9975 1.0000 0.9975 2706.36 0.967 985.8 19302.1 +Core_Nozz 1.232 0.9999 1.0000 0.9999 862.88 0.558 806.9 2020.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 266 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 9/ 29/ 2/ 6 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 25000.0 0.00 626.92 845.8 1.6116 1363.15 9.7586 813.15 5.960 1374.9 1347.7 1044.0 + core size:22.45 Q: 352.14 Maximum Thrust: 16916.0 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 626.92 8.316 484.68 115.81 0.0000 1070.96 5.453 429.52 3239.7 0.8000 1.40103 +FS_2 Inlet.Fl_O 626.92 8.274 484.68 115.81 0.0000 1076.35 7.690 474.61 5943.4 0.3251 1.40103 +FS_21 Fan.Fl_O 626.92 9.033 500.38 119.57 0.0000 1001.78 8.028 483.76 4515.2 0.4139 1.40082 +FS_13 Splitter.Fl_O2 568.65 9.033 500.38 119.57 0.0000 908.66 7.831 480.34 3795.6 0.4561 1.40082 +FS_22 Splitter.Fl_O1 58.27 9.033 500.38 119.57 0.0000 93.11 8.720 495.36 719.5 0.2249 1.40082 +FS_23 Duct1.Fl_O 58.27 9.011 500.38 119.57 0.0000 93.35 8.699 495.36 721.3 0.2249 1.40082 +FS_24 LPC.Fl_O 58.27 13.054 568.84 135.99 0.0000 68.70 12.057 556.07 366.0 0.3389 1.39955 +FS_25 Duct2.Fl_O 58.27 13.022 568.84 135.99 0.0000 68.87 12.027 556.07 366.9 0.3389 1.39955 +FS_3 HPC.Fl_O 58.27 49.566 876.05 210.39 0.0000 22.45 45.794 856.85 119.9 0.3394 1.38823 +FS_36 Bld3.Fl_O 53.03 49.566 876.05 210.39 0.0000 20.43 45.794 856.85 109.1 0.3394 1.38823 +FS_4 Burner.Fl_O 53.41 46.840 1374.88 338.61 0.0071 27.28 46.541 1372.59 483.4 0.0974 1.35228 +FS_45 HPT.Fl_O 58.65 16.671 1043.97 253.23 0.0065 73.35 15.681 1026.71 439.1 0.2997 1.37348 +FS_48 Duct3.Fl_O 58.65 16.588 1043.97 253.23 0.0065 73.72 15.602 1026.71 441.4 0.2997 1.37348 +FS_5 LPT.Fl_O 58.65 6.092 816.69 196.70 0.0065 177.53 5.911 809.85 1477.4 0.2089 1.38701 +FS_7 Duct4.Fl_O 58.65 6.031 816.69 196.70 0.0065 179.33 5.935 813.03 2018.9 0.1526 1.38701 +FS_9 Core_Nozz.Fl_O 58.65 6.031 816.69 196.70 0.0065 179.33 5.453 794.02 862.9 0.3838 1.38701 +FS_15 BypBld.Fl_O 568.65 9.033 500.38 119.57 0.0000 908.66 7.831 480.34 3795.6 0.4561 1.40082 +FS_17 Duct5.Fl_O 568.65 8.965 500.38 119.57 0.0000 915.53 7.772 480.34 3824.3 0.4561 1.40082 +FS_19 Byp_Nozz.Fl_O 568.65 8.965 500.38 119.57 0.0000 915.53 5.453 433.99 2706.4 0.8732 1.40082 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1076.35 1.092 0.7848 2080.882 1.0324 0.7876 -3336.2 81.04 25.90 +LPC 93.35 1.449 0.8172 2047.972 1.1368 0.8265 -1353.8 26.44 7.79 +HPC 68.87 3.806 0.8524 6009.054 1.5401 0.8768 -6134.3 50.72 51.75 +HPT 27.28 2.810 0.9180 169.717 1.2827 0.9069 6134.3 +LPT 73.72 2.723 0.9021 62.256 1.2783 0.8890 4690.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2063.76 1.064 0.8108 0.528 2.6327 0.5215 1.4369 0.9679 3943.9586 +LPC 100.13 1.138 0.8512 0.559 1.5221 0.9323 3.2631 0.9600 3662.6571 +HPC 163.73 13.973 0.8410 0.945 2.3862 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.259 0.9364 110.845 5.2592 1.4085 0.4249 0.9803 1.5311 +LPT 153.18 3.403 0.9009 76.754 3.4032 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3239.67 15844.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 677.07 162.03 18.375 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 677.07 162.03 18.375 +Duct1 0.0025 0.2249 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 677.07 162.03 18.375 +Duct2 0.0025 0.3389 365.99 +Duct3 0.0050 0.2997 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2089 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.0395 876.05 210.39 49.566 +Duct5 0.0075 0.4561 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.2050 876.05 210.39 49.566 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 500.38 119.57 9.033 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.7586 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6293.0 5119.7 6134.3 +LP_Shaft 2011.5 12246.2 4690.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1374.88 0.9940 0.0550 0.37865 0.00714 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.644 0.9975 1.0000 0.9975 2706.36 0.873 889.9 15728.1 +Core_Nozz 1.106 0.9999 1.0000 0.9999 862.88 0.384 527.9 962.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 267 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 9/ 19/ 1/ 7 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 30000.0 0.00 643.10 12409.8 0.5037 6250.67 5.0393 497.55 22.735 2295.4 2236.8 1787.6 + core size:19.96 Q: 110.07 Maximum Thrust: 12409.8 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 643.10 5.177 432.34 103.28 0.0000 1666.72 4.364 411.69 6505.5 0.5000 1.40133 +FS_2 Inlet.Fl_O 643.10 5.151 432.34 103.28 0.0000 1675.11 4.112 405.33 5943.4 0.5763 1.40133 +FS_21 Fan.Fl_O 643.10 8.471 508.61 121.54 0.0000 1104.80 7.283 487.07 4515.2 0.4696 1.40069 +FS_13 Splitter.Fl_O2 536.62 8.471 508.61 121.54 0.0000 921.87 7.304 487.48 3795.6 0.4650 1.40069 +FS_22 Splitter.Fl_O1 106.49 8.471 508.61 121.54 0.0000 182.94 7.165 484.81 719.5 0.4948 1.40069 +FS_23 Duct1.Fl_O 106.49 8.450 508.61 121.54 0.0000 183.39 7.147 484.81 721.3 0.4948 1.40069 +FS_24 LPC.Fl_O 106.49 21.011 682.41 163.32 0.0000 85.43 18.377 656.92 366.0 0.4420 1.39662 +FS_25 Duct2.Fl_O 106.49 20.959 682.41 163.32 0.0000 85.65 18.331 656.92 366.9 0.4420 1.39662 +FS_3 HPC.Fl_O 106.49 117.703 1169.02 283.44 0.0000 19.96 110.759 1149.95 119.9 0.2990 1.37009 +FS_36 Bld3.Fl_O 96.90 117.703 1169.02 283.44 0.0000 18.16 110.759 1149.95 109.1 0.2990 1.37009 +FS_4 Burner.Fl_O 98.64 111.229 2295.36 600.49 0.0179 27.42 110.511 2291.87 483.4 0.0996 1.30659 +FS_45 HPT.Fl_O 108.22 41.628 1787.58 454.22 0.0163 70.93 39.322 1762.73 439.1 0.2942 1.32502 +FS_48 Duct3.Fl_O 108.22 41.420 1787.58 454.22 0.0163 71.28 39.125 1762.73 441.4 0.2942 1.32502 +FS_5 LPT.Fl_O 108.22 8.455 1235.33 304.59 0.0163 290.29 7.738 1206.94 1477.4 0.3636 1.35470 +FS_7 Duct4.Fl_O 108.22 8.371 1235.33 304.59 0.0163 293.22 8.001 1220.79 2018.9 0.2589 1.35470 +FS_9 Core_Nozz.Fl_O 108.22 8.371 1235.33 304.59 0.0163 293.22 4.467 1045.82 862.9 1.0000 1.35470 +FS_15 BypBld.Fl_O 536.62 8.471 508.61 121.54 0.0000 921.87 7.304 487.48 3795.6 0.4650 1.40069 +FS_17 Duct5.Fl_O 536.62 8.408 508.61 121.54 0.0000 928.83 7.249 487.48 3824.3 0.4650 1.40069 +FS_19 Byp_Nozz.Fl_O 536.62 8.408 508.61 121.54 0.0000 928.83 4.439 423.62 2706.4 1.0000 1.40069 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.645 0.8675 3944.235 1.1764 0.8765 -16616.8 24.71 17.45 +LPC 183.39 2.487 0.8684 3636.498 1.3417 0.8841 -6294.5 28.46 23.37 +HPC 85.65 5.616 0.8650 6328.015 1.7131 0.8924 -18097.1 20.03 20.08 +HPT 27.42 2.672 0.9132 151.503 1.2359 0.9033 18097.7 +LPT 71.28 4.899 0.9321 85.172 1.4470 0.9174 22910.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8962 1.000 2.3709 0.5215 1.4369 0.9679 3943.9586 +LPC 196.73 1.456 0.9046 0.993 1.7687 0.9323 3.2631 0.9600 3662.6571 +HPC 203.61 22.338 0.8533 0.995 2.0428 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.935 0.9315 98.949 4.9352 1.4085 0.4249 0.9803 1.5311 +LPT 148.12 6.439 0.9309 105.006 6.4385 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6505.45 9945.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 855.50 205.36 35.132 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 855.50 205.36 35.132 +Duct1 0.0025 0.4948 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 855.50 205.36 35.132 +Duct2 0.0025 0.4420 365.99 +Duct3 0.0050 0.2942 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.7270 1169.02 283.44 117.703 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.8567 1169.02 283.44 117.703 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 508.61 121.54 8.471 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0393 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7258.5 13095.2 18097.7 +LP_Shaft 3601.0 33414.3 22910.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2295.36 0.9940 0.0550 1.73630 0.01792 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.927 0.9975 1.0000 0.9975 2706.36 1.000 1006.9 16997.7 +Core_Nozz 1.918 0.9999 1.0000 0.9999 862.88 1.000 1566.2 5357.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 268 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 30000.0 0.00 625.75 11168.9 0.4924 5499.16 5.3139 497.55 20.743 2208.9 2152.9 1713.6 + core size:20.05 Q: 110.07 Maximum Thrust: 12409.8 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 625.75 5.177 432.34 103.28 0.0000 1621.74 4.364 411.69 6329.9 0.5000 1.40133 +FS_2 Inlet.Fl_O 625.75 5.151 432.34 103.28 0.0000 1629.91 4.186 407.41 5943.4 0.5522 1.40133 +FS_21 Fan.Fl_O 625.75 8.264 502.46 120.07 0.0000 1095.31 7.128 481.65 4515.2 0.4642 1.40078 +FS_13 Splitter.Fl_O2 526.64 8.264 502.46 120.07 0.0000 921.83 7.125 481.59 3795.6 0.4649 1.40078 +FS_22 Splitter.Fl_O1 99.11 8.264 502.46 120.07 0.0000 173.48 7.145 481.97 719.5 0.4604 1.40078 +FS_23 Duct1.Fl_O 99.11 8.243 502.46 120.07 0.0000 173.91 7.127 481.97 721.3 0.4604 1.40078 +FS_24 LPC.Fl_O 99.11 19.132 660.09 157.93 0.0000 85.88 16.703 635.07 366.0 0.4449 1.39745 +FS_25 Duct2.Fl_O 99.11 19.084 660.09 157.93 0.0000 86.10 16.662 635.07 366.9 0.4449 1.39745 +FS_3 HPC.Fl_O 99.11 107.387 1133.79 274.52 0.0000 20.05 100.989 1115.03 119.9 0.3003 1.37232 +FS_36 Bld3.Fl_O 90.19 107.387 1133.79 274.52 0.0000 18.25 100.989 1115.03 109.1 0.3003 1.37232 +FS_4 Burner.Fl_O 91.71 101.481 2208.91 574.65 0.0169 27.41 100.826 2205.53 483.4 0.0994 1.30958 +FS_45 HPT.Fl_O 100.63 37.585 1713.64 433.24 0.0154 71.52 35.465 1689.16 439.1 0.2965 1.32895 +FS_48 Duct3.Fl_O 100.63 37.397 1713.64 433.24 0.0154 71.88 35.288 1689.16 441.4 0.2965 1.32895 +FS_5 LPT.Fl_O 100.63 7.719 1186.16 291.55 0.0154 289.74 7.067 1158.82 1477.4 0.3623 1.35842 +FS_7 Duct4.Fl_O 100.63 7.642 1186.16 291.55 0.0154 292.67 7.306 1172.15 2018.9 0.2580 1.35842 +FS_9 Core_Nozz.Fl_O 100.63 7.642 1186.16 291.55 0.0154 292.67 4.364 1021.40 862.9 0.9399 1.35842 +FS_15 BypBld.Fl_O 526.64 8.264 502.46 120.07 0.0000 921.83 7.125 481.59 3795.6 0.4649 1.40078 +FS_17 Duct5.Fl_O 526.64 8.202 502.46 120.07 0.0000 928.80 7.072 481.59 3824.3 0.4649 1.40078 +FS_19 Byp_Nozz.Fl_O 526.64 8.202 502.46 120.07 0.0000 928.80 4.364 419.41 2706.4 0.9934 1.40078 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1629.91 1.604 0.8933 3732.714 1.1622 0.9002 -14864.1 28.45 17.79 +LPC 173.91 2.321 0.8660 3462.472 1.3137 0.8809 -5309.9 29.04 22.23 +HPC 86.10 5.627 0.8638 6339.631 1.7176 0.8916 -16347.1 20.41 20.43 +HPT 27.41 2.700 0.9137 152.171 1.2411 0.9036 16347.1 +LPT 71.88 4.845 0.9275 82.325 1.4447 0.9120 20174.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3125.16 1.421 0.9229 0.946 2.1689 0.5215 1.4369 0.9679 3943.9586 +LPC 186.54 1.405 0.9021 0.945 1.7548 0.9323 3.2631 0.9600 3662.6571 +HPC 204.68 22.390 0.8521 0.997 2.0727 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 5.001 0.9321 99.386 5.0013 1.4085 0.4249 0.9803 1.5311 +LPT 149.37 6.363 0.9263 101.496 6.3634 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6329.92 9676.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 828.40 198.74 32.020 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 828.40 198.74 32.020 +Duct1 0.0025 0.4604 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 828.40 198.74 32.020 +Duct2 0.0025 0.4449 365.99 +Duct3 0.0050 0.2965 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3623 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.4687 1133.79 274.52 107.387 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.4509 1133.79 274.52 107.387 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 502.46 120.07 8.264 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3139 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7151.9 12004.8 16347.1 +LP_Shaft 3407.9 31091.5 20174.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2208.91 0.9940 0.0550 1.52754 0.01694 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.879 0.9975 1.0000 0.9975 2706.36 0.993 995.3 16291.6 +Core_Nozz 1.751 0.9999 1.0000 0.9999 862.88 0.940 1456.0 4554.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 269 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 30000.0 0.00 605.26 9927.8 0.4869 4833.77 5.5244 497.55 19.021 2122.7 2069.4 1642.5 + core size:20.19 Q: 110.07 Maximum Thrust: 12409.8 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 605.26 5.177 432.34 103.28 0.0000 1568.63 4.364 411.69 6122.6 0.5000 1.40133 +FS_2 Inlet.Fl_O 605.26 5.151 432.34 103.28 0.0000 1576.53 4.267 409.64 5943.4 0.5255 1.40133 +FS_21 Fan.Fl_O 605.26 8.003 496.65 118.68 0.0000 1087.65 6.922 476.44 4515.2 0.4599 1.40087 +FS_13 Splitter.Fl_O2 512.49 8.003 496.65 118.68 0.0000 920.94 6.903 476.07 3795.6 0.4643 1.40087 +FS_22 Splitter.Fl_O1 92.77 8.003 496.65 118.68 0.0000 166.71 7.017 478.32 719.5 0.4371 1.40087 +FS_23 Duct1.Fl_O 92.77 7.983 496.65 118.68 0.0000 167.12 7.000 478.32 721.3 0.4371 1.40087 +FS_24 LPC.Fl_O 92.77 17.866 645.48 154.42 0.0000 85.13 15.645 621.53 366.0 0.4398 1.39797 +FS_25 Duct2.Fl_O 92.77 17.822 645.48 154.42 0.0000 85.34 15.606 621.53 366.9 0.4398 1.39797 +FS_3 HPC.Fl_O 92.77 98.470 1103.36 266.84 0.0000 20.19 92.515 1084.75 119.9 0.3024 1.37423 +FS_36 Bld3.Fl_O 84.42 98.470 1103.36 266.84 0.0000 18.38 92.515 1084.75 109.1 0.3024 1.37423 +FS_4 Burner.Fl_O 85.76 93.054 2122.74 549.10 0.0159 27.40 92.455 2119.47 483.4 0.0993 1.31279 +FS_45 HPT.Fl_O 94.11 34.280 1642.53 413.23 0.0145 71.80 32.331 1618.66 439.1 0.2973 1.33294 +FS_48 Duct3.Fl_O 94.11 34.109 1642.53 413.23 0.0145 72.16 32.170 1618.66 441.4 0.2973 1.33294 +FS_5 LPT.Fl_O 94.11 7.153 1138.40 278.97 0.0145 286.47 6.564 1112.66 1477.4 0.3569 1.36211 +FS_7 Duct4.Fl_O 94.11 7.081 1138.40 278.97 0.0145 289.36 6.777 1125.19 2018.9 0.2545 1.36211 +FS_9 Core_Nozz.Fl_O 94.11 7.081 1138.40 278.97 0.0145 289.36 4.364 999.60 862.9 0.8689 1.36211 +FS_15 BypBld.Fl_O 512.49 8.003 496.65 118.68 0.0000 920.94 6.903 476.07 3795.6 0.4643 1.40087 +FS_17 Duct5.Fl_O 512.49 7.943 496.65 118.68 0.0000 927.90 6.851 476.07 3824.3 0.4643 1.40087 +FS_19 Byp_Nozz.Fl_O 512.49 7.943 496.65 118.68 0.0000 927.90 4.364 418.39 2706.3 0.9655 1.40087 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1576.53 1.554 0.9036 3593.568 1.1488 0.9095 -13186.1 32.28 18.40 +LPC 167.12 2.238 0.8633 3352.829 1.2997 0.8777 -4690.9 28.40 20.62 +HPC 85.34 5.525 0.8645 6319.333 1.7094 0.8921 -14756.3 21.87 21.94 +HPT 27.40 2.715 0.9144 153.010 1.2450 0.9041 14756.4 +LPT 72.16 4.769 0.9259 80.953 1.4428 0.9102 17877.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3022.81 1.385 0.9336 0.911 2.0845 0.5215 1.4369 0.9679 3943.9586 +LPC 179.26 1.379 0.8992 0.915 1.7227 0.9323 3.2631 0.9600 3662.6571 +HPC 202.88 21.920 0.8528 0.994 2.0971 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 5.035 0.9327 99.934 5.0353 1.4085 0.4249 0.9803 1.5311 +LPT 149.94 6.257 0.9247 99.806 6.2572 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 6122.61 9359.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 808.00 193.76 29.637 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 808.00 193.76 29.637 +Duct1 0.0025 0.4371 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 808.00 193.76 29.637 +Duct2 0.0025 0.4398 365.99 +Duct3 0.0050 0.2973 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3569 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.2469 1103.36 266.84 98.470 +Duct5 0.0075 0.4643 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.1023 1103.36 266.84 98.470 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 496.65 118.68 8.003 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5244 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7049.7 10993.7 14756.4 +LP_Shaft 3280.9 28618.1 17877.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2122.74 0.9940 0.0550 1.34271 0.01591 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.820 0.9975 1.0000 0.9975 2706.36 0.966 966.2 15390.0 +Core_Nozz 1.623 0.9999 1.0000 0.9999 862.88 0.869 1332.5 3897.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 270 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 30000.0 0.00 557.08 7446.0 0.4877 3631.71 5.9921 497.55 15.633 1949.8 1901.9 1501.3 + core size:20.49 Q: 110.07 Maximum Thrust: 12409.8 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 557.08 5.177 432.34 103.28 0.0000 1443.77 4.364 411.69 5635.2 0.5000 1.40133 +FS_2 Inlet.Fl_O 557.08 5.151 432.34 103.28 0.0000 1451.04 4.432 414.13 5943.4 0.4681 1.40133 +FS_21 Fan.Fl_O 557.08 7.424 484.65 115.80 0.0000 1065.93 6.469 465.90 4515.2 0.4479 1.40103 +FS_13 Splitter.Fl_O2 477.41 7.424 484.65 115.80 0.0000 913.48 6.424 464.97 3795.6 0.4593 1.40103 +FS_22 Splitter.Fl_O1 79.67 7.424 484.65 115.80 0.0000 152.45 6.681 470.23 719.5 0.3910 1.40103 +FS_23 Duct1.Fl_O 79.67 7.406 484.65 115.80 0.0000 152.83 6.664 470.23 721.3 0.3910 1.40103 +FS_24 LPC.Fl_O 79.67 15.342 615.62 147.23 0.0000 83.14 13.538 594.04 366.0 0.4267 1.39876 +FS_25 Duct2.Fl_O 79.67 15.304 615.62 147.23 0.0000 83.35 13.504 594.04 366.9 0.4267 1.39876 +FS_3 HPC.Fl_O 79.67 80.932 1040.04 250.96 0.0000 20.49 75.885 1021.80 119.9 0.3069 1.37821 +FS_36 Bld3.Fl_O 72.50 80.932 1040.04 250.96 0.0000 18.64 75.885 1021.80 109.1 0.3069 1.37821 +FS_4 Burner.Fl_O 73.51 76.481 1949.78 498.59 0.0139 27.39 75.989 1946.73 483.4 0.0990 1.32006 +FS_45 HPT.Fl_O 80.68 27.958 1501.35 374.14 0.0127 72.15 26.353 1478.89 439.1 0.2979 1.34133 +FS_48 Duct3.Fl_O 80.68 27.819 1501.35 374.14 0.0127 72.52 26.221 1478.89 441.4 0.2979 1.34133 +FS_5 LPT.Fl_O 80.68 6.239 1052.69 256.64 0.0127 270.74 5.786 1031.49 1477.4 0.3335 1.36882 +FS_7 Duct4.Fl_O 80.68 6.177 1052.69 256.64 0.0127 273.48 5.941 1041.72 2018.9 0.2389 1.36882 +FS_9 Core_Nozz.Fl_O 80.68 6.177 1052.69 256.64 0.0127 273.48 4.364 957.99 862.8 0.7283 1.36882 +FS_15 BypBld.Fl_O 477.41 7.424 484.65 115.80 0.0000 913.48 6.424 464.97 3795.6 0.4593 1.40103 +FS_17 Duct5.Fl_O 477.41 7.369 484.65 115.80 0.0000 920.38 6.375 464.97 3824.3 0.4593 1.40103 +FS_19 Byp_Nozz.Fl_O 477.41 7.369 484.65 115.80 0.0000 920.38 4.364 417.14 2706.4 0.8981 1.40103 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1451.04 1.441 0.9119 3303.936 1.1210 0.9163 -9870.6 40.43 19.50 +LPC 152.83 2.072 0.8563 3120.538 1.2702 0.8701 -3542.7 26.86 17.39 +HPC 83.35 5.288 0.8654 6274.457 1.6894 0.8923 -11693.4 25.15 25.27 +HPT 27.39 2.736 0.9148 154.808 1.2525 0.9044 11693.4 +LPT 72.52 4.459 0.9219 77.850 1.4262 0.9060 13413.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2782.18 1.307 0.9421 0.838 2.0164 0.5215 1.4369 0.9679 3943.9586 +LPC 163.93 1.328 0.8919 0.852 1.6576 0.9323 3.2631 0.9600 3662.6571 +HPC 198.16 20.824 0.8537 0.987 2.1347 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.085 0.9331 101.108 5.0848 1.4085 0.4249 0.9803 1.5311 +LPT 150.68 5.825 0.9207 95.979 5.8249 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5635.25 8614.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 765.94 183.54 24.918 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 765.94 183.54 24.918 +Duct1 0.0025 0.3910 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 765.94 183.54 24.918 +Duct2 0.0025 0.4267 365.99 +Duct3 0.0050 0.2979 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3335 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.7885 1040.04 250.96 80.932 +Duct5 0.0075 0.4593 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.3820 1040.04 250.96 80.932 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 484.65 115.80 7.424 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9921 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6835.8 8984.4 11693.4 +LP_Shaft 3016.5 23354.0 13413.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1949.78 0.9940 0.0550 1.00881 0.01391 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.689 0.9975 1.0000 0.9975 2706.36 0.898 897.3 13315.0 +Core_Nozz 1.415 0.9999 1.0000 0.9999 862.88 0.728 1094.9 2745.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 271 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 30000.0 0.00 498.23 4964.0 0.5074 2518.89 6.6267 497.55 12.132 1752.1 1710.3 1340.7 + core size:20.84 Q: 110.07 Maximum Thrust: 12409.8 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 498.23 5.177 432.34 103.28 0.0000 1291.24 4.364 411.69 5039.9 0.5000 1.40133 +FS_2 Inlet.Fl_O 498.23 5.151 432.34 103.28 0.0000 1297.75 4.599 418.52 5943.4 0.4057 1.40133 +FS_21 Fan.Fl_O 498.23 6.795 471.44 112.64 0.0000 1027.26 5.994 454.79 4515.2 0.4271 1.40118 +FS_13 Splitter.Fl_O2 432.90 6.795 471.44 112.64 0.0000 892.56 5.929 453.38 3795.6 0.4456 1.40118 +FS_22 Splitter.Fl_O1 65.33 6.795 471.44 112.64 0.0000 134.69 6.279 460.89 719.5 0.3377 1.40118 +FS_23 Duct1.Fl_O 65.33 6.778 471.44 112.64 0.0000 135.03 6.264 460.89 721.3 0.3377 1.40118 +FS_24 LPC.Fl_O 65.33 12.546 578.47 138.30 0.0000 80.81 11.165 559.53 366.0 0.4116 1.39939 +FS_25 Duct2.Fl_O 65.33 12.515 578.47 138.30 0.0000 81.01 11.137 559.53 366.9 0.4116 1.39939 +FS_3 HPC.Fl_O 65.33 62.810 964.20 232.10 0.0000 20.84 58.746 946.49 119.9 0.3123 1.38293 +FS_36 Bld3.Fl_O 59.45 62.810 964.20 232.10 0.0000 18.96 58.746 946.49 109.1 0.3123 1.38293 +FS_4 Burner.Fl_O 60.15 59.355 1752.12 442.23 0.0118 27.37 58.973 1749.32 483.4 0.0985 1.32969 +FS_45 HPT.Fl_O 66.03 21.454 1340.71 330.71 0.0107 72.72 20.201 1319.86 439.1 0.2993 1.35188 +FS_48 Duct3.Fl_O 66.03 21.346 1340.71 330.71 0.0107 73.08 20.100 1319.86 441.4 0.2993 1.35188 +FS_5 LPT.Fl_O 66.03 5.520 967.26 234.70 0.0107 240.07 5.210 952.15 1477.4 0.2905 1.37557 +FS_7 Duct4.Fl_O 66.03 5.464 967.26 234.70 0.0107 242.49 5.302 959.33 2018.9 0.2097 1.37557 +FS_9 Core_Nozz.Fl_O 66.03 5.464 967.26 234.70 0.0107 242.49 4.364 909.48 862.8 0.5798 1.37557 +FS_15 BypBld.Fl_O 432.90 6.795 471.44 112.64 0.0000 892.56 5.929 453.38 3795.6 0.4456 1.40118 +FS_17 Duct5.Fl_O 432.90 6.744 471.44 112.64 0.0000 899.31 5.884 453.38 3824.3 0.4456 1.40118 +FS_19 Byp_Nozz.Fl_O 432.90 6.744 471.44 112.64 0.0000 899.31 4.364 416.18 2706.4 0.8134 1.40118 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1297.75 1.319 0.9128 2923.892 1.0904 0.9162 -6597.6 46.41 20.15 +LPC 135.03 1.851 0.8479 2800.020 1.2270 0.8605 -2372.1 26.53 14.46 +HPC 81.01 5.019 0.8648 6230.606 1.6668 0.8911 -8670.0 29.16 29.35 +HPT 27.37 2.767 0.9153 157.196 1.2623 0.9045 8670.0 +LPT 73.08 3.867 0.9190 72.905 1.3861 0.9040 8969.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2488.25 1.222 0.9431 0.741 2.0241 0.5215 1.4369 0.9679 3943.9586 +LPC 144.84 1.261 0.8832 0.764 1.6182 0.9323 3.2631 0.9600 3662.6571 +HPC 192.60 19.578 0.8531 0.980 2.1705 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.158 0.9336 102.668 5.1580 1.4085 0.4249 0.9803 1.5311 +LPT 151.86 5.000 0.9178 89.883 4.9999 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5039.93 7704.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 714.75 171.13 19.883 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 714.75 171.13 19.883 +Duct1 0.0025 0.3377 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 714.75 171.13 19.883 +Duct2 0.0025 0.4116 365.99 +Duct3 0.0050 0.2993 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2905 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.2864 964.20 232.10 62.810 +Duct5 0.0075 0.4456 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.5930 964.20 232.10 62.810 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 471.44 112.64 6.795 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6267 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6580.0 6920.3 8670.0 +LP_Shaft 2669.5 17647.3 8969.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1752.12 0.9940 0.0550 0.69969 0.01177 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.545 0.9975 1.0000 0.9975 2706.36 0.813 811.8 10923.0 +Core_Nozz 1.252 0.9999 1.0000 0.9999 862.88 0.580 850.7 1745.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 272 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 30000.0 0.00 422.36 2481.9 0.5943 1475.09 7.5905 497.55 8.423 1495.7 1461.6 1135.2 + core size:21.38 Q: 110.07 Maximum Thrust: 12409.8 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 422.36 5.177 432.34 103.28 0.0000 1094.63 4.364 411.69 4272.5 0.5000 1.40133 +FS_2 Inlet.Fl_O 422.36 5.151 432.34 103.28 0.0000 1100.15 4.769 422.91 5943.4 0.3333 1.40133 +FS_21 Fan.Fl_O 422.36 6.103 456.14 108.98 0.0000 953.75 5.496 442.66 4515.2 0.3895 1.40130 +FS_13 Splitter.Fl_O2 373.20 6.103 456.14 108.98 0.0000 842.73 5.423 440.96 3795.6 0.4142 1.40130 +FS_22 Splitter.Fl_O1 49.17 6.103 456.14 108.98 0.0000 111.02 5.797 449.48 719.5 0.2718 1.40130 +FS_23 Duct1.Fl_O 49.17 6.088 456.14 108.98 0.0000 111.30 5.783 449.48 721.3 0.2718 1.40130 +FS_24 LPC.Fl_O 49.17 9.479 529.75 126.61 0.0000 77.03 8.544 514.25 366.0 0.3879 1.40031 +FS_25 Duct2.Fl_O 49.17 9.456 529.75 126.61 0.0000 77.23 8.523 514.25 366.9 0.3879 1.40031 +FS_3 HPC.Fl_O 49.17 43.605 863.07 207.21 0.0000 21.38 40.625 846.12 119.9 0.3207 1.38892 +FS_36 Bld3.Fl_O 44.74 43.605 863.07 207.21 0.0000 19.45 40.625 846.12 109.1 0.3207 1.38892 +FS_4 Burner.Fl_O 45.15 41.206 1495.68 371.36 0.0092 27.34 40.942 1493.21 483.4 0.0979 1.34404 +FS_45 HPT.Fl_O 49.58 14.704 1135.19 276.77 0.0083 73.30 13.831 1116.70 439.1 0.3003 1.36642 +FS_48 Duct3.Fl_O 49.58 14.630 1135.19 276.77 0.0083 73.67 13.762 1116.70 441.4 0.3003 1.36642 +FS_5 LPT.Fl_O 49.58 4.967 872.62 210.74 0.0083 190.26 4.797 864.22 1477.4 0.2252 1.38297 +FS_7 Duct4.Fl_O 49.58 4.917 872.62 210.74 0.0083 192.18 4.827 868.14 2018.9 0.1641 1.38297 +FS_9 Core_Nozz.Fl_O 49.58 4.917 872.62 210.74 0.0083 192.18 4.364 844.23 862.9 0.4186 1.38297 +FS_15 BypBld.Fl_O 373.20 6.103 456.14 108.98 0.0000 842.73 5.423 440.96 3795.6 0.4142 1.40130 +FS_17 Duct5.Fl_O 373.20 6.057 456.14 108.98 0.0000 849.10 5.382 440.96 3824.3 0.4142 1.40130 +FS_19 Byp_Nozz.Fl_O 373.20 6.057 456.14 108.98 0.0000 849.10 4.364 415.25 2706.4 0.7005 1.40130 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1100.15 1.185 0.9038 2380.425 1.0551 0.9061 -3404.9 54.80 19.89 +LPC 111.30 1.557 0.8372 2317.481 1.1614 0.8471 -1226.6 31.05 11.70 +HPC 77.23 4.612 0.8631 6163.115 1.6292 0.8886 -5607.3 35.68 36.08 +HPT 27.34 2.802 0.9162 161.053 1.2758 0.9049 5607.4 +LPT 73.67 2.946 0.9061 64.504 1.3009 0.8924 4631.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2109.38 1.129 0.9337 0.604 2.1438 0.5215 1.4369 0.9679 3943.9586 +LPC 119.39 1.171 0.8721 0.633 1.6494 0.9323 3.2631 0.9600 3662.6571 +HPC 183.59 17.695 0.8514 0.969 2.2226 0.4206 0.2163 1.0137 6357.1603 +HPT 30.09 5.242 0.9345 105.187 5.2422 1.4085 0.4249 0.9803 1.5311 +LPT 153.08 3.714 0.9050 79.525 3.7140 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4272.53 6531.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 647.16 154.82 14.458 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 647.16 154.82 14.458 +Duct1 0.0025 0.2718 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 647.16 154.82 14.458 +Duct2 0.0025 0.3879 365.99 +Duct3 0.0050 0.3003 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2252 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.7208 863.07 207.21 43.605 +Duct5 0.0075 0.4142 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.7042 863.07 207.21 43.605 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 456.14 108.98 6.103 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.5905 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6228.6 4728.3 5607.4 +LP_Shaft 2173.3 11192.3 4631.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1495.68 0.9940 0.0550 0.40975 0.00916 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.388 0.9975 1.0000 0.9975 2706.36 0.700 698.3 8099.9 +Core_Nozz 1.127 0.9999 1.0000 0.9999 862.88 0.419 592.9 913.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 273 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 14/ 34/ 2/11 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.500 30000.0 0.00 343.26 620.5 1.1106 689.13 8.9246 497.55 5.266 1183.7 1159.8 891.8 + core size:22.39 Q: 110.07 Maximum Thrust: 12409.8 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 343.26 5.177 432.34 103.28 0.0000 889.62 4.364 411.69 3472.3 0.5000 1.40133 +FS_2 Inlet.Fl_O 343.26 5.151 432.34 103.28 0.0000 894.10 4.907 426.36 5943.4 0.2644 1.40133 +FS_21 Fan.Fl_O 343.26 5.518 442.40 105.69 0.0000 844.24 5.100 432.52 4515.2 0.3372 1.40134 +FS_13 Splitter.Fl_O2 308.67 5.518 442.40 105.69 0.0000 759.17 5.033 430.88 3795.6 0.3648 1.40134 +FS_22 Splitter.Fl_O1 34.59 5.518 442.40 105.69 0.0000 85.07 5.360 438.72 719.5 0.2043 1.40134 +FS_23 Duct1.Fl_O 34.59 5.505 442.40 105.69 0.0000 85.28 5.347 438.72 721.3 0.2043 1.40134 +FS_24 LPC.Fl_O 34.59 7.023 481.38 115.02 0.0000 69.72 6.469 470.18 366.0 0.3446 1.40107 +FS_25 Duct2.Fl_O 34.59 7.005 481.38 115.02 0.0000 69.90 6.452 470.18 366.9 0.3446 1.40107 +FS_3 HPC.Fl_O 34.59 27.262 747.89 179.16 0.0000 22.39 25.202 731.44 119.9 0.3375 1.39435 +FS_36 Bld3.Fl_O 31.47 27.262 747.89 179.16 0.0000 20.37 25.202 731.44 109.1 0.3375 1.39435 +FS_4 Burner.Fl_O 31.67 25.763 1183.75 288.67 0.0061 27.29 25.598 1181.72 483.4 0.0970 1.36488 +FS_45 HPT.Fl_O 34.78 9.109 891.82 215.08 0.0055 73.57 8.565 876.70 439.1 0.2996 1.38366 +FS_48 Duct3.Fl_O 34.78 9.064 891.82 215.08 0.0055 73.94 8.522 876.70 441.4 0.2996 1.38366 +FS_5 LPT.Fl_O 34.78 4.645 757.28 182.04 0.0055 132.95 4.569 753.76 1477.4 0.1545 1.39054 +FS_7 Duct4.Fl_O 34.78 4.599 757.28 182.04 0.0055 134.29 4.558 755.38 2018.9 0.1134 1.39054 +FS_9 Core_Nozz.Fl_O 34.78 4.599 757.28 182.04 0.0055 134.29 4.364 746.22 862.9 0.2755 1.39054 +FS_15 BypBld.Fl_O 308.67 5.518 442.40 105.69 0.0000 759.17 5.033 430.88 3795.6 0.3648 1.40134 +FS_17 Duct5.Fl_O 308.67 5.477 442.40 105.69 0.0000 764.91 4.995 430.88 3824.3 0.3648 1.40134 +FS_19 Byp_Nozz.Fl_O 308.67 5.477 442.40 105.69 0.0000 764.91 4.364 414.52 2706.4 0.5789 1.40134 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 894.10 1.071 0.8563 1739.958 1.0233 0.8578 -1169.1 81.95 17.92 +LPC 85.28 1.276 0.8198 1720.067 1.0881 0.8259 -456.7 42.95 10.02 +HPC 69.90 3.892 0.8544 6027.917 1.5536 0.8790 -3138.7 49.14 50.11 +HPT 27.29 2.828 0.9179 168.785 1.2923 0.9062 3138.6 +LPT 73.94 1.951 0.8865 53.194 1.1777 0.8766 1625.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1714.31 1.050 0.8847 0.441 2.4231 0.5215 1.4369 0.9679 3943.9586 +LPC 91.47 1.085 0.8539 0.470 1.7977 0.9323 3.2631 0.9600 3662.6571 +HPC 166.18 14.367 0.8429 0.948 2.3790 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.303 0.9363 110.237 5.3028 1.4085 0.4249 0.9803 1.5311 +LPT 153.64 2.327 0.8853 65.582 2.3270 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3472.33 5308.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 574.99 137.47 9.973 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 574.99 137.47 9.973 +Duct1 0.0025 0.2043 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 574.99 137.47 9.973 +Duct2 0.0025 0.3446 365.99 +Duct3 0.0050 0.2996 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1545 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.2105 747.89 179.16 27.262 +Duct5 0.0075 0.3648 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 1.9023 747.89 179.16 27.262 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 442.40 105.69 5.518 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 8.9246 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 5807.2 2838.7 3138.6 +LP_Shaft 1588.6 5375.3 1625.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1183.75 0.9940 0.0550 0.19142 0.00608 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.255 0.9975 1.0000 0.9975 2706.36 0.579 576.6 5531.4 +Core_Nozz 1.054 0.9999 1.0000 0.9999 862.88 0.275 367.6 397.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 274 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 4/ 14/ 1/ 2 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 30000.0 0.00 684.40 12526.4 0.5442 6817.48 5.0399 597.05 22.729 2340.5 2280.8 1824.6 + core size:19.95 Q: 158.50 Maximum Thrust: 12526.4 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 684.40 5.567 441.43 105.45 0.0000 1666.72 4.364 411.69 5769.3 0.6000 1.40134 +FS_2 Inlet.Fl_O 684.40 5.539 441.43 105.45 0.0000 1675.11 4.422 413.84 5943.4 0.5763 1.40134 +FS_21 Fan.Fl_O 684.40 9.110 519.29 124.10 0.0000 1104.76 7.832 497.31 4515.2 0.4696 1.40051 +FS_13 Splitter.Fl_O2 571.09 9.110 519.29 124.10 0.0000 921.85 7.854 497.73 3795.6 0.4650 1.40051 +FS_22 Splitter.Fl_O1 113.31 9.110 519.29 124.10 0.0000 182.91 7.706 495.01 719.5 0.4947 1.40051 +FS_23 Duct1.Fl_O 113.31 9.087 519.29 124.10 0.0000 183.37 7.686 495.01 721.3 0.4947 1.40051 +FS_24 LPC.Fl_O 113.31 22.604 696.74 166.78 0.0000 85.38 19.774 670.77 366.0 0.4418 1.39612 +FS_25 Duct2.Fl_O 113.31 22.548 696.74 166.78 0.0000 85.60 19.725 670.77 366.9 0.4418 1.39612 +FS_3 HPC.Fl_O 113.31 126.536 1192.08 289.30 0.0000 19.95 119.078 1172.70 119.9 0.2990 1.36864 +FS_36 Bld3.Fl_O 103.11 126.536 1192.08 289.30 0.0000 18.16 119.078 1172.70 109.1 0.2990 1.36864 +FS_4 Burner.Fl_O 105.01 119.577 2340.48 614.02 0.0184 27.41 118.805 2336.94 483.4 0.0996 1.30506 +FS_45 HPT.Fl_O 115.21 44.773 1824.55 464.77 0.0167 70.92 42.293 1799.30 439.1 0.2944 1.32316 +FS_48 Duct3.Fl_O 115.21 44.550 1824.55 464.77 0.0167 71.28 42.081 1799.30 441.4 0.2944 1.32316 +FS_5 LPT.Fl_O 115.21 9.108 1263.20 312.01 0.0167 290.10 8.336 1234.33 1477.4 0.3636 1.35267 +FS_7 Duct4.Fl_O 115.21 9.017 1263.20 312.01 0.0167 293.03 8.619 1248.42 2018.9 0.2589 1.35267 +FS_9 Core_Nozz.Fl_O 115.21 9.017 1263.20 312.01 0.0167 293.03 4.814 1070.29 862.9 1.0000 1.35267 +FS_15 BypBld.Fl_O 571.09 9.110 519.29 124.10 0.0000 921.85 7.854 497.73 3795.6 0.4650 1.40051 +FS_17 Duct5.Fl_O 571.09 9.041 519.29 124.10 0.0000 928.82 7.795 497.73 3824.3 0.4650 1.40051 +FS_19 Byp_Nozz.Fl_O 571.09 9.041 519.29 124.10 0.0000 928.82 4.774 432.53 2706.4 1.0000 1.40051 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.645 0.8675 3944.235 1.1764 0.8766 -18056.9 24.71 17.45 +LPC 183.37 2.488 0.8684 3636.527 1.3417 0.8840 -6842.3 28.41 23.32 +HPC 85.60 5.612 0.8651 6326.811 1.7109 0.8923 -19642.1 20.06 20.12 +HPT 27.41 2.671 0.9133 151.573 1.2347 0.9034 19642.0 +LPT 71.28 4.891 0.9322 85.186 1.4444 0.9177 24899.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8963 1.000 2.3706 0.5215 1.4369 0.9679 3943.9586 +LPC 196.69 1.456 0.9045 0.993 1.7673 0.9323 3.2631 0.9600 3662.6571 +HPC 203.50 22.320 0.8534 0.995 2.0424 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.932 0.9316 98.995 4.9322 1.4085 0.4249 0.9803 1.5311 +LPT 148.11 6.428 0.9310 105.024 6.4282 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5769.35 12700.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 873.06 209.66 37.782 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 873.06 209.66 37.782 +Duct1 0.0025 0.4947 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 873.06 209.66 37.782 +Duct2 0.0025 0.4418 365.99 +Duct3 0.0050 0.2944 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.9660 1192.08 289.30 126.536 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.2322 1192.08 289.30 126.536 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 519.29 124.10 9.110 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0399 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7332.9 14068.4 19642.0 +LP_Shaft 3638.7 35939.6 24899.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2340.48 0.9940 0.0550 1.89374 0.01837 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.072 0.9976 1.0000 0.9975 2706.36 1.000 1017.4 19169.2 +Core_Nozz 2.066 0.9997 1.0000 0.9999 862.88 1.000 1583.3 6057.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 275 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 30000.0 0.00 666.76 11273.2 0.5333 6012.45 5.3082 597.05 20.787 2253.5 2196.4 1750.1 + core size:20.05 Q: 158.50 Maximum Thrust: 12526.4 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 666.76 5.567 441.43 105.45 0.0000 1623.76 4.364 411.69 5620.7 0.6000 1.40134 +FS_2 Inlet.Fl_O 666.76 5.539 441.43 105.45 0.0000 1631.94 4.498 415.88 5943.4 0.5533 1.40134 +FS_21 Fan.Fl_O 666.76 8.897 513.25 122.65 0.0000 1095.53 7.674 491.99 4515.2 0.4643 1.40061 +FS_13 Splitter.Fl_O2 561.06 8.897 513.25 122.65 0.0000 921.86 7.671 491.94 3795.6 0.4650 1.40061 +FS_22 Splitter.Fl_O1 105.70 8.897 513.25 122.65 0.0000 173.67 7.690 492.27 719.5 0.4611 1.40061 +FS_23 Duct1.Fl_O 105.70 8.875 513.25 122.65 0.0000 174.10 7.671 492.27 721.3 0.4611 1.40061 +FS_24 LPC.Fl_O 105.70 20.652 674.73 161.46 0.0000 85.79 18.037 649.25 366.0 0.4444 1.39690 +FS_25 Duct2.Fl_O 105.70 20.600 674.73 161.46 0.0000 86.00 17.992 649.25 366.9 0.4444 1.39690 +FS_3 HPC.Fl_O 105.70 115.722 1157.12 280.42 0.0000 20.05 108.830 1138.04 119.9 0.3004 1.37084 +FS_36 Bld3.Fl_O 96.18 115.722 1157.12 280.42 0.0000 18.24 108.830 1138.04 109.1 0.3004 1.37084 +FS_4 Burner.Fl_O 97.86 109.357 2253.45 587.88 0.0174 27.41 108.652 2250.02 483.4 0.0995 1.30809 +FS_45 HPT.Fl_O 107.37 40.535 1750.10 443.53 0.0158 71.50 38.250 1725.23 439.1 0.2966 1.32702 +FS_48 Duct3.Fl_O 107.37 40.333 1750.10 443.53 0.0158 71.86 38.059 1725.23 441.4 0.2966 1.32702 +FS_5 LPT.Fl_O 107.37 8.305 1212.58 298.52 0.0158 290.50 7.600 1184.57 1477.4 0.3636 1.35648 +FS_7 Duct4.Fl_O 107.37 8.222 1212.58 298.52 0.0158 293.43 7.858 1198.24 2018.9 0.2589 1.35648 +FS_9 Core_Nozz.Fl_O 107.37 8.222 1212.58 298.52 0.0158 293.43 4.386 1025.83 862.9 1.0000 1.35648 +FS_15 BypBld.Fl_O 561.06 8.897 513.25 122.65 0.0000 921.86 7.671 491.94 3795.6 0.4650 1.40061 +FS_17 Duct5.Fl_O 561.06 8.831 513.25 122.65 0.0000 928.83 7.614 491.94 3824.3 0.4650 1.40061 +FS_19 Byp_Nozz.Fl_O 561.06 8.831 513.25 122.65 0.0000 928.83 4.663 427.49 2706.4 1.0000 1.40061 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1631.94 1.606 0.8929 3738.725 1.1627 0.8998 -16226.5 28.29 17.75 +LPC 174.10 2.327 0.8660 3467.262 1.3146 0.8809 -5804.1 28.93 22.18 +HPC 86.00 5.618 0.8640 6336.914 1.7149 0.8916 -17789.4 20.51 20.53 +HPT 27.41 2.698 0.9138 152.256 1.2398 0.9038 17789.7 +LPT 71.86 4.856 0.9276 82.447 1.4433 0.9121 22028.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3128.70 1.422 0.9224 0.948 2.1722 0.5215 1.4369 0.9679 3943.9586 +LPC 186.75 1.407 0.9021 0.947 1.7527 0.9323 3.2631 0.9600 3662.6571 +HPC 204.45 22.346 0.8523 0.997 2.0725 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.996 0.9321 99.441 4.9960 1.4085 0.4249 0.9803 1.5311 +LPT 149.31 6.380 0.9264 101.647 6.3796 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5620.65 12373.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 846.25 203.10 34.535 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 846.25 203.10 34.535 +Duct1 0.0025 0.4611 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 846.25 203.10 34.535 +Duct2 0.0025 0.4444 365.99 +Duct3 0.0050 0.2966 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.6994 1157.12 280.42 115.722 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.8134 1157.12 280.42 115.722 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 513.25 122.65 8.897 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3082 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7227.7 12927.2 17789.7 +LP_Shaft 3449.1 33544.0 22028.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2253.45 0.9940 0.0550 1.67012 0.01736 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.024 0.9976 1.0000 0.9975 2706.36 1.000 1011.5 18447.6 +Core_Nozz 1.884 0.9999 1.0000 0.9999 862.88 1.000 1552.1 5198.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 276 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 30000.0 0.00 646.58 10021.2 0.5285 5296.01 5.5169 597.05 19.117 2166.0 2111.7 1677.9 + core size:20.20 Q: 158.50 Maximum Thrust: 12526.4 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 646.58 5.567 441.43 105.45 0.0000 1574.60 4.364 411.69 5450.5 0.6000 1.40134 +FS_2 Inlet.Fl_O 646.58 5.539 441.43 105.45 0.0000 1582.53 4.579 418.01 5943.4 0.5284 1.40134 +FS_21 Fan.Fl_O 646.58 8.633 507.65 121.31 0.0000 1088.95 7.463 486.94 4515.2 0.4606 1.40070 +FS_13 Splitter.Fl_O2 547.36 8.633 507.65 121.31 0.0000 921.85 7.443 486.56 3795.6 0.4649 1.40070 +FS_22 Splitter.Fl_O1 99.21 8.633 507.65 121.31 0.0000 167.10 7.564 488.81 719.5 0.4385 1.40070 +FS_23 Duct1.Fl_O 99.21 8.611 507.65 121.31 0.0000 167.51 7.545 488.81 721.3 0.4385 1.40070 +FS_24 LPC.Fl_O 99.21 19.378 660.86 158.12 0.0000 84.93 16.982 636.50 366.0 0.4386 1.39742 +FS_25 Duct2.Fl_O 99.21 19.330 660.86 158.12 0.0000 85.14 16.940 636.50 366.9 0.4386 1.39742 +FS_3 HPC.Fl_O 99.21 106.427 1127.23 272.86 0.0000 20.20 99.988 1108.27 119.9 0.3027 1.37273 +FS_36 Bld3.Fl_O 90.29 106.427 1127.23 272.86 0.0000 18.38 99.988 1108.27 109.1 0.3027 1.37273 +FS_4 Burner.Fl_O 91.76 100.574 2165.98 561.81 0.0163 27.40 99.925 2162.66 483.4 0.0993 1.31123 +FS_45 HPT.Fl_O 100.69 37.090 1677.93 423.12 0.0148 71.75 34.984 1653.68 439.1 0.2973 1.33101 +FS_48 Duct3.Fl_O 100.69 36.905 1677.93 423.12 0.0148 72.12 34.809 1653.68 441.4 0.2973 1.33101 +FS_5 LPT.Fl_O 100.69 7.645 1161.47 285.01 0.0148 289.64 7.000 1134.62 1477.4 0.3618 1.36039 +FS_7 Duct4.Fl_O 100.69 7.568 1161.47 285.01 0.0148 292.57 7.236 1147.71 2018.9 0.2577 1.36039 +FS_9 Core_Nozz.Fl_O 100.69 7.568 1161.47 285.01 0.0148 292.57 4.364 1002.13 862.9 0.9309 1.36039 +FS_15 BypBld.Fl_O 547.36 8.633 507.65 121.31 0.0000 921.85 7.443 486.56 3795.6 0.4649 1.40070 +FS_17 Duct5.Fl_O 547.36 8.568 507.65 121.31 0.0000 928.82 7.387 486.56 3824.3 0.4649 1.40070 +FS_19 Byp_Nozz.Fl_O 547.36 8.568 507.65 121.31 0.0000 928.82 4.524 422.82 2706.4 1.0000 1.40070 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1582.53 1.558 0.9027 3606.633 1.1500 0.9087 -14506.9 31.92 18.38 +LPC 167.51 2.250 0.8631 3363.169 1.3018 0.8777 -5167.1 28.14 20.51 +HPC 85.14 5.506 0.8647 6314.547 1.7057 0.8921 -16106.5 22.08 22.14 +HPT 27.40 2.712 0.9145 153.153 1.2436 0.9042 16106.3 +LPT 72.12 4.827 0.9258 81.227 1.4447 0.9100 19674.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3034.29 1.389 0.9326 0.914 2.0937 0.5215 1.4369 0.9679 3943.9586 +LPC 179.68 1.383 0.8991 0.918 1.7176 0.9323 3.2631 0.9600 3662.6571 +HPC 202.42 21.830 0.8531 0.993 2.0975 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 5.028 0.9328 100.027 5.0284 1.4085 0.4249 0.9803 1.5311 +LPT 149.85 6.339 0.9246 100.142 6.3391 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5450.49 11998.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 826.52 198.28 32.090 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 826.52 198.28 32.090 +Duct1 0.0025 0.4385 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 826.52 198.28 32.090 +Duct2 0.0025 0.4386 365.99 +Duct3 0.0050 0.2973 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3618 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.4725 1127.23 272.86 106.427 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.4568 1127.23 272.86 106.427 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 507.65 121.31 8.633 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5169 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7127.7 11868.0 16106.3 +LP_Shaft 3327.2 31056.0 19674.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2165.98 0.9940 0.0550 1.47111 0.01629 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.963 0.9975 1.0000 0.9975 2706.36 1.000 1006.0 17547.1 +Core_Nozz 1.734 0.9999 1.0000 0.9999 862.88 0.931 1429.2 4472.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 277 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 30000.0 0.00 600.22 7515.9 0.5316 3995.61 6.0042 597.05 15.805 1990.5 1941.8 1535.1 + core size:20.51 Q: 158.50 Maximum Thrust: 12526.4 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 600.22 5.567 441.43 105.45 0.0000 1461.72 4.364 411.69 5059.7 0.6000 1.40134 +FS_2 Inlet.Fl_O 600.22 5.539 441.43 105.45 0.0000 1469.07 4.743 422.23 5943.4 0.4760 1.40134 +FS_21 Fan.Fl_O 600.22 8.026 495.70 118.45 0.0000 1074.49 6.973 476.15 4515.2 0.4526 1.40088 +FS_13 Splitter.Fl_O2 514.53 8.026 495.70 118.45 0.0000 921.08 6.922 475.15 3795.6 0.4644 1.40088 +FS_22 Splitter.Fl_O1 85.69 8.026 495.70 118.45 0.0000 153.41 7.210 480.74 719.5 0.3940 1.40088 +FS_23 Duct1.Fl_O 85.69 8.005 495.70 118.45 0.0000 153.79 7.192 480.74 721.3 0.3940 1.40088 +FS_24 LPC.Fl_O 85.69 16.838 632.82 151.37 0.0000 82.61 14.887 611.00 366.0 0.4233 1.39835 +FS_25 Duct2.Fl_O 85.69 16.796 632.82 151.37 0.0000 82.82 14.850 611.00 366.9 0.4233 1.39835 +FS_3 HPC.Fl_O 85.69 87.987 1064.86 257.17 0.0000 20.51 82.486 1046.20 119.9 0.3075 1.37665 +FS_36 Bld3.Fl_O 77.98 87.987 1064.86 257.17 0.0000 18.66 82.486 1046.20 109.1 0.3075 1.37665 +FS_4 Burner.Fl_O 79.09 83.148 1990.48 510.30 0.0142 27.39 82.612 1987.38 483.4 0.0990 1.31835 +FS_45 HPT.Fl_O 86.80 30.452 1535.07 383.35 0.0130 72.07 28.708 1512.26 439.1 0.2978 1.33936 +FS_48 Duct3.Fl_O 86.80 30.300 1535.07 383.35 0.0130 72.43 28.564 1512.26 441.4 0.2978 1.33936 +FS_5 LPT.Fl_O 86.80 6.575 1069.56 261.00 0.0130 278.60 6.067 1046.63 1477.4 0.3448 1.36754 +FS_7 Duct4.Fl_O 86.80 6.509 1069.56 261.00 0.0130 281.42 6.246 1057.74 2018.9 0.2464 1.36754 +FS_9 Core_Nozz.Fl_O 86.80 6.509 1069.56 261.00 0.0130 281.42 4.364 959.72 862.9 0.7843 1.36754 +FS_15 BypBld.Fl_O 514.53 8.026 495.70 118.45 0.0000 921.08 6.922 475.15 3795.6 0.4644 1.40088 +FS_17 Duct5.Fl_O 514.53 7.965 495.70 118.45 0.0000 928.04 6.870 475.15 3824.3 0.4644 1.40088 +FS_19 Byp_Nozz.Fl_O 514.53 7.965 495.70 118.45 0.0000 928.04 4.364 417.25 2706.4 0.9681 1.40088 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1469.07 1.449 0.9107 3338.378 1.1230 0.9153 -11036.4 40.34 19.89 +LPC 153.79 2.103 0.8555 3150.307 1.2766 0.8697 -3991.1 26.05 17.04 +HPC 82.82 5.238 0.8656 6263.879 1.6827 0.8923 -12828.6 25.69 25.83 +HPT 27.39 2.730 0.9148 155.081 1.2508 0.9046 12828.6 +LPT 72.43 4.608 0.9217 78.606 1.4352 0.9055 15027.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2816.74 1.312 0.9409 0.846 2.0409 0.5215 1.4369 0.9679 3943.9586 +LPC 164.96 1.338 0.8911 0.860 1.6407 0.9323 3.2631 0.9600 3662.6571 +HPC 196.89 20.594 0.8540 0.985 2.1337 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.073 0.9332 101.286 5.0727 1.4085 0.4249 0.9803 1.5311 +LPT 150.50 6.033 0.9205 96.911 6.0333 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5059.73 11138.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 785.96 188.40 27.226 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 785.96 188.40 27.226 +Duct1 0.0025 0.3940 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 785.96 188.40 27.226 +Duct2 0.0025 0.4233 365.99 +Duct3 0.0050 0.2978 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3448 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.9993 1064.86 257.17 87.987 +Duct5 0.0075 0.4644 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.7132 1064.86 257.17 87.987 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 495.70 118.45 8.026 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.0042 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6918.9 9738.1 12828.6 +LP_Shaft 3079.8 25627.1 15027.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1990.48 0.9940 0.0550 1.10989 0.01423 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.825 0.9975 1.0000 0.9975 2706.36 0.968 967.4 15470.3 +Core_Nozz 1.492 0.9999 1.0000 0.9999 862.88 0.784 1180.1 3183.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 278 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 30000.0 0.00 543.86 5010.6 0.5567 2789.36 6.6909 597.05 12.354 1791.7 1749.2 1373.5 + core size:20.87 Q: 158.50 Maximum Thrust: 12526.4 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 543.86 5.567 441.43 105.45 0.0000 1324.46 4.364 411.69 4584.6 0.6000 1.40134 +FS_2 Inlet.Fl_O 543.86 5.539 441.43 105.45 0.0000 1331.13 4.909 426.42 5943.4 0.4187 1.40134 +FS_21 Fan.Fl_O 543.86 7.353 482.38 115.26 0.0000 1048.20 6.444 464.48 4515.2 0.4382 1.40106 +FS_13 Splitter.Fl_O2 473.15 7.353 482.38 115.26 0.0000 911.91 6.366 462.88 3795.6 0.4583 1.40106 +FS_22 Splitter.Fl_O1 70.71 7.353 482.38 115.26 0.0000 136.29 6.780 471.30 719.5 0.3423 1.40106 +FS_23 Duct1.Fl_O 70.71 7.335 482.38 115.26 0.0000 136.63 6.763 471.30 721.3 0.3423 1.40106 +FS_24 LPC.Fl_O 70.71 13.915 596.84 142.71 0.0000 80.11 12.413 577.71 366.0 0.4072 1.39909 +FS_25 Duct2.Fl_O 70.71 13.880 596.84 142.71 0.0000 80.32 12.382 577.71 366.9 0.4072 1.39909 +FS_3 HPC.Fl_O 70.71 68.779 989.99 238.50 0.0000 20.87 64.312 971.79 119.9 0.3131 1.38133 +FS_36 Bld3.Fl_O 64.35 68.779 989.99 238.50 0.0000 19.00 64.312 971.79 109.1 0.3131 1.38133 +FS_4 Burner.Fl_O 65.13 64.996 1791.70 453.33 0.0120 27.37 64.578 1788.85 483.4 0.0986 1.32775 +FS_45 HPT.Fl_O 71.49 23.558 1373.54 339.45 0.0110 72.57 22.189 1352.37 439.1 0.2989 1.34973 +FS_48 Duct3.Fl_O 71.49 23.440 1373.54 339.45 0.0110 72.94 22.078 1352.37 441.4 0.2989 1.34973 +FS_5 LPT.Fl_O 71.49 5.732 979.07 237.71 0.0110 251.83 5.376 962.11 1477.4 0.3065 1.37465 +FS_7 Duct4.Fl_O 71.49 5.675 979.07 237.71 0.0110 254.37 5.488 970.21 2018.9 0.2207 1.37465 +FS_9 Core_Nozz.Fl_O 71.49 5.675 979.07 237.71 0.0110 254.37 4.364 911.18 863.0 0.6284 1.37465 +FS_15 BypBld.Fl_O 473.15 7.353 482.38 115.26 0.0000 911.91 6.366 462.88 3795.6 0.4583 1.40106 +FS_17 Duct5.Fl_O 473.15 7.298 482.38 115.26 0.0000 918.80 6.319 462.88 3824.3 0.4583 1.40106 +FS_19 Byp_Nozz.Fl_O 473.15 7.298 482.38 115.26 0.0000 918.80 4.364 416.32 2706.4 0.8892 1.40106 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1331.13 1.328 0.9108 2981.340 1.0928 0.9143 -7544.2 47.59 21.20 +LPC 136.63 1.897 0.8465 2851.977 1.2373 0.8597 -2747.1 24.96 13.95 +HPC 80.32 4.955 0.8648 6218.840 1.6587 0.8909 -9583.3 29.92 30.13 +HPT 27.37 2.759 0.9153 157.601 1.2602 0.9045 9583.4 +LPT 72.94 4.089 0.9187 74.212 1.4029 0.9030 10291.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2552.27 1.228 0.9409 0.756 2.0673 0.5215 1.4369 0.9679 3943.9586 +LPC 146.56 1.275 0.8818 0.779 1.5878 0.9323 3.2631 0.9600 3662.6571 +HPC 190.94 19.284 0.8532 0.978 2.1684 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.140 0.9337 102.932 5.1399 1.4085 0.4249 0.9803 1.5311 +LPT 151.56 5.310 0.9175 91.494 5.3097 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4584.63 10092.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 735.85 176.24 21.923 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 735.85 176.24 21.923 +Duct1 0.0025 0.3423 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 735.85 176.24 21.923 +Duct2 0.0025 0.4072 365.99 +Duct3 0.0050 0.2989 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3065 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.4750 989.99 238.50 68.779 +Duct5 0.0075 0.4583 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.8893 989.99 238.50 68.779 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 482.38 115.26 7.353 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6909 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6671.0 7545.0 9583.4 +LP_Shaft 2750.4 19652.6 10291.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1791.70 0.9940 0.0550 0.77482 0.01204 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.672 0.9975 1.0000 0.9975 2706.36 0.889 887.6 13053.0 +Core_Nozz 1.300 0.9999 1.0000 0.9999 862.88 0.628 922.7 2050.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 279 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 30000.0 0.00 471.67 2505.3 0.6602 1653.90 7.7661 597.05 8.687 1535.1 1500.5 1167.6 + core size:21.42 Q: 158.50 Maximum Thrust: 12526.4 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 471.67 5.567 441.43 105.45 0.0000 1148.65 4.364 411.69 3976.1 0.6000 1.40134 +FS_2 Inlet.Fl_O 471.67 5.539 441.43 105.45 0.0000 1154.43 5.083 430.69 5943.4 0.3525 1.40134 +FS_21 Fan.Fl_O 471.67 6.603 466.87 111.54 0.0000 995.90 5.879 451.58 4515.2 0.4108 1.40123 +FS_13 Splitter.Fl_O2 417.86 6.603 466.87 111.54 0.0000 882.29 5.784 449.49 3795.6 0.4390 1.40123 +FS_22 Splitter.Fl_O1 53.81 6.603 466.87 111.54 0.0000 113.61 6.256 459.70 719.5 0.2788 1.40123 +FS_23 Duct1.Fl_O 53.81 6.587 466.87 111.54 0.0000 113.89 6.240 459.70 721.3 0.2788 1.40123 +FS_24 LPC.Fl_O 53.81 10.667 549.49 131.34 0.0000 76.30 9.637 533.78 366.0 0.3835 1.39992 +FS_25 Duct2.Fl_O 53.81 10.640 549.49 131.34 0.0000 76.49 9.613 533.78 366.9 0.3835 1.39992 +FS_3 HPC.Fl_O 53.81 48.363 890.58 213.96 0.0000 21.42 45.042 873.05 119.9 0.3217 1.38740 +FS_36 Bld3.Fl_O 48.96 48.363 890.58 213.96 0.0000 19.50 45.042 873.05 109.1 0.3217 1.38740 +FS_4 Burner.Fl_O 49.42 45.703 1535.13 382.03 0.0094 27.34 45.410 1532.61 483.4 0.0980 1.34181 +FS_45 HPT.Fl_O 54.27 16.360 1167.61 285.12 0.0085 73.14 15.393 1148.76 439.1 0.2998 1.36421 +FS_48 Duct3.Fl_O 54.27 16.278 1167.61 285.12 0.0085 73.51 15.316 1148.76 441.4 0.2998 1.36421 +FS_5 LPT.Fl_O 54.27 5.085 879.80 212.55 0.0085 204.26 4.883 869.97 1477.4 0.2430 1.38243 +FS_7 Duct4.Fl_O 54.27 5.034 879.80 212.55 0.0085 206.32 4.927 874.58 2018.9 0.1767 1.38243 +FS_9 Core_Nozz.Fl_O 54.27 5.034 879.80 212.55 0.0085 206.32 4.364 845.68 863.0 0.4586 1.38243 +FS_15 BypBld.Fl_O 417.86 6.603 466.87 111.54 0.0000 882.29 5.784 449.49 3795.6 0.4390 1.40123 +FS_17 Duct5.Fl_O 417.86 6.554 466.87 111.54 0.0000 888.96 5.741 449.49 3824.3 0.4390 1.40123 +FS_19 Byp_Nozz.Fl_O 417.86 6.554 466.87 111.54 0.0000 888.96 4.364 415.54 2706.4 0.7846 1.40123 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1154.43 1.192 0.8953 2476.704 1.0576 0.8979 -4064.7 56.96 22.14 +LPC 113.89 1.619 0.8356 2408.267 1.1770 0.8464 -1507.4 27.64 11.02 +HPC 76.49 4.545 0.8631 6149.125 1.6207 0.8883 -6289.2 36.61 37.07 +HPT 27.34 2.794 0.9162 161.539 1.2734 0.9050 6289.2 +LPT 73.51 3.201 0.9084 66.866 1.3271 0.8938 5572.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2213.47 1.134 0.9249 0.628 2.2140 0.5215 1.4369 0.9679 3943.9586 +LPC 122.17 1.190 0.8704 0.658 1.5899 0.9323 3.2631 0.9600 3662.6571 +HPC 181.85 17.389 0.8514 0.967 2.2296 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.222 0.9346 105.504 5.2215 1.4085 0.4249 0.9803 1.5311 +LPT 152.74 4.071 0.9072 82.438 4.0705 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3976.06 8752.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 669.73 160.26 16.167 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 669.73 160.26 16.167 +Duct1 0.0025 0.2788 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 669.73 160.26 16.167 +Duct2 0.0025 0.3835 365.99 +Duct3 0.0050 0.2998 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2430 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.8832 890.58 213.96 48.363 +Duct5 0.0075 0.4390 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.9593 890.58 213.96 48.363 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 466.87 111.54 6.603 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.7661 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6329.2 5218.9 6289.2 +LP_Shaft 2284.8 12808.4 5572.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1535.13 0.9940 0.0550 0.45942 0.00938 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.502 0.9975 1.0000 0.9975 2706.36 0.785 782.4 10161.7 +Core_Nozz 1.154 0.9999 1.0000 0.9999 862.88 0.459 650.0 1096.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 280 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 11/ 21/ 1/ 9 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 30000.0 0.00 397.97 626.3 1.2776 800.15 9.3727 597.05 5.541 1230.8 1206.0 929.0 + core size:22.38 Q: 158.50 Maximum Thrust: 12526.4 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 397.97 5.567 441.43 105.45 0.0000 969.18 4.364 411.69 3354.8 0.6000 1.40134 +FS_2 Inlet.Fl_O 397.97 5.539 441.43 105.45 0.0000 974.06 5.224 434.07 5943.4 0.2905 1.40134 +FS_21 Fan.Fl_O 397.97 5.967 453.06 108.24 0.0000 916.06 5.425 440.88 4515.2 0.3711 1.40131 +FS_13 Splitter.Fl_O2 359.60 5.967 453.06 108.24 0.0000 827.75 5.329 438.62 3795.6 0.4050 1.40131 +FS_22 Splitter.Fl_O1 38.37 5.967 453.06 108.24 0.0000 88.32 5.782 448.99 719.5 0.2126 1.40131 +FS_23 Duct1.Fl_O 38.37 5.952 453.06 108.24 0.0000 88.54 5.767 448.99 721.3 0.2126 1.40131 +FS_24 LPC.Fl_O 38.37 7.952 500.71 119.65 0.0000 69.67 7.325 489.08 366.0 0.3443 1.40081 +FS_25 Duct2.Fl_O 38.37 7.932 500.71 119.65 0.0000 69.84 7.307 489.08 366.9 0.3443 1.40081 +FS_3 HPC.Fl_O 38.37 30.846 777.35 186.31 0.0000 22.38 28.517 760.31 119.9 0.3375 1.39305 +FS_36 Bld3.Fl_O 34.91 30.846 777.35 186.31 0.0000 20.36 28.517 760.31 109.1 0.3375 1.39305 +FS_4 Burner.Fl_O 35.14 29.150 1230.85 300.86 0.0064 27.29 28.964 1228.75 483.4 0.0971 1.36170 +FS_45 HPT.Fl_O 38.59 10.324 928.99 224.33 0.0058 73.51 9.708 913.34 439.1 0.2996 1.38120 +FS_48 Duct3.Fl_O 38.59 10.273 928.99 224.33 0.0058 73.88 9.660 913.34 441.4 0.2996 1.38120 +FS_5 LPT.Fl_O 38.59 4.704 766.24 184.26 0.0058 146.55 4.609 761.90 1477.4 0.1708 1.38997 +FS_7 Duct4.Fl_O 38.59 4.657 766.24 184.26 0.0058 148.03 4.606 763.90 2018.9 0.1253 1.38997 +FS_9 Core_Nozz.Fl_O 38.59 4.657 766.24 184.26 0.0058 148.03 4.364 752.41 862.9 0.3069 1.38997 +FS_15 BypBld.Fl_O 359.60 5.967 453.06 108.24 0.0000 827.75 5.329 438.62 3795.6 0.4050 1.40131 +FS_17 Duct5.Fl_O 359.60 5.922 453.06 108.24 0.0000 834.00 5.289 438.62 3824.3 0.4050 1.40131 +FS_19 Byp_Nozz.Fl_O 359.60 5.922 453.06 108.24 0.0000 834.00 4.364 415.12 2706.4 0.6749 1.40131 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 974.06 1.077 0.8166 1867.610 1.0264 0.8186 -1568.6 84.00 21.57 +LPC 88.54 1.336 0.8221 1843.466 1.1052 0.8293 -619.3 36.46 9.36 +HPC 69.84 3.889 0.8544 6026.883 1.5525 0.8790 -3618.6 49.13 50.11 +HPT 27.29 2.823 0.9179 168.786 1.2899 0.9063 3618.5 +LPT 73.88 2.184 0.8966 56.528 1.2124 0.8859 2188.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1867.62 1.054 0.8437 0.474 2.5531 0.5215 1.4369 0.9679 3943.9586 +LPC 94.97 1.103 0.8563 0.503 1.6932 0.9323 3.2631 0.9600 3662.6571 +HPC 166.04 14.355 0.8429 0.948 2.3781 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.292 0.9363 110.237 5.2916 1.4085 0.4249 0.9803 1.5311 +LPT 153.52 2.652 0.8954 69.692 2.6517 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3354.81 7385.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 597.94 142.98 11.289 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 597.94 142.98 11.289 +Duct1 0.0025 0.2126 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 597.94 142.98 11.289 +Duct2 0.0025 0.3443 365.99 +Duct3 0.0050 0.2996 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1708 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.3429 777.35 186.31 30.846 +Duct5 0.0075 0.4050 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.1102 777.35 186.31 30.846 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 453.06 108.24 5.967 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.3727 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 5921.6 3209.4 3618.5 +LP_Shaft 1722.9 6669.7 2188.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1230.85 0.9940 0.0550 0.22226 0.00637 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.357 0.9975 1.0000 0.9975 2706.36 0.675 672.7 7518.2 +Core_Nozz 1.067 0.9999 1.0000 0.9999 862.88 0.307 411.3 493.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 281 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 4/ 14/ 1/ 2 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 30000.0 0.00 735.44 12895.0 0.5844 7536.29 5.0409 696.56 22.720 2393.5 2332.6 1868.0 + core size:19.94 Q: 215.73 Maximum Thrust: 12895.0 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 735.44 6.055 452.17 108.02 0.0000 1666.72 4.364 411.69 5314.0 0.7000 1.40131 +FS_2 Inlet.Fl_O 735.44 6.024 452.17 108.02 0.0000 1675.11 4.809 423.91 5943.4 0.5763 1.40131 +FS_21 Fan.Fl_O 735.44 9.907 531.91 127.13 0.0000 1104.74 8.518 509.41 4515.2 0.4696 1.40027 +FS_13 Splitter.Fl_O2 613.70 9.907 531.91 127.13 0.0000 921.86 8.542 509.83 3795.6 0.4650 1.40027 +FS_22 Splitter.Fl_O1 121.74 9.907 531.91 127.13 0.0000 182.88 8.381 507.06 719.5 0.4946 1.40027 +FS_23 Duct1.Fl_O 121.74 9.883 531.91 127.13 0.0000 183.34 8.360 507.06 721.3 0.4946 1.40027 +FS_24 LPC.Fl_O 121.74 24.593 713.63 170.86 0.0000 85.34 21.517 687.09 366.0 0.4416 1.39556 +FS_25 Duct2.Fl_O 121.74 24.531 713.63 170.86 0.0000 85.55 21.464 687.09 366.9 0.4416 1.39556 +FS_3 HPC.Fl_O 121.74 137.561 1219.16 296.20 0.0000 19.94 129.462 1199.44 119.9 0.2990 1.36694 +FS_36 Bld3.Fl_O 110.79 137.561 1219.16 296.20 0.0000 18.15 129.462 1199.44 109.1 0.2990 1.36694 +FS_4 Burner.Fl_O 112.88 129.995 2393.51 630.00 0.0189 27.41 129.157 2389.91 483.4 0.0997 1.30333 +FS_45 HPT.Fl_O 123.84 48.701 1868.03 477.24 0.0172 70.92 46.003 1842.30 439.1 0.2946 1.32102 +FS_48 Duct3.Fl_O 123.84 48.458 1868.03 477.24 0.0172 71.27 45.773 1842.30 441.4 0.2946 1.32102 +FS_5 LPT.Fl_O 123.84 9.924 1296.05 320.80 0.0172 289.89 9.084 1266.61 1477.4 0.3636 1.35029 +FS_7 Duct4.Fl_O 123.84 9.825 1296.05 320.80 0.0172 292.82 9.392 1280.98 2018.9 0.2589 1.35029 +FS_9 Core_Nozz.Fl_O 123.84 9.825 1296.05 320.80 0.0172 292.82 5.248 1099.18 862.9 1.0000 1.35029 +FS_15 BypBld.Fl_O 613.70 9.907 531.91 127.13 0.0000 921.86 8.542 509.83 3795.6 0.4650 1.40027 +FS_17 Duct5.Fl_O 613.70 9.833 531.91 127.13 0.0000 928.83 8.478 509.83 3824.3 0.4650 1.40027 +FS_19 Byp_Nozz.Fl_O 613.70 9.833 531.91 127.13 0.0000 928.83 5.192 443.06 2706.4 1.0000 1.40027 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.645 0.8675 3944.235 1.1764 0.8766 -19877.0 24.71 17.45 +LPC 183.34 2.489 0.8683 3636.578 1.3416 0.8840 -7533.5 28.36 23.28 +HPC 85.55 5.608 0.8651 6325.586 1.7084 0.8922 -21590.0 20.10 20.16 +HPT 27.41 2.669 0.9133 151.661 1.2334 0.9035 21589.9 +LPT 71.27 4.883 0.9323 85.207 1.4413 0.9180 27410.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8963 1.000 2.3706 0.5215 1.4369 0.9679 3943.9586 +LPC 196.66 1.456 0.9045 0.993 1.7661 0.9323 3.2631 0.9600 3662.6571 +HPC 203.38 22.300 0.8535 0.995 2.0421 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.929 0.9316 99.052 4.9287 1.4085 0.4249 0.9803 1.5311 +LPT 148.10 6.417 0.9311 105.049 6.4166 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5313.97 15922.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 893.73 214.73 41.090 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 893.73 214.73 41.090 +Duct1 0.0025 0.4946 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 893.73 214.73 41.090 +Duct2 0.0025 0.4416 365.99 +Duct3 0.0050 0.2946 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.2611 1219.16 296.20 137.561 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.6960 1219.16 296.20 137.561 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 531.91 127.13 9.907 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0409 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7419.8 15282.5 21589.9 +LP_Shaft 3682.7 39091.6 27410.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2393.51 0.9940 0.0550 2.09342 0.01890 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.253 0.9972 1.0000 0.9975 2706.36 1.000 1029.8 21883.4 +Core_Nozz 2.251 0.9991 1.0000 0.9999 862.88 1.000 1603.3 6933.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 282 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 30000.0 0.00 716.79 11605.1 0.5738 6659.32 5.3058 696.56 20.806 2306.2 2247.8 1793.2 + core size:20.04 Q: 215.73 Maximum Thrust: 12895.0 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 716.79 6.055 452.17 108.02 0.0000 1624.45 4.364 411.69 5179.2 0.7000 1.40131 +FS_2 Inlet.Fl_O 716.79 6.024 452.17 108.02 0.0000 1632.63 4.891 425.97 5943.4 0.5536 1.40131 +FS_21 Fan.Fl_O 716.79 9.681 525.82 125.67 0.0000 1095.61 8.350 504.04 4515.2 0.4644 1.40039 +FS_13 Splitter.Fl_O2 603.12 9.681 525.82 125.67 0.0000 921.86 8.347 503.98 3795.6 0.4650 1.40039 +FS_22 Splitter.Fl_O1 113.67 9.681 525.82 125.67 0.0000 173.75 8.365 504.30 719.5 0.4614 1.40039 +FS_23 Duct1.Fl_O 113.67 9.656 525.82 125.67 0.0000 174.18 8.344 504.30 721.3 0.4614 1.40039 +FS_24 LPC.Fl_O 113.67 22.492 691.35 165.48 0.0000 85.75 19.647 665.29 366.0 0.4442 1.39631 +FS_25 Duct2.Fl_O 113.67 22.436 691.35 165.48 0.0000 85.96 19.598 665.29 366.9 0.4442 1.39631 +FS_3 HPC.Fl_O 113.67 125.972 1184.05 287.25 0.0000 20.04 118.478 1164.61 119.9 0.3004 1.36915 +FS_36 Bld3.Fl_O 103.44 125.972 1184.05 287.25 0.0000 18.23 118.478 1164.61 109.1 0.3004 1.36915 +FS_4 Burner.Fl_O 105.29 119.043 2306.18 603.62 0.0179 27.41 118.275 2302.68 483.4 0.0996 1.30632 +FS_45 HPT.Fl_O 115.52 44.154 1793.21 455.78 0.0163 71.49 41.665 1767.86 439.1 0.2968 1.32480 +FS_48 Duct3.Fl_O 115.52 43.933 1793.21 455.78 0.0163 71.85 41.457 1767.86 441.4 0.2968 1.32480 +FS_5 LPT.Fl_O 115.52 9.063 1245.12 307.15 0.0163 290.24 8.294 1216.55 1477.4 0.3636 1.35410 +FS_7 Duct4.Fl_O 115.52 8.972 1245.12 307.15 0.0163 293.17 8.576 1230.49 2018.9 0.2589 1.35410 +FS_9 Core_Nozz.Fl_O 115.52 8.972 1245.12 307.15 0.0163 293.17 4.789 1054.36 862.9 1.0000 1.35410 +FS_15 BypBld.Fl_O 603.12 9.681 525.82 125.67 0.0000 921.86 8.347 503.98 3795.6 0.4650 1.40039 +FS_17 Duct5.Fl_O 603.12 9.608 525.82 125.67 0.0000 928.83 8.284 503.98 3824.3 0.4650 1.40039 +FS_19 Byp_Nozz.Fl_O 603.12 9.608 525.82 125.67 0.0000 928.83 5.073 437.97 2706.4 1.0000 1.40039 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1632.63 1.607 0.8926 3741.084 1.1629 0.8996 -17891.0 28.24 17.74 +LPC 174.18 2.329 0.8660 3469.203 1.3148 0.8809 -6402.9 28.89 22.16 +HPC 85.96 5.615 0.8640 6335.890 1.7127 0.8915 -19585.6 20.52 20.55 +HPT 27.41 2.696 0.9138 152.323 1.2383 0.9039 19585.7 +LPT 71.85 4.848 0.9278 82.487 1.4402 0.9125 24292.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3130.12 1.422 0.9222 0.949 2.1740 0.5215 1.4369 0.9679 3943.9586 +LPC 186.83 1.407 0.9021 0.947 1.7519 0.9323 3.2631 0.9600 3662.6571 +HPC 204.36 22.333 0.8524 0.997 2.0717 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.992 0.9322 99.485 4.9919 1.4085 0.4249 0.9803 1.5311 +LPT 149.30 6.367 0.9266 101.696 6.3673 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5179.20 15518.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 866.69 208.10 37.604 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 866.69 208.10 37.604 +Duct1 0.0025 0.4614 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 866.69 208.10 37.604 +Duct2 0.0025 0.4442 365.99 +Duct3 0.0050 0.2968 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.9785 1184.05 287.25 125.972 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.2520 1184.05 287.25 125.972 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 525.82 125.67 9.681 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3058 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7314.9 14062.5 19585.7 +LP_Shaft 3493.0 36526.5 24292.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2306.18 0.9940 0.0550 1.84981 0.01788 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.202 0.9974 1.0000 0.9975 2706.36 1.000 1023.8 21111.9 +Core_Nozz 2.056 0.9997 1.0000 0.9999 862.88 1.000 1572.3 6011.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 283 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 30000.0 0.00 695.83 10316.0 0.5692 5871.82 5.5112 696.56 19.164 2216.8 2161.3 1719.4 + core size:20.19 Q: 215.73 Maximum Thrust: 12895.0 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 695.83 6.055 452.17 108.02 0.0000 1576.93 4.364 411.69 5027.7 0.7000 1.40131 +FS_2 Inlet.Fl_O 695.83 6.024 452.17 108.02 0.0000 1584.87 4.976 428.08 5943.4 0.5295 1.40131 +FS_21 Fan.Fl_O 695.83 9.404 520.27 124.34 0.0000 1089.12 8.129 499.04 4515.2 0.4608 1.40049 +FS_13 Splitter.Fl_O2 588.96 9.404 520.27 124.34 0.0000 921.85 8.108 498.67 3795.6 0.4650 1.40049 +FS_22 Splitter.Fl_O1 106.87 9.404 520.27 124.34 0.0000 167.27 8.237 500.92 719.5 0.4391 1.40049 +FS_23 Duct1.Fl_O 106.87 9.380 520.27 124.34 0.0000 167.69 8.216 500.92 721.3 0.4391 1.40049 +FS_24 LPC.Fl_O 106.87 21.156 677.67 162.17 0.0000 84.85 18.545 652.77 366.0 0.4382 1.39679 +FS_25 Duct2.Fl_O 106.87 21.103 677.67 162.17 0.0000 85.07 18.499 652.77 366.9 0.4382 1.39679 +FS_3 HPC.Fl_O 106.87 116.031 1154.12 279.66 0.0000 20.19 109.015 1134.78 119.9 0.3028 1.37103 +FS_36 Bld3.Fl_O 97.25 116.031 1154.12 279.66 0.0000 18.37 109.015 1134.78 109.1 0.3028 1.37103 +FS_4 Burner.Fl_O 98.88 109.649 2216.81 576.83 0.0168 27.40 108.943 2213.42 483.4 0.0994 1.30948 +FS_45 HPT.Fl_O 108.50 40.472 1719.41 434.77 0.0153 71.73 38.175 1694.70 439.1 0.2975 1.32878 +FS_48 Duct3.Fl_O 108.50 40.270 1719.41 434.77 0.0153 72.09 37.984 1694.70 441.4 0.2975 1.32878 +FS_5 LPT.Fl_O 108.50 8.314 1191.44 292.89 0.0153 290.66 7.607 1163.79 1477.4 0.3636 1.35819 +FS_7 Duct4.Fl_O 108.50 8.231 1191.44 292.89 0.0153 293.59 7.867 1177.28 2018.9 0.2589 1.35819 +FS_9 Core_Nozz.Fl_O 108.50 8.231 1191.44 292.89 0.0153 293.59 4.390 1007.25 862.9 1.0000 1.35819 +FS_15 BypBld.Fl_O 588.96 9.404 520.27 124.34 0.0000 921.85 8.108 498.67 3795.6 0.4650 1.40049 +FS_17 Duct5.Fl_O 588.96 9.333 520.27 124.34 0.0000 928.81 8.047 498.67 3824.3 0.4650 1.40049 +FS_19 Byp_Nozz.Fl_O 588.96 9.333 520.27 124.34 0.0000 928.81 4.928 433.35 2706.4 1.0000 1.40049 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1584.87 1.561 0.9024 3612.241 1.1506 0.9084 -16058.9 31.72 18.34 +LPC 167.69 2.255 0.8631 3367.527 1.3025 0.8778 -5721.3 28.04 20.47 +HPC 85.07 5.498 0.8648 6312.698 1.7031 0.8920 -17763.7 22.16 22.24 +HPT 27.40 2.709 0.9145 153.255 1.2422 0.9044 17763.6 +LPT 72.09 4.843 0.9258 81.337 1.4431 0.9099 21780.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3038.80 1.390 0.9323 0.916 2.0958 0.5215 1.4369 0.9679 3943.9586 +LPC 179.87 1.385 0.8990 0.919 1.7157 0.9323 3.2631 0.9600 3662.6571 +HPC 202.24 21.795 0.8532 0.993 2.0975 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.023 0.9328 100.094 5.0229 1.4085 0.4249 0.9803 1.5311 +LPT 149.80 6.361 0.9246 100.279 6.3614 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5027.71 15064.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 847.05 203.29 35.010 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 847.05 203.29 35.010 +Duct1 0.0025 0.4391 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 847.05 203.29 35.010 +Duct2 0.0025 0.4382 365.99 +Duct3 0.0050 0.2975 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.7403 1154.12 279.66 116.031 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.8776 1154.12 279.66 116.031 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 520.27 124.34 9.404 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5112 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7215.7 12929.6 17763.6 +LP_Shaft 3372.7 33917.3 21780.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2216.81 0.9940 0.0550 1.63106 0.01677 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.139 0.9975 1.0000 0.9975 2706.36 1.000 1018.4 20168.9 +Core_Nozz 1.886 0.9999 1.0000 0.9999 862.88 1.000 1538.8 5211.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:52 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 284 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 30000.0 0.00 648.77 7736.9 0.5738 4439.28 5.9932 696.56 15.920 2036.6 1987.0 1573.1 + core size:20.53 Q: 215.73 Maximum Thrust: 12895.0 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 648.77 6.055 452.17 108.02 0.0000 1470.30 4.364 411.69 4687.7 0.7000 1.40131 +FS_2 Inlet.Fl_O 648.77 6.024 452.17 108.02 0.0000 1477.70 5.146 432.20 5943.4 0.4798 1.40131 +FS_21 Fan.Fl_O 648.77 8.778 508.66 121.55 0.0000 1075.67 7.623 488.54 4515.2 0.4533 1.40069 +FS_13 Splitter.Fl_O2 556.00 8.778 508.66 121.55 0.0000 921.85 7.568 487.53 3795.6 0.4649 1.40069 +FS_22 Splitter.Fl_O1 92.77 8.778 508.66 121.55 0.0000 153.82 7.881 493.21 719.5 0.3953 1.40069 +FS_23 Duct1.Fl_O 92.77 8.756 508.66 121.55 0.0000 154.20 7.861 493.21 721.3 0.3953 1.40069 +FS_24 LPC.Fl_O 92.77 18.596 651.45 155.85 0.0000 82.17 16.469 629.30 366.0 0.4205 1.39776 +FS_25 Duct2.Fl_O 92.77 18.550 651.45 155.85 0.0000 82.37 16.427 629.30 366.9 0.4205 1.39776 +FS_3 HPC.Fl_O 92.77 96.391 1092.27 264.05 0.0000 20.53 90.353 1073.15 119.9 0.3080 1.37493 +FS_36 Bld3.Fl_O 84.42 96.391 1092.27 264.05 0.0000 18.68 90.353 1073.15 109.1 0.3080 1.37493 +FS_4 Burner.Fl_O 85.66 91.089 2036.60 523.63 0.0146 27.38 90.503 2033.44 483.4 0.0991 1.31648 +FS_45 HPT.Fl_O 94.01 33.409 1573.10 393.80 0.0133 72.01 31.498 1549.87 439.1 0.2978 1.33718 +FS_48 Duct3.Fl_O 94.01 33.242 1573.10 393.80 0.0133 72.38 31.341 1549.87 441.4 0.2978 1.33718 +FS_5 LPT.Fl_O 94.01 7.023 1091.12 266.57 0.0133 285.31 6.450 1066.49 1477.4 0.3547 1.36593 +FS_7 Duct4.Fl_O 94.01 6.953 1091.12 266.57 0.0133 288.19 6.657 1078.47 2018.9 0.2530 1.36593 +FS_9 Core_Nozz.Fl_O 94.01 6.953 1091.12 266.57 0.0133 288.19 4.364 961.97 862.9 0.8505 1.36593 +FS_15 BypBld.Fl_O 556.00 8.778 508.66 121.55 0.0000 921.85 7.568 487.53 3795.6 0.4649 1.40069 +FS_17 Duct5.Fl_O 556.00 8.712 508.66 121.55 0.0000 928.82 7.511 487.53 3824.3 0.4649 1.40069 +FS_19 Byp_Nozz.Fl_O 556.00 8.712 508.66 121.55 0.0000 928.82 4.600 423.67 2706.4 1.0000 1.40069 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1477.70 1.457 0.9105 3359.587 1.1249 0.9152 -12419.0 39.73 19.78 +LPC 154.20 2.124 0.8546 3167.526 1.2807 0.8691 -4502.0 25.40 16.71 +HPC 82.37 5.196 0.8658 6255.275 1.6767 0.8923 -14202.2 26.16 26.31 +HPT 27.38 2.726 0.9148 155.342 1.2490 0.9046 14202.3 +LPT 72.38 4.733 0.9212 79.088 1.4417 0.9047 16921.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2833.26 1.318 0.9406 0.852 2.0412 0.5215 1.4369 0.9679 3943.9586 +LPC 165.40 1.344 0.8902 0.865 1.6267 0.9323 3.2631 0.9600 3662.6571 +HPC 195.82 20.399 0.8542 0.984 2.1331 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.063 0.9332 101.456 5.0634 1.4085 0.4249 0.9803 1.5311 +LPT 150.39 6.208 0.9200 97.506 6.2079 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4687.73 14045.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 807.83 193.72 29.953 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 807.83 193.72 29.953 +Duct1 0.0025 0.3953 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 807.83 193.72 29.953 +Duct2 0.0025 0.4205 365.99 +Duct3 0.0050 0.2978 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3547 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.2470 1092.27 264.05 96.391 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.1025 1092.27 264.05 96.391 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 508.66 121.55 8.778 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9932 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7010.4 10640.2 14202.3 +LP_Shaft 3136.8 28331.8 16921.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2036.60 0.9940 0.0550 1.23313 0.01461 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.996 0.9976 1.0000 0.9975 2706.36 1.000 1007.0 18040.2 +Core_Nozz 1.593 0.9999 1.0000 0.9999 862.88 0.850 1280.9 3742.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 285 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 30000.0 0.00 593.76 5158.2 0.6038 3114.58 6.7073 696.56 12.530 1835.1 1791.8 1409.4 + core size:20.91 Q: 215.73 Maximum Thrust: 12895.0 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 593.76 6.055 452.17 108.02 0.0000 1345.63 4.364 411.69 4290.3 0.7000 1.40131 +FS_2 Inlet.Fl_O 593.76 6.024 452.17 108.02 0.0000 1352.41 5.313 436.19 5943.4 0.4272 1.40131 +FS_21 Fan.Fl_O 593.76 8.055 495.27 118.35 0.0000 1058.58 7.035 476.45 4515.2 0.4439 1.40089 +FS_13 Splitter.Fl_O2 516.73 8.055 495.27 118.35 0.0000 921.23 6.947 474.73 3795.6 0.4645 1.40089 +FS_22 Splitter.Fl_O1 77.04 8.055 495.27 118.35 0.0000 137.35 7.416 483.70 719.5 0.3454 1.40089 +FS_23 Duct1.Fl_O 77.04 8.035 495.27 118.35 0.0000 137.69 7.398 483.70 721.3 0.3454 1.40089 +FS_24 LPC.Fl_O 77.04 15.536 616.78 147.51 0.0000 79.47 13.891 597.40 366.0 0.4032 1.39874 +FS_25 Duct2.Fl_O 77.04 15.497 616.78 147.51 0.0000 79.67 13.856 597.40 366.9 0.4032 1.39874 +FS_3 HPC.Fl_O 77.04 75.866 1018.27 245.53 0.0000 20.91 70.921 999.54 119.9 0.3139 1.37957 +FS_36 Bld3.Fl_O 70.11 75.866 1018.27 245.53 0.0000 19.03 70.921 999.54 109.1 0.3139 1.37957 +FS_4 Burner.Fl_O 70.97 71.693 1835.13 465.56 0.0123 27.36 71.232 1832.23 483.4 0.0987 1.32569 +FS_45 HPT.Fl_O 77.90 26.047 1409.38 349.05 0.0112 72.46 24.538 1387.83 439.1 0.2986 1.34742 +FS_48 Duct3.Fl_O 77.90 25.917 1409.38 349.05 0.0112 72.82 24.415 1387.83 441.4 0.2986 1.34742 +FS_5 LPT.Fl_O 77.90 6.013 994.08 241.53 0.0112 263.58 5.601 975.06 1477.4 0.3228 1.37352 +FS_7 Duct4.Fl_O 77.90 5.953 994.08 241.53 0.0112 266.24 5.739 984.20 2018.9 0.2317 1.37352 +FS_9 Core_Nozz.Fl_O 77.90 5.953 994.08 241.53 0.0112 266.24 4.364 913.19 862.8 0.6857 1.37352 +FS_15 BypBld.Fl_O 516.73 8.055 495.27 118.35 0.0000 921.23 6.947 474.73 3795.6 0.4645 1.40089 +FS_17 Duct5.Fl_O 516.73 7.995 495.27 118.35 0.0000 928.20 6.895 474.73 3824.3 0.4645 1.40089 +FS_19 Byp_Nozz.Fl_O 516.73 7.995 495.27 118.35 0.0000 928.20 4.364 416.45 2706.3 0.9713 1.40089 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1352.41 1.337 0.9096 3025.312 1.0953 0.9132 -8671.1 47.68 21.59 +LPC 137.69 1.934 0.8451 2890.659 1.2453 0.8587 -3178.8 23.68 13.47 +HPC 79.67 4.895 0.8648 6208.354 1.6509 0.8907 -10684.4 30.68 30.90 +HPT 27.36 2.752 0.9154 158.038 1.2582 0.9046 10684.4 +LPT 72.82 4.310 0.9174 75.242 1.4178 0.9009 11850.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2593.06 1.235 0.9397 0.767 2.0831 0.5215 1.4369 0.9679 3943.9586 +LPC 147.69 1.286 0.8802 0.789 1.5617 0.9323 3.2631 0.9600 3662.6571 +HPC 189.40 19.008 0.8531 0.977 2.1675 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.125 0.9337 103.218 5.1246 1.4085 0.4249 0.9803 1.5311 +LPT 151.31 5.617 0.9162 92.764 5.6172 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4290.26 12854.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 758.86 181.82 24.341 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 758.86 181.82 24.341 +Duct1 0.0025 0.3454 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 758.86 181.82 24.341 +Duct2 0.0025 0.4032 365.99 +Duct3 0.0050 0.2986 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3228 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.6964 1018.27 245.53 75.866 +Duct5 0.0075 0.4645 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.2372 1018.27 245.53 75.866 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 495.27 118.35 8.055 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.7073 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6770.1 8288.7 10684.4 +LP_Shaft 2824.7 22033.7 11850.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1835.13 0.9940 0.0550 0.86516 0.01234 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.832 0.9975 1.0000 0.9975 2706.36 0.971 969.7 15572.9 +Core_Nozz 1.364 0.9999 1.0000 0.9999 862.88 0.686 1007.8 2440.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 286 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 30000.0 0.00 524.45 2579.0 0.7213 1860.20 7.8616 696.56 8.903 1575.3 1540.1 1200.6 + core size:21.49 Q: 215.73 Maximum Thrust: 12895.0 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 524.45 6.055 452.17 108.02 0.0000 1188.55 4.364 411.69 3789.4 0.7000 1.40131 +FS_2 Inlet.Fl_O 524.45 6.024 452.17 108.02 0.0000 1194.53 5.489 440.27 5943.4 0.3669 1.40131 +FS_21 Fan.Fl_O 524.45 7.234 479.51 114.57 0.0000 1024.47 6.386 462.69 4515.2 0.4256 1.40110 +FS_13 Splitter.Fl_O2 465.27 7.234 479.51 114.57 0.0000 908.86 6.270 460.29 3795.6 0.4562 1.40110 +FS_22 Splitter.Fl_O1 59.18 7.234 479.51 114.57 0.0000 115.61 6.839 471.86 719.5 0.2842 1.40110 +FS_23 Duct1.Fl_O 59.18 7.216 479.51 114.57 0.0000 115.90 6.822 471.86 721.3 0.2842 1.40110 +FS_24 LPC.Fl_O 59.18 12.084 570.94 136.49 0.0000 75.51 10.944 555.02 366.0 0.3788 1.39952 +FS_25 Duct2.Fl_O 59.18 12.054 570.94 136.49 0.0000 75.70 10.917 555.02 366.9 0.3788 1.39952 +FS_3 HPC.Fl_O 59.18 53.907 919.97 221.18 0.0000 21.49 50.181 901.79 119.9 0.3230 1.38564 +FS_36 Bld3.Fl_O 53.86 53.907 919.97 221.18 0.0000 19.55 50.181 901.79 109.1 0.3230 1.38564 +FS_4 Burner.Fl_O 54.37 50.942 1575.28 392.94 0.0096 27.34 50.616 1572.71 483.4 0.0980 1.33961 +FS_45 HPT.Fl_O 59.70 18.287 1200.63 293.66 0.0087 72.99 17.211 1181.42 439.1 0.2994 1.36198 +FS_48 Duct3.Fl_O 59.70 18.195 1200.63 293.66 0.0087 73.36 17.125 1181.42 441.4 0.2994 1.36198 +FS_5 LPT.Fl_O 59.70 5.237 887.26 214.42 0.0087 219.12 4.995 875.75 1477.4 0.2622 1.38186 +FS_7 Duct4.Fl_O 59.70 5.185 887.26 214.42 0.0087 221.33 5.057 881.18 2018.9 0.1901 1.38186 +FS_9 Core_Nozz.Fl_O 59.70 5.185 887.26 214.42 0.0087 221.33 4.364 845.96 862.9 0.5047 1.38186 +FS_15 BypBld.Fl_O 465.27 7.234 479.51 114.57 0.0000 908.86 6.270 460.29 3795.6 0.4562 1.40110 +FS_17 Duct5.Fl_O 465.27 7.179 479.51 114.57 0.0000 915.73 6.223 460.29 3824.3 0.4562 1.40110 +FS_19 Byp_Nozz.Fl_O 465.27 7.179 479.51 114.57 0.0000 915.73 4.364 415.80 2706.4 0.8739 1.40110 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1194.53 1.201 0.8892 2557.734 1.0605 0.8921 -4857.4 57.78 23.54 +LPC 115.90 1.675 0.8333 2483.737 1.1907 0.8450 -1835.7 24.78 10.32 +HPC 75.70 4.472 0.8629 6134.214 1.6113 0.8878 -7091.3 37.71 38.23 +HPT 27.34 2.786 0.9163 162.155 1.2713 0.9051 7091.4 +LPT 73.36 3.474 0.9103 68.921 1.3532 0.8949 6693.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2290.35 1.140 0.9186 0.649 2.2519 0.5215 1.4369 0.9679 3943.9586 +LPC 124.31 1.207 0.8680 0.678 1.5377 0.9323 3.2631 0.9600 3662.6571 +HPC 179.97 17.051 0.8513 0.965 2.2397 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.203 0.9347 105.906 5.2030 1.4085 0.4249 0.9803 1.5311 +LPT 152.44 4.452 0.9091 84.971 4.4518 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3789.43 11354.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 694.07 166.13 18.185 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 694.07 166.13 18.185 +Duct1 0.0025 0.2842 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 694.07 166.13 18.185 +Duct2 0.0025 0.3788 365.99 +Duct3 0.0050 0.2994 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2622 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.0714 919.97 221.18 53.907 +Duct5 0.0075 0.4562 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.2550 919.97 221.18 53.907 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 479.51 114.57 7.234 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8616 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6435.9 5787.0 7091.4 +LP_Shaft 2388.1 14720.0 6693.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1575.28 0.9940 0.0550 0.51672 0.00959 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.645 0.9975 1.0000 0.9975 2706.36 0.874 871.7 12605.9 +Core_Nozz 1.188 0.9999 1.0000 0.9999 862.88 0.505 715.4 1327.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 287 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 11/ 21/ 1/ 9 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 30000.0 0.00 454.41 644.8 1.4420 929.73 9.6247 696.56 5.791 1278.8 1253.1 967.3 + core size:22.39 Q: 215.73 Maximum Thrust: 12895.0 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 454.41 6.055 452.17 108.02 0.0000 1029.82 4.364 411.69 3283.4 0.7000 1.40131 +FS_2 Inlet.Fl_O 454.41 6.024 452.17 108.02 0.0000 1035.01 5.633 443.56 5943.4 0.3109 1.40131 +FS_21 Fan.Fl_O 454.41 6.530 465.52 111.22 0.0000 968.91 5.857 451.24 4515.2 0.3971 1.40124 +FS_13 Splitter.Fl_O2 411.64 6.530 465.52 111.22 0.0000 877.72 5.729 448.41 3795.6 0.4360 1.40124 +FS_22 Splitter.Fl_O1 42.77 6.530 465.52 111.22 0.0000 91.19 6.313 461.05 719.5 0.2199 1.40124 +FS_23 Duct1.Fl_O 42.77 6.513 465.52 111.22 0.0000 91.42 6.297 461.05 721.3 0.2199 1.40124 +FS_24 LPC.Fl_O 42.77 9.097 522.43 124.85 0.0000 69.35 8.387 510.43 366.0 0.3425 1.40045 +FS_25 Duct2.Fl_O 42.77 9.074 522.43 124.85 0.0000 69.52 8.366 510.43 366.9 0.3425 1.40045 +FS_3 HPC.Fl_O 42.77 35.061 809.07 194.02 0.0000 22.39 32.410 791.36 119.9 0.3379 1.39151 +FS_36 Bld3.Fl_O 38.92 35.061 809.07 194.02 0.0000 20.38 32.410 791.36 109.1 0.3379 1.39151 +FS_4 Burner.Fl_O 39.18 33.132 1278.80 313.34 0.0066 27.29 32.920 1276.63 483.4 0.0972 1.35850 +FS_45 HPT.Fl_O 43.03 11.766 967.31 233.91 0.0060 73.39 11.067 951.15 439.1 0.2993 1.37864 +FS_48 Duct3.Fl_O 43.03 11.708 967.31 233.91 0.0060 73.76 11.012 951.15 441.4 0.2993 1.37864 +FS_5 LPT.Fl_O 43.03 4.781 775.70 186.60 0.0060 161.76 4.663 770.32 1477.4 0.1893 1.38936 +FS_7 Duct4.Fl_O 43.03 4.733 775.70 186.60 0.0060 163.39 4.670 772.81 2018.9 0.1386 1.38936 +FS_9 Core_Nozz.Fl_O 43.03 4.733 775.70 186.60 0.0060 163.39 4.364 758.25 862.8 0.3436 1.38936 +FS_15 BypBld.Fl_O 411.64 6.530 465.52 111.22 0.0000 877.72 5.729 448.41 3795.6 0.4360 1.40124 +FS_17 Duct5.Fl_O 411.64 6.481 465.52 111.22 0.0000 884.35 5.686 448.41 3824.3 0.4360 1.40124 +FS_19 Byp_Nozz.Fl_O 411.64 6.481 465.52 111.22 0.0000 884.35 4.364 415.67 2706.4 0.7730 1.40124 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1035.01 1.084 0.7899 1986.923 1.0295 0.7923 -2055.4 83.22 24.30 +LPC 91.42 1.397 0.8206 1958.215 1.1222 0.8289 -824.9 30.92 8.60 +HPC 69.52 3.864 0.8540 6020.961 1.5487 0.8785 -4185.8 49.53 50.52 +HPT 27.29 2.816 0.9179 168.979 1.2871 0.9065 4185.7 +LPT 73.76 2.449 0.8999 59.649 1.2470 0.8879 2880.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1984.48 1.058 0.8160 0.504 2.6187 0.5215 1.4369 0.9679 3943.9586 +LPC 98.06 1.122 0.8547 0.535 1.6002 0.9323 3.2631 0.9600 3662.6571 +HPC 165.27 14.239 0.8424 0.947 2.3792 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.274 0.9363 110.363 5.2737 1.4085 0.4249 0.9803 1.5311 +LPT 153.26 3.021 0.8987 73.539 3.0213 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3283.37 9838.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 623.25 149.06 12.881 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 623.25 149.06 12.881 +Duct1 0.0025 0.2199 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 623.25 149.06 12.881 +Duct2 0.0025 0.3425 365.99 +Duct3 0.0050 0.2993 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1893 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.4969 809.07 194.02 35.061 +Duct5 0.0075 0.4360 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.3523 809.07 194.02 35.061 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 465.52 111.22 6.530 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.6247 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6042.7 3638.1 4185.7 +LP_Shaft 1855.2 8154.3 2880.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1278.80 0.9940 0.0550 0.25826 0.00664 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.485 0.9975 1.0000 0.9975 2706.36 0.773 771.0 9864.6 +Core_Nozz 1.085 0.9999 1.0000 0.9999 862.88 0.344 462.2 618.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 288 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 30000.0 0.00 764.98 13170.1 0.6045 7961.54 5.0411 746.32 22.715 2423.0 2361.3 1892.2 + core size:19.94 Q: 247.65 Maximum Thrust: 13170.1 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 764.98 6.339 458.16 109.46 0.0000 1666.72 4.364 411.69 5158.9 0.7500 1.40129 +FS_2 Inlet.Fl_O 764.98 6.308 458.16 109.46 0.0000 1675.11 5.035 429.53 5943.4 0.5763 1.40129 +FS_21 Fan.Fl_O 764.98 10.373 538.94 128.81 0.0000 1104.74 8.918 516.15 4515.2 0.4696 1.40013 +FS_13 Splitter.Fl_O2 638.35 10.373 538.94 128.81 0.0000 921.87 8.944 516.58 3795.6 0.4650 1.40013 +FS_22 Splitter.Fl_O1 126.63 10.373 538.94 128.81 0.0000 182.87 8.775 513.78 719.5 0.4946 1.40013 +FS_23 Duct1.Fl_O 126.63 10.347 538.94 128.81 0.0000 183.33 8.753 513.78 721.3 0.4946 1.40013 +FS_24 LPC.Fl_O 126.63 25.753 723.03 173.14 0.0000 85.32 22.534 696.17 366.0 0.4415 1.39525 +FS_25 Duct2.Fl_O 126.63 25.689 723.03 173.14 0.0000 85.53 22.478 696.17 366.9 0.4415 1.39525 +FS_3 HPC.Fl_O 126.63 143.999 1234.22 300.05 0.0000 19.94 135.524 1214.30 119.9 0.2991 1.36599 +FS_36 Bld3.Fl_O 115.23 143.999 1234.22 300.05 0.0000 18.14 135.524 1214.30 109.1 0.2991 1.36599 +FS_4 Burner.Fl_O 117.44 136.079 2422.96 638.91 0.0192 27.41 135.201 2419.32 483.4 0.0997 1.30241 +FS_45 HPT.Fl_O 128.84 50.995 1892.15 484.19 0.0175 70.92 48.170 1866.16 439.1 0.2948 1.31987 +FS_48 Duct3.Fl_O 128.84 50.740 1892.15 484.19 0.0175 71.27 47.929 1866.16 441.4 0.2948 1.31987 +FS_5 LPT.Fl_O 128.84 10.401 1314.31 325.71 0.0175 289.80 9.521 1284.56 1477.4 0.3637 1.34898 +FS_7 Duct4.Fl_O 128.84 10.297 1314.31 325.71 0.0175 292.73 9.843 1299.08 2018.9 0.2590 1.34898 +FS_9 Core_Nozz.Fl_O 128.84 10.297 1314.31 325.71 0.0175 292.73 5.502 1115.26 862.9 1.0000 1.34898 +FS_15 BypBld.Fl_O 638.35 10.373 538.94 128.81 0.0000 921.87 8.944 516.58 3795.6 0.4650 1.40013 +FS_17 Duct5.Fl_O 638.35 10.295 538.94 128.81 0.0000 928.83 8.877 516.58 3824.3 0.4650 1.40013 +FS_19 Byp_Nozz.Fl_O 638.35 10.295 538.94 128.81 0.0000 928.83 5.436 448.93 2706.3 1.0000 1.40013 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.645 0.8675 3944.235 1.1763 0.8766 -20949.8 24.71 17.45 +LPC 183.33 2.489 0.8683 3636.613 1.3416 0.8839 -7940.8 28.35 23.26 +HPC 85.53 5.606 0.8652 6325.036 1.7070 0.8922 -22738.3 20.12 20.18 +HPT 27.41 2.668 0.9134 151.713 1.2326 0.9036 22738.6 +LPT 71.27 4.879 0.9324 85.221 1.4397 0.9182 28890.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8963 1.000 2.3707 0.5215 1.4369 0.9679 3943.9586 +LPC 196.64 1.456 0.9045 0.993 1.7656 0.9323 3.2631 0.9600 3662.6571 +HPC 203.33 22.290 0.8535 0.995 2.0421 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.927 0.9317 99.086 4.9269 1.4085 0.4249 0.9803 1.5311 +LPT 148.10 6.411 0.9312 105.067 6.4105 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5158.89 17744.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 905.22 217.56 43.021 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 905.22 217.56 43.021 +Duct1 0.0025 0.4946 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 905.22 217.56 43.021 +Duct2 0.0025 0.4415 365.99 +Duct3 0.0050 0.2948 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3637 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.4320 1234.22 300.05 143.999 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.9646 1234.22 300.05 143.999 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 538.94 128.81 10.373 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0411 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7467.8 15992.0 22738.6 +LP_Shaft 3707.0 40932.5 28890.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2422.96 0.9940 0.0550 2.21154 0.01919 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.359 0.9968 1.0000 0.9975 2706.36 1.000 1036.6 23468.4 +Core_Nozz 2.359 0.9986 1.0000 0.9999 862.88 1.000 1614.2 7446.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 289 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 30000.0 0.00 745.68 11852.7 0.5939 7039.59 5.3053 746.32 20.810 2335.2 2276.1 1817.0 + core size:20.03 Q: 247.65 Maximum Thrust: 13170.1 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 745.68 6.339 458.16 109.46 0.0000 1624.67 4.364 411.69 5028.8 0.7500 1.40129 +FS_2 Inlet.Fl_O 745.68 6.308 458.16 109.46 0.0000 1632.85 5.120 431.60 5943.4 0.5537 1.40129 +FS_21 Fan.Fl_O 745.68 10.137 532.80 127.34 0.0000 1095.64 8.743 510.73 4515.2 0.4645 1.40025 +FS_13 Splitter.Fl_O2 627.42 10.137 532.80 127.34 0.0000 921.88 8.740 510.68 3795.6 0.4650 1.40025 +FS_22 Splitter.Fl_O1 118.26 10.137 532.80 127.34 0.0000 173.77 8.759 511.00 719.5 0.4615 1.40025 +FS_23 Duct1.Fl_O 118.26 10.112 532.80 127.34 0.0000 174.20 8.737 511.00 721.3 0.4615 1.40025 +FS_24 LPC.Fl_O 118.26 23.563 700.56 167.70 0.0000 85.72 20.584 674.19 366.0 0.4441 1.39599 +FS_25 Duct2.Fl_O 118.26 23.504 700.56 167.70 0.0000 85.94 20.533 674.19 366.9 0.4441 1.39599 +FS_3 HPC.Fl_O 118.26 131.922 1198.89 291.03 0.0000 20.03 124.080 1179.26 119.9 0.3004 1.36821 +FS_36 Bld3.Fl_O 107.62 131.922 1198.89 291.03 0.0000 18.23 124.080 1179.26 109.1 0.3004 1.36821 +FS_4 Burner.Fl_O 109.58 124.666 2335.20 612.33 0.0182 27.41 123.862 2331.67 483.4 0.0996 1.30534 +FS_45 HPT.Fl_O 120.22 46.255 1816.97 462.56 0.0165 71.49 43.648 1791.36 439.1 0.2970 1.32360 +FS_48 Duct3.Fl_O 120.22 46.024 1816.97 462.56 0.0165 71.85 43.430 1791.36 441.4 0.2970 1.32360 +FS_5 LPT.Fl_O 120.22 9.503 1263.09 311.94 0.0165 290.11 8.698 1234.21 1477.4 0.3636 1.35279 +FS_7 Duct4.Fl_O 120.22 9.408 1263.09 311.94 0.0165 293.04 8.993 1248.30 2018.9 0.2589 1.35279 +FS_9 Core_Nozz.Fl_O 120.22 9.408 1263.09 311.94 0.0165 293.04 5.023 1070.13 862.9 1.0000 1.35279 +FS_15 BypBld.Fl_O 627.42 10.137 532.80 127.34 0.0000 921.88 8.740 510.68 3795.6 0.4650 1.40025 +FS_17 Duct5.Fl_O 627.42 10.061 532.80 127.34 0.0000 928.84 8.675 510.68 3824.3 0.4650 1.40025 +FS_19 Byp_Nozz.Fl_O 627.42 10.061 532.80 127.34 0.0000 928.84 5.313 443.80 2706.4 1.0000 1.40025 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1632.85 1.607 0.8926 3741.849 1.1629 0.8996 -18866.5 28.22 17.74 +LPC 174.20 2.330 0.8660 3469.848 1.3149 0.8809 -6753.6 28.86 22.15 +HPC 85.94 5.613 0.8641 6335.229 1.7113 0.8915 -20636.3 20.53 20.56 +HPT 27.41 2.695 0.9139 152.362 1.2375 0.9040 20636.3 +LPT 71.85 4.843 0.9279 82.504 1.4385 0.9126 25619.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3130.58 1.423 0.9221 0.949 2.1747 0.5215 1.4369 0.9679 3943.9586 +LPC 186.85 1.408 0.9021 0.947 1.7514 0.9323 3.2631 0.9600 3662.6571 +HPC 204.30 22.324 0.8524 0.997 2.0713 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.990 0.9322 99.510 4.9898 1.4085 0.4249 0.9803 1.5311 +LPT 149.29 6.361 0.9267 101.717 6.3608 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5028.75 17297.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 877.98 210.87 39.387 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 877.98 210.87 39.387 +Duct1 0.0025 0.4615 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 877.98 210.87 39.387 +Duct2 0.0025 0.4441 365.99 +Duct3 0.0050 0.2970 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.1392 1198.89 291.03 131.922 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.5045 1198.89 291.03 131.922 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 532.80 127.34 10.137 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3053 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7362.7 14720.7 20636.3 +LP_Shaft 3516.8 38260.8 25619.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2335.20 0.9940 0.0550 1.95544 0.01817 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.306 0.9971 1.0000 0.9975 2706.36 1.000 1030.6 22665.5 +Core_Nozz 2.156 0.9995 1.0000 0.9999 862.88 1.000 1583.3 6484.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 290 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 30000.0 0.00 723.94 10536.1 0.5893 6209.00 5.5101 746.32 19.172 2245.0 2188.9 1742.4 + core size:20.18 Q: 247.65 Maximum Thrust: 13170.1 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 723.94 6.339 458.16 109.46 0.0000 1577.30 4.364 411.69 4882.1 0.7500 1.40129 +FS_2 Inlet.Fl_O 723.94 6.308 458.16 109.46 0.0000 1585.24 5.209 433.73 5943.4 0.5297 1.40129 +FS_21 Fan.Fl_O 723.94 9.848 527.20 126.00 0.0000 1089.16 8.513 505.68 4515.2 0.4608 1.40036 +FS_13 Splitter.Fl_O2 612.74 9.848 527.20 126.00 0.0000 921.85 8.491 505.31 3795.6 0.4650 1.40036 +FS_22 Splitter.Fl_O1 111.20 9.848 527.20 126.00 0.0000 167.30 8.625 507.58 719.5 0.4392 1.40036 +FS_23 Duct1.Fl_O 111.20 9.823 527.20 126.00 0.0000 167.72 8.604 507.58 721.3 0.4392 1.40036 +FS_24 LPC.Fl_O 111.20 22.162 686.69 164.35 0.0000 84.85 19.428 661.48 366.0 0.4382 1.39647 +FS_25 Duct2.Fl_O 111.20 22.107 686.69 164.35 0.0000 85.06 19.379 661.48 366.9 0.4382 1.39647 +FS_3 HPC.Fl_O 111.20 121.539 1168.74 283.37 0.0000 20.18 114.195 1149.20 119.9 0.3028 1.37011 +FS_36 Bld3.Fl_O 101.19 121.539 1168.74 283.37 0.0000 18.37 114.195 1149.20 109.1 0.3028 1.37011 +FS_4 Burner.Fl_O 102.92 114.855 2245.01 585.21 0.0170 27.40 114.114 2241.59 483.4 0.0994 1.30854 +FS_45 HPT.Fl_O 112.93 42.407 1742.40 441.26 0.0155 71.73 40.001 1717.43 439.1 0.2976 1.32757 +FS_48 Duct3.Fl_O 112.93 42.195 1742.40 441.26 0.0155 72.09 39.801 1717.43 441.4 0.2976 1.32757 +FS_5 LPT.Fl_O 112.93 8.721 1208.80 297.47 0.0155 290.52 7.980 1180.85 1477.4 0.3636 1.35691 +FS_7 Duct4.Fl_O 112.93 8.633 1208.80 297.47 0.0155 293.46 8.252 1194.49 2018.9 0.2589 1.35691 +FS_9 Core_Nozz.Fl_O 112.93 8.633 1208.80 297.47 0.0155 293.46 4.605 1022.45 862.9 1.0000 1.35691 +FS_15 BypBld.Fl_O 612.74 9.848 527.20 126.00 0.0000 921.85 8.491 505.31 3795.6 0.4650 1.40036 +FS_17 Duct5.Fl_O 612.74 9.774 527.20 126.00 0.0000 928.82 8.427 505.31 3824.3 0.4650 1.40036 +FS_19 Byp_Nozz.Fl_O 612.74 9.774 527.20 126.00 0.0000 928.82 5.161 439.12 2706.4 1.0000 1.40036 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1585.24 1.561 0.9024 3613.100 1.1507 0.9084 -16939.8 31.70 18.33 +LPC 167.72 2.256 0.8631 3368.219 1.3025 0.8778 -6034.9 28.04 20.47 +HPC 85.06 5.498 0.8648 6312.538 1.7020 0.8920 -18725.1 22.16 22.24 +HPT 27.40 2.708 0.9145 153.296 1.2414 0.9045 18724.9 +LPT 72.09 4.839 0.9259 81.352 1.4414 0.9101 22974.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3039.50 1.391 0.9323 0.916 2.0963 0.5215 1.4369 0.9679 3943.9586 +LPC 179.91 1.385 0.8990 0.920 1.7157 0.9323 3.2631 0.9600 3662.6571 +HPC 202.22 21.793 0.8532 0.993 2.0974 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.021 0.9328 100.120 5.0208 1.4085 0.4249 0.9803 1.5311 +LPT 149.79 6.355 0.9247 100.296 6.3546 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4882.12 16792.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 858.14 206.01 36.673 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 858.14 206.01 36.673 +Duct1 0.0025 0.4392 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 858.14 206.01 36.673 +Duct2 0.0025 0.4382 365.99 +Duct3 0.0050 0.2976 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.8921 1168.74 283.37 121.539 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.1162 1168.74 283.37 121.539 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 527.20 126.00 9.848 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5101 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7263.4 13539.9 18724.9 +LP_Shaft 3395.8 35534.3 22974.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2245.01 0.9940 0.0550 1.72472 0.01704 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.240 0.9973 1.0000 0.9975 2706.36 1.000 1025.2 21680.9 +Core_Nozz 1.978 0.9998 1.0000 0.9999 862.88 1.000 1549.7 5647.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 291 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 30000.0 0.00 676.07 7902.0 0.5941 4694.66 5.9896 746.32 15.954 2061.7 2011.5 1593.7 + core size:20.53 Q: 247.65 Maximum Thrust: 13170.1 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 676.07 6.339 458.16 109.46 0.0000 1473.01 4.364 411.69 4559.3 0.7500 1.40129 +FS_2 Inlet.Fl_O 676.07 6.308 458.16 109.46 0.0000 1480.42 5.383 437.83 5943.4 0.4810 1.40129 +FS_21 Fan.Fl_O 676.07 9.210 515.73 123.25 0.0000 1075.75 7.998 495.33 4515.2 0.4533 1.40057 +FS_13 Splitter.Fl_O2 579.35 9.210 515.73 123.25 0.0000 921.85 7.941 494.31 3795.6 0.4650 1.40057 +FS_22 Splitter.Fl_O1 96.73 9.210 515.73 123.25 0.0000 153.91 8.267 500.05 719.5 0.3956 1.40057 +FS_23 Duct1.Fl_O 96.73 9.187 515.73 123.25 0.0000 154.29 8.247 500.05 721.3 0.3956 1.40057 +FS_24 LPC.Fl_O 96.73 19.577 661.23 158.21 0.0000 81.98 17.349 638.88 366.0 0.4193 1.39741 +FS_25 Duct2.Fl_O 96.73 19.528 661.23 158.21 0.0000 82.19 17.306 638.88 366.9 0.4193 1.39741 +FS_3 HPC.Fl_O 96.73 101.139 1106.88 267.73 0.0000 20.53 94.799 1087.52 119.9 0.3082 1.37401 +FS_36 Bld3.Fl_O 88.02 101.139 1106.88 267.73 0.0000 18.68 94.799 1087.52 109.1 0.3082 1.37401 +FS_4 Burner.Fl_O 89.32 95.576 2061.67 530.91 0.0148 27.38 94.961 2058.48 483.4 0.0991 1.31550 +FS_45 HPT.Fl_O 98.03 35.076 1593.71 399.48 0.0135 71.99 33.071 1570.25 439.1 0.2978 1.33601 +FS_48 Duct3.Fl_O 98.03 34.901 1593.71 399.48 0.0135 72.36 32.905 1570.25 441.4 0.2978 1.33601 +FS_5 LPT.Fl_O 98.03 7.300 1103.89 269.89 0.0135 287.90 6.693 1078.50 1477.4 0.3586 1.36498 +FS_7 Duct4.Fl_O 98.03 7.227 1103.89 269.89 0.0135 290.80 6.914 1090.87 2018.9 0.2556 1.36498 +FS_9 Core_Nozz.Fl_O 98.03 7.227 1103.89 269.89 0.0135 290.80 4.364 963.24 862.9 0.8875 1.36498 +FS_15 BypBld.Fl_O 579.35 9.210 515.73 123.25 0.0000 921.85 7.941 494.31 3795.6 0.4650 1.40057 +FS_17 Duct5.Fl_O 579.35 9.141 515.73 123.25 0.0000 928.81 7.881 494.31 3824.3 0.4650 1.40057 +FS_19 Byp_Nozz.Fl_O 579.35 9.141 515.73 123.25 0.0000 928.81 4.826 429.56 2706.4 1.0000 1.40057 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1480.42 1.460 0.9105 3366.539 1.1257 0.9152 -13190.1 39.48 19.72 +LPC 154.29 2.131 0.8543 3173.070 1.2821 0.8688 -4784.6 25.15 16.56 +HPC 82.19 5.179 0.8659 6251.837 1.6740 0.8923 -14987.9 26.36 26.51 +HPT 27.38 2.725 0.9149 155.463 1.2481 0.9046 14988.0 +LPT 72.36 4.781 0.9210 79.257 1.4437 0.9044 17974.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2838.44 1.320 0.9406 0.854 2.0402 0.5215 1.4369 0.9679 3943.9586 +LPC 165.50 1.347 0.8898 0.866 1.6211 0.9323 3.2631 0.9600 3662.6571 +HPC 195.38 20.319 0.8542 0.983 2.1329 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.060 0.9332 101.536 5.0595 1.4085 0.4249 0.9803 1.5311 +LPT 150.35 6.274 0.9198 97.714 6.2741 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4559.32 15682.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 819.39 196.54 31.484 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 819.39 196.54 31.484 +Duct1 0.0025 0.3956 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 819.39 196.54 31.484 +Duct2 0.0025 0.4193 365.99 +Duct3 0.0050 0.2978 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3586 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.3854 1106.88 267.73 101.139 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.3199 1106.88 267.73 101.139 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 515.73 123.25 9.210 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9896 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7058.9 11151.7 14988.0 +LP_Shaft 3164.1 29836.3 17974.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2061.67 0.9940 0.0550 1.30407 0.01482 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.095 0.9975 1.0000 0.9975 2706.36 1.000 1013.9 19509.2 +Core_Nozz 1.656 0.9999 1.0000 0.9999 862.88 0.888 1337.5 4075.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 292 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 30000.0 0.00 620.19 5268.1 0.6260 3297.60 6.6992 746.32 12.592 1857.7 1814.0 1427.9 + core size:20.93 Q: 247.65 Maximum Thrust: 13170.1 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 620.19 6.339 458.16 109.46 0.0000 1351.24 4.364 411.69 4182.4 0.7500 1.40129 +FS_2 Inlet.Fl_O 620.19 6.308 458.16 109.46 0.0000 1358.04 5.556 441.80 5943.4 0.4294 1.40129 +FS_21 Fan.Fl_O 620.19 8.467 502.43 120.06 0.0000 1059.48 7.393 483.29 4515.2 0.4444 1.40078 +FS_13 Splitter.Fl_O2 539.63 8.467 502.43 120.06 0.0000 921.87 7.300 481.56 3795.6 0.4649 1.40078 +FS_22 Splitter.Fl_O1 80.55 8.467 502.43 120.06 0.0000 137.61 7.793 490.64 719.5 0.3462 1.40078 +FS_23 Duct1.Fl_O 80.55 8.446 502.43 120.06 0.0000 137.95 7.773 490.64 721.3 0.3462 1.40078 +FS_24 LPC.Fl_O 80.55 16.444 627.19 150.01 0.0000 79.16 14.718 607.67 366.0 0.4014 1.39850 +FS_25 Duct2.Fl_O 80.55 16.403 627.19 150.01 0.0000 79.36 14.681 607.67 366.9 0.4014 1.39850 +FS_3 HPC.Fl_O 80.55 79.828 1033.06 249.22 0.0000 20.93 74.615 1014.05 119.9 0.3143 1.37865 +FS_36 Bld3.Fl_O 73.30 79.828 1033.06 249.22 0.0000 19.04 74.615 1014.05 109.1 0.3143 1.37865 +FS_4 Burner.Fl_O 74.22 75.438 1857.69 471.94 0.0125 27.36 74.953 1854.76 483.4 0.0987 1.32465 +FS_45 HPT.Fl_O 81.47 27.434 1427.94 354.03 0.0114 72.41 25.846 1406.18 439.1 0.2986 1.34626 +FS_48 Duct3.Fl_O 81.47 27.297 1427.94 354.03 0.0114 72.78 25.717 1406.18 441.4 0.2986 1.34626 +FS_5 LPT.Fl_O 81.47 6.184 1002.57 243.70 0.0114 269.18 5.740 982.48 1477.4 0.3308 1.37288 +FS_7 Duct4.Fl_O 81.47 6.122 1002.57 243.70 0.0114 271.90 5.891 992.16 2018.9 0.2370 1.37288 +FS_9 Core_Nozz.Fl_O 81.47 6.122 1002.57 243.70 0.0114 271.90 4.364 914.02 862.9 0.7174 1.37288 +FS_15 BypBld.Fl_O 539.63 8.467 502.43 120.06 0.0000 921.87 7.300 481.56 3795.6 0.4649 1.40078 +FS_17 Duct5.Fl_O 539.63 8.403 502.43 120.06 0.0000 928.83 7.245 481.56 3824.3 0.4649 1.40078 +FS_19 Byp_Nozz.Fl_O 539.63 8.403 502.43 120.06 0.0000 928.83 4.437 418.47 2706.3 1.0000 1.40078 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1358.04 1.342 0.9098 3040.817 1.0966 0.9135 -9303.4 47.34 21.51 +LPC 137.95 1.947 0.8443 2903.748 1.2483 0.8581 -3413.7 23.14 13.23 +HPC 79.36 4.867 0.8647 6203.533 1.6471 0.8906 -11306.7 31.06 31.29 +HPT 27.36 2.750 0.9154 158.273 1.2573 0.9047 11306.7 +LPT 72.78 4.414 0.9167 75.630 1.4243 0.8998 12717.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2603.86 1.238 0.9399 0.771 2.0797 0.5215 1.4369 0.9679 3943.9586 +LPC 147.97 1.290 0.8794 0.793 1.5503 0.9323 3.2631 0.9600 3662.6571 +HPC 188.67 18.875 0.8531 0.976 2.1675 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.118 0.9338 103.371 5.1184 1.4085 0.4249 0.9803 1.5311 +LPT 151.22 5.763 0.9155 93.243 5.7627 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4182.42 14386.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 770.88 184.74 25.695 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 770.88 184.74 25.695 +Duct1 0.0025 0.3462 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 770.88 184.74 25.695 +Duct2 0.0025 0.4014 365.99 +Duct3 0.0050 0.2986 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3308 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.8193 1033.06 249.22 79.828 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.4304 1033.06 249.22 79.828 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 502.43 120.06 8.467 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6992 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6821.7 8705.2 11306.7 +LP_Shaft 2857.9 23371.1 12717.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1857.69 0.9940 0.0550 0.91600 0.01250 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.926 0.9975 1.0000 0.9975 2706.36 1.000 1000.8 16983.3 +Core_Nozz 1.403 0.9999 1.0000 0.9999 862.88 0.717 1054.8 2670.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 293 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 30000.0 0.00 551.95 2634.2 0.7492 1973.51 7.8824 746.32 8.987 1595.3 1559.9 1217.1 + core size:21.52 Q: 247.65 Maximum Thrust: 13170.1 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 551.95 6.339 458.16 109.46 0.0000 1202.57 4.364 411.69 3722.3 0.7500 1.40129 +FS_2 Inlet.Fl_O 551.95 6.308 458.16 109.46 0.0000 1208.63 5.732 445.77 5943.4 0.3721 1.40129 +FS_21 Fan.Fl_O 551.95 7.605 486.53 116.25 0.0000 1033.08 6.695 469.12 4515.2 0.4302 1.40101 +FS_13 Splitter.Fl_O2 489.81 7.605 486.53 116.25 0.0000 916.77 6.571 466.59 3795.6 0.4615 1.40101 +FS_22 Splitter.Fl_O1 62.14 7.605 486.53 116.25 0.0000 116.31 7.184 478.67 719.5 0.2861 1.40101 +FS_23 Duct1.Fl_O 62.14 7.586 486.53 116.25 0.0000 116.60 7.166 478.67 721.3 0.2861 1.40101 +FS_24 LPC.Fl_O 62.14 12.879 582.10 139.17 0.0000 75.11 11.679 566.07 366.0 0.3765 1.39932 +FS_25 Duct2.Fl_O 62.14 12.847 582.10 139.17 0.0000 75.30 11.650 566.07 366.9 0.3765 1.39932 +FS_3 HPC.Fl_O 62.14 56.971 935.09 224.91 0.0000 21.52 53.018 916.58 119.9 0.3237 1.38471 +FS_36 Bld3.Fl_O 56.55 56.971 935.09 224.91 0.0000 19.59 53.018 916.58 109.1 0.3237 1.38471 +FS_4 Burner.Fl_O 57.10 53.837 1595.32 398.41 0.0097 27.33 53.492 1592.73 483.4 0.0981 1.33853 +FS_45 HPT.Fl_O 62.69 19.349 1217.11 297.94 0.0088 72.94 18.213 1197.71 439.1 0.2993 1.36087 +FS_48 Duct3.Fl_O 62.69 19.252 1217.11 297.94 0.0088 73.30 18.122 1197.71 441.4 0.2993 1.36087 +FS_5 LPT.Fl_O 62.69 5.328 891.17 215.41 0.0088 226.65 5.064 878.75 1477.4 0.2720 1.38157 +FS_7 Duct4.Fl_O 62.69 5.275 891.17 215.41 0.0088 228.94 5.136 884.62 2018.9 0.1970 1.38157 +FS_9 Core_Nozz.Fl_O 62.69 5.275 891.17 215.41 0.0088 228.94 4.364 845.67 862.8 0.5299 1.38157 +FS_15 BypBld.Fl_O 489.81 7.605 486.53 116.25 0.0000 916.77 6.571 466.59 3795.6 0.4615 1.40101 +FS_17 Duct5.Fl_O 489.81 7.548 486.53 116.25 0.0000 923.70 6.521 466.59 3824.3 0.4615 1.40101 +FS_19 Byp_Nozz.Fl_O 489.81 7.548 486.53 116.25 0.0000 923.70 4.364 415.89 2706.3 0.9201 1.40101 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1208.63 1.206 0.8879 2590.298 1.0619 0.8909 -5305.4 57.72 23.90 +LPC 116.60 1.698 0.8319 2513.631 1.1964 0.8440 -2015.2 23.57 9.98 +HPC 75.30 4.434 0.8628 6126.682 1.6064 0.8876 -7537.9 38.30 38.85 +HPT 27.33 2.782 0.9163 162.500 1.2703 0.9052 7538.1 +LPT 73.30 3.613 0.9110 69.782 1.3657 0.8952 7320.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2317.38 1.143 0.9173 0.657 2.2579 0.5215 1.4369 0.9679 3943.9586 +LPC 125.06 1.214 0.8666 0.686 1.5148 0.9323 3.2631 0.9600 3662.6571 +HPC 179.02 16.877 0.8511 0.964 2.2458 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.195 0.9347 106.131 5.1952 1.4085 0.4249 0.9803 1.5311 +LPT 152.32 4.646 0.9099 86.033 4.6457 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3722.26 12803.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 706.68 169.18 19.311 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 706.68 169.18 19.311 +Duct1 0.0025 0.2861 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 706.68 169.18 19.311 +Duct2 0.0025 0.3765 365.99 +Duct3 0.0050 0.2993 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2720 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.1749 935.09 224.91 56.971 +Duct5 0.0075 0.4615 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.4177 935.09 224.91 56.971 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 486.53 116.25 7.605 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8824 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6490.5 6099.8 7538.1 +LP_Shaft 2434.5 15792.9 7320.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1595.32 0.9940 0.0550 0.54820 0.00969 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.730 0.9975 1.0000 0.9975 2706.36 0.920 917.9 13974.1 +Core_Nozz 1.209 0.9999 1.0000 0.9999 862.88 0.530 751.0 1463.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 294 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 12/ 32/ 2/ 9 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 30000.0 0.00 483.25 658.5 1.5125 995.97 9.7015 746.32 5.889 1300.1 1274.1 984.4 + core size:22.42 Q: 247.65 Maximum Thrust: 13170.1 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 483.25 6.339 458.16 109.46 0.0000 1052.90 4.364 411.69 3259.0 0.7500 1.40129 +FS_2 Inlet.Fl_O 483.25 6.308 458.16 109.46 0.0000 1058.20 5.878 449.00 5943.4 0.3188 1.40129 +FS_21 Fan.Fl_O 483.25 6.860 472.35 112.86 0.0000 987.88 6.121 457.18 4515.2 0.4067 1.40118 +FS_13 Splitter.Fl_O2 438.10 6.860 472.35 112.86 0.0000 895.57 5.979 454.11 3795.6 0.4475 1.40118 +FS_22 Splitter.Fl_O1 45.16 6.860 472.35 112.86 0.0000 92.31 6.627 467.70 719.5 0.2228 1.40118 +FS_23 Duct1.Fl_O 45.16 6.843 472.35 112.86 0.0000 92.54 6.611 467.70 721.3 0.2228 1.40118 +FS_24 LPC.Fl_O 45.16 9.745 533.72 127.56 0.0000 69.08 8.991 521.57 366.0 0.3410 1.40023 +FS_25 Duct2.Fl_O 45.16 9.720 533.72 127.56 0.0000 69.26 8.968 521.57 366.9 0.3410 1.40023 +FS_3 HPC.Fl_O 45.16 37.331 824.90 197.88 0.0000 22.42 34.501 806.81 119.9 0.3385 1.39076 +FS_36 Bld3.Fl_O 41.09 37.331 824.90 197.88 0.0000 20.40 34.501 806.81 109.1 0.3385 1.39076 +FS_4 Burner.Fl_O 41.37 35.278 1300.08 318.91 0.0067 27.28 35.053 1297.88 483.4 0.0972 1.35711 +FS_45 HPT.Fl_O 45.43 12.537 984.35 238.19 0.0061 73.37 11.792 967.95 439.1 0.2994 1.37751 +FS_48 Duct3.Fl_O 45.43 12.475 984.35 238.19 0.0061 73.74 11.733 967.95 441.4 0.2994 1.37751 +FS_5 LPT.Fl_O 45.43 4.826 778.99 187.42 0.0061 169.57 4.695 773.03 1477.4 0.1989 1.38914 +FS_7 Duct4.Fl_O 45.43 4.777 778.99 187.42 0.0061 171.29 4.708 775.80 2018.9 0.1455 1.38914 +FS_9 Core_Nozz.Fl_O 45.43 4.777 778.99 187.42 0.0061 171.29 4.364 759.48 862.9 0.3632 1.38914 +FS_15 BypBld.Fl_O 438.10 6.860 472.35 112.86 0.0000 895.57 5.979 454.11 3795.6 0.4475 1.40118 +FS_17 Duct5.Fl_O 438.10 6.809 472.35 112.86 0.0000 902.34 5.934 454.11 3824.3 0.4475 1.40118 +FS_19 Byp_Nozz.Fl_O 438.10 6.809 472.35 112.86 0.0000 902.34 4.364 415.85 2706.4 0.8229 1.40118 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1058.20 1.088 0.7855 2037.411 1.0310 0.7881 -2324.3 82.19 25.25 +LPC 92.54 1.424 0.8192 2006.553 1.1299 0.8280 -939.4 28.59 8.21 +HPC 69.26 3.841 0.8534 6016.109 1.5456 0.8779 -4493.0 50.01 51.02 +HPT 27.28 2.814 0.9179 169.255 1.2861 0.9066 4493.0 +LPT 73.74 2.585 0.9011 61.033 1.2636 0.8885 3263.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2028.95 1.061 0.8115 0.517 2.6307 0.5215 1.4369 0.9679 3943.9586 +LPC 99.27 1.130 0.8533 0.548 1.5602 0.9323 3.2631 0.9600 3662.6571 +HPC 164.65 14.131 0.8419 0.946 2.3821 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.269 0.9363 110.544 5.2691 1.4085 0.4249 0.9803 1.5311 +LPT 153.22 3.211 0.9000 75.246 3.2112 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3258.97 11209.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 636.17 152.17 13.765 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 636.17 152.17 13.765 +Duct1 0.0025 0.2228 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 636.17 152.17 13.765 +Duct2 0.0025 0.3410 365.99 +Duct3 0.0050 0.2994 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1989 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.5805 824.90 197.88 37.331 +Duct5 0.0075 0.4475 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.4837 824.90 197.88 37.331 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 472.35 112.86 6.860 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.7015 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6102.8 3866.7 4493.0 +LP_Shaft 1914.9 8951.8 3263.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1300.08 0.9940 0.0550 0.27666 0.00673 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.560 0.9975 1.0000 0.9975 2706.36 0.823 820.9 11177.9 +Core_Nozz 1.095 0.9999 1.0000 0.9999 862.88 0.363 488.8 690.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 295 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 30000.0 0.00 797.42 13503.5 0.6247 8435.45 5.0412 796.07 22.710 2454.3 2391.9 1917.8 + core size:19.93 Q: 281.77 Maximum Thrust: 13503.5 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 797.42 6.654 464.56 110.99 0.0000 1666.72 4.364 411.69 5041.5 0.8000 1.40124 +FS_2 Inlet.Fl_O 797.42 6.621 464.56 110.99 0.0000 1675.11 5.285 435.53 5943.4 0.5763 1.40124 +FS_21 Fan.Fl_O 797.42 10.888 546.46 130.62 0.0000 1104.74 9.361 523.35 4515.2 0.4697 1.39998 +FS_13 Splitter.Fl_O2 665.42 10.888 546.46 130.62 0.0000 921.87 9.388 523.79 3795.6 0.4651 1.39998 +FS_22 Splitter.Fl_O1 132.00 10.888 546.46 130.62 0.0000 182.87 9.211 520.95 719.5 0.4946 1.39998 +FS_23 Duct1.Fl_O 132.00 10.861 546.46 130.62 0.0000 183.33 9.188 520.95 721.3 0.4946 1.39998 +FS_24 LPC.Fl_O 132.00 27.033 733.04 175.56 0.0000 85.31 23.655 705.83 366.0 0.4415 1.39491 +FS_25 Duct2.Fl_O 132.00 26.966 733.04 175.56 0.0000 85.52 23.596 705.83 366.9 0.4415 1.39491 +FS_3 HPC.Fl_O 132.00 151.118 1250.27 304.16 0.0000 19.93 142.229 1230.15 119.9 0.2991 1.36499 +FS_36 Bld3.Fl_O 120.12 151.118 1250.27 304.16 0.0000 18.14 142.229 1230.15 109.1 0.2991 1.36499 +FS_4 Burner.Fl_O 122.46 142.806 2454.27 648.40 0.0195 27.41 141.885 2450.59 483.4 0.0998 1.30147 +FS_45 HPT.Fl_O 134.34 53.533 1917.77 491.60 0.0178 70.91 50.567 1891.50 439.1 0.2949 1.31867 +FS_48 Duct3.Fl_O 134.34 53.265 1917.77 491.60 0.0178 71.27 50.314 1891.50 441.4 0.2949 1.31867 +FS_5 LPT.Fl_O 134.34 10.928 1333.71 330.94 0.0178 289.71 10.004 1303.63 1477.4 0.3638 1.34760 +FS_7 Duct4.Fl_O 134.34 10.818 1333.71 330.94 0.0178 292.63 10.343 1318.31 2018.9 0.2590 1.34760 +FS_9 Core_Nozz.Fl_O 134.34 10.818 1333.71 330.94 0.0178 292.63 5.784 1132.37 862.9 1.0000 1.34760 +FS_15 BypBld.Fl_O 665.42 10.888 546.46 130.62 0.0000 921.87 9.388 523.79 3795.6 0.4651 1.39998 +FS_17 Duct5.Fl_O 665.42 10.807 546.46 130.62 0.0000 928.84 9.317 523.79 3824.3 0.4651 1.39998 +FS_19 Byp_Nozz.Fl_O 665.42 10.807 546.46 130.62 0.0000 928.84 5.706 455.20 2706.3 1.0000 1.39998 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.645 0.8675 3944.235 1.1763 0.8765 -22143.7 24.71 17.45 +LPC 183.33 2.489 0.8683 3636.658 1.3414 0.8839 -8393.3 28.34 23.26 +HPC 85.52 5.604 0.8652 6324.730 1.7056 0.8922 -24017.4 20.14 20.20 +HPT 27.41 2.668 0.9134 151.775 1.2319 0.9036 24017.8 +LPT 71.27 4.874 0.9325 85.239 1.4379 0.9184 30537.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8963 1.000 2.3708 0.5215 1.4369 0.9679 3943.9586 +LPC 196.64 1.456 0.9044 0.993 1.7655 0.9323 3.2631 0.9600 3662.6571 +HPC 203.31 22.284 0.8535 0.995 2.0424 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.925 0.9317 99.127 4.9250 1.4085 0.4249 0.9803 1.5311 +LPT 148.09 6.405 0.9313 105.089 6.4045 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5041.53 19730.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 917.49 220.57 45.154 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 917.49 220.57 45.154 +Duct1 0.0025 0.4946 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 917.49 220.57 45.154 +Duct2 0.0025 0.4415 365.99 +Duct3 0.0050 0.2949 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3638 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.6199 1250.27 304.16 151.118 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.2598 1250.27 304.16 151.118 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 546.46 130.62 10.888 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0412 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7519.0 16776.7 24017.8 +LP_Shaft 3732.8 42965.9 30537.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2454.27 0.9940 0.0550 2.34318 0.01951 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.476 0.9962 1.0000 0.9975 2706.36 1.000 1043.8 25220.4 +Core_Nozz 2.479 0.9978 1.0000 0.9999 862.88 1.000 1625.8 8013.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 296 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 30000.0 0.00 777.37 12152.8 0.6140 7462.23 5.3051 796.07 20.811 2365.9 2306.1 1842.1 + core size:20.02 Q: 281.77 Maximum Thrust: 13503.5 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 777.37 6.654 464.56 110.99 0.0000 1624.83 4.364 411.69 4914.8 0.8000 1.40124 +FS_2 Inlet.Fl_O 777.37 6.621 464.56 110.99 0.0000 1633.01 5.374 437.62 5943.4 0.5538 1.40124 +FS_21 Fan.Fl_O 777.37 10.642 540.25 129.13 0.0000 1095.66 9.178 517.88 4515.2 0.4645 1.40010 +FS_13 Splitter.Fl_O2 654.08 10.642 540.25 129.13 0.0000 921.89 9.175 517.83 3795.6 0.4651 1.40010 +FS_22 Splitter.Fl_O1 123.29 10.642 540.25 129.13 0.0000 173.77 9.195 518.15 719.5 0.4616 1.40010 +FS_23 Duct1.Fl_O 123.29 10.615 540.25 129.13 0.0000 174.21 9.172 518.15 721.3 0.4616 1.40010 +FS_24 LPC.Fl_O 123.29 24.744 710.37 170.07 0.0000 85.70 21.618 683.67 366.0 0.4440 1.39566 +FS_25 Duct2.Fl_O 123.29 24.682 710.37 170.07 0.0000 85.91 21.564 683.67 366.9 0.4440 1.39566 +FS_3 HPC.Fl_O 123.29 138.479 1214.65 295.05 0.0000 20.02 130.253 1194.81 119.9 0.3004 1.36722 +FS_36 Bld3.Fl_O 112.20 138.479 1214.65 295.05 0.0000 18.22 130.253 1194.81 109.1 0.3004 1.36722 +FS_4 Burner.Fl_O 114.27 130.862 2365.95 621.57 0.0185 27.41 130.019 2362.38 483.4 0.0996 1.30431 +FS_45 HPT.Fl_O 125.37 48.571 1842.15 469.76 0.0168 71.49 45.833 1816.25 439.1 0.2971 1.32235 +FS_48 Duct3.Fl_O 125.37 48.328 1842.15 469.76 0.0168 71.84 45.604 1816.25 441.4 0.2971 1.32235 +FS_5 LPT.Fl_O 125.37 9.989 1282.13 317.02 0.0168 289.99 9.143 1252.93 1477.4 0.3636 1.35141 +FS_7 Duct4.Fl_O 125.37 9.889 1282.13 317.02 0.0168 292.92 9.453 1267.18 2018.9 0.2589 1.35141 +FS_9 Core_Nozz.Fl_O 125.37 9.889 1282.13 317.02 0.0168 292.92 5.281 1086.88 862.9 1.0000 1.35141 +FS_15 BypBld.Fl_O 654.08 10.642 540.25 129.13 0.0000 921.89 9.175 517.83 3795.6 0.4651 1.40010 +FS_17 Duct5.Fl_O 654.08 10.562 540.25 129.13 0.0000 928.85 9.106 517.83 3824.3 0.4651 1.40010 +FS_19 Byp_Nozz.Fl_O 654.08 10.562 540.25 129.13 0.0000 928.85 5.577 450.02 2706.4 1.0000 1.40010 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1633.01 1.607 0.8925 3742.390 1.1629 0.8995 -19949.3 28.21 17.74 +LPC 174.21 2.331 0.8660 3470.318 1.3149 0.8809 -7142.6 28.84 22.13 +HPC 85.91 5.611 0.8641 6334.525 1.7099 0.8915 -21801.0 20.55 20.58 +HPT 27.41 2.694 0.9139 152.408 1.2367 0.9041 21801.0 +LPT 71.84 4.838 0.9280 82.520 1.4368 0.9128 27091.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3130.91 1.423 0.9221 0.949 2.1752 0.5215 1.4369 0.9679 3943.9586 +LPC 186.86 1.408 0.9020 0.947 1.7508 0.9323 3.2631 0.9600 3662.6571 +HPC 204.24 22.314 0.8525 0.996 2.0709 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.988 0.9322 99.540 4.9877 1.4085 0.4249 0.9803 1.5311 +LPT 149.28 6.354 0.9268 101.737 6.3542 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4914.82 19234.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 890.00 213.82 41.353 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 890.00 213.82 41.353 +Duct1 0.0025 0.4616 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 890.00 213.82 41.353 +Duct2 0.0025 0.4440 365.99 +Duct3 0.0050 0.2971 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.3152 1214.65 295.05 138.479 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.7811 1214.65 295.05 138.479 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 540.25 129.13 10.642 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3051 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7413.3 15445.4 21801.0 +LP_Shaft 3541.8 40173.7 27091.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2365.95 0.9940 0.0550 2.07284 0.01848 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.420 0.9965 1.0000 0.9975 2706.36 1.000 1037.8 24381.5 +Core_Nozz 2.266 0.9991 1.0000 0.9999 862.88 1.000 1594.9 7005.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 297 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 30000.0 0.00 754.73 10802.9 0.6094 6582.94 5.5099 796.07 19.174 2274.8 2218.0 1766.8 + core size:20.18 Q: 281.77 Maximum Thrust: 13503.5 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 754.73 6.654 464.56 110.99 0.0000 1577.50 4.364 411.69 4771.7 0.8000 1.40124 +FS_2 Inlet.Fl_O 754.73 6.621 464.56 110.99 0.0000 1585.45 5.468 439.78 5943.4 0.5298 1.40124 +FS_21 Fan.Fl_O 754.73 10.338 534.58 127.77 0.0000 1089.18 8.937 512.77 4515.2 0.4608 1.40022 +FS_13 Splitter.Fl_O2 638.80 10.338 534.58 127.77 0.0000 921.86 8.914 512.39 3795.6 0.4650 1.40022 +FS_22 Splitter.Fl_O1 115.94 10.338 534.58 127.77 0.0000 167.31 9.054 514.69 719.5 0.4393 1.40022 +FS_23 Duct1.Fl_O 115.94 10.313 534.58 127.77 0.0000 167.73 9.032 514.69 721.3 0.4393 1.40022 +FS_24 LPC.Fl_O 115.94 23.272 696.30 166.67 0.0000 84.83 20.402 670.76 366.0 0.4381 1.39614 +FS_25 Duct2.Fl_O 115.94 23.214 696.30 166.67 0.0000 85.04 20.351 670.76 366.9 0.4381 1.39614 +FS_3 HPC.Fl_O 115.94 127.590 1184.20 287.29 0.0000 20.18 119.885 1164.46 119.9 0.3028 1.36914 +FS_36 Bld3.Fl_O 105.50 127.590 1184.20 287.29 0.0000 18.36 119.885 1164.46 109.1 0.3028 1.36914 +FS_4 Burner.Fl_O 107.33 120.573 2274.85 594.09 0.0173 27.40 119.796 2271.39 483.4 0.0995 1.30754 +FS_45 HPT.Fl_O 117.77 44.533 1766.77 448.16 0.0158 71.73 42.006 1741.53 439.1 0.2977 1.32630 +FS_48 Duct3.Fl_O 117.77 44.311 1766.77 448.16 0.0158 72.09 41.796 1741.53 441.4 0.2977 1.32630 +FS_5 LPT.Fl_O 117.77 9.168 1227.24 302.34 0.0158 290.38 8.390 1198.97 1477.4 0.3636 1.35557 +FS_7 Duct4.Fl_O 117.77 9.076 1227.24 302.34 0.0158 293.31 8.675 1212.76 2018.9 0.2589 1.35557 +FS_9 Core_Nozz.Fl_O 117.77 9.076 1227.24 302.34 0.0158 293.31 4.843 1038.60 862.9 1.0000 1.35557 +FS_15 BypBld.Fl_O 638.80 10.338 534.58 127.77 0.0000 921.86 8.914 512.39 3795.6 0.4650 1.40022 +FS_17 Duct5.Fl_O 638.80 10.261 534.58 127.77 0.0000 928.83 8.847 512.39 3824.3 0.4650 1.40022 +FS_19 Byp_Nozz.Fl_O 638.80 10.261 534.58 127.77 0.0000 928.83 5.418 445.28 2706.4 1.0000 1.40022 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1585.45 1.561 0.9023 3613.587 1.1507 0.9083 -17914.1 31.68 18.33 +LPC 167.73 2.257 0.8631 3368.626 1.3025 0.8778 -6382.1 28.02 20.46 +HPC 85.04 5.496 0.8649 6312.075 1.7007 0.8919 -19785.7 22.17 22.25 +HPT 27.40 2.707 0.9145 153.338 1.2406 0.9045 19785.6 +LPT 72.09 4.833 0.9260 81.362 1.4396 0.9102 24296.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3039.90 1.391 0.9322 0.916 2.0965 0.5215 1.4369 0.9679 3943.9586 +LPC 179.91 1.385 0.8990 0.920 1.7153 0.9323 3.2631 0.9600 3662.6571 +HPC 202.18 21.786 0.8532 0.993 2.0971 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.019 0.9328 100.148 5.0187 1.4085 0.4249 0.9803 1.5311 +LPT 149.79 6.347 0.9248 100.309 6.3473 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4771.67 18674.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 869.92 208.89 38.505 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 869.92 208.89 38.505 +Duct1 0.0025 0.4393 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 869.92 208.89 38.505 +Duct2 0.0025 0.4381 365.99 +Duct3 0.0050 0.2977 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.0578 1184.20 287.29 127.590 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.3765 1184.20 287.29 127.590 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 534.58 127.77 10.338 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5099 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7313.5 14208.8 19785.6 +LP_Shaft 3419.9 37313.5 24296.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2274.85 0.9940 0.0550 1.82859 0.01733 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.351 0.9969 1.0000 0.9975 2706.36 1.000 1032.3 23349.3 +Core_Nozz 2.080 0.9997 1.0000 0.9999 862.88 1.000 1561.2 6127.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 298 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 30000.0 0.00 705.62 8102.1 0.6141 4975.61 5.9880 796.07 15.973 2088.2 2037.5 1615.4 + core size:20.54 Q: 281.77 Maximum Thrust: 13503.5 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 705.62 6.654 464.56 110.99 0.0000 1474.85 4.364 411.69 4461.2 0.8000 1.40124 +FS_2 Inlet.Fl_O 705.62 6.621 464.56 110.99 0.0000 1482.28 5.648 443.88 5943.4 0.4818 1.40124 +FS_21 Fan.Fl_O 705.62 9.681 523.16 125.03 0.0000 1075.80 8.407 502.47 4515.2 0.4534 1.40044 +FS_13 Splitter.Fl_O2 604.64 9.681 523.16 125.03 0.0000 921.85 8.347 501.44 3795.6 0.4650 1.40044 +FS_22 Splitter.Fl_O1 100.98 9.681 523.16 125.03 0.0000 153.95 8.690 507.24 719.5 0.3957 1.40044 +FS_23 Duct1.Fl_O 100.98 9.657 523.16 125.03 0.0000 154.34 8.668 507.24 721.3 0.3957 1.40044 +FS_24 LPC.Fl_O 100.98 20.629 671.28 160.63 0.0000 81.84 18.290 648.69 366.0 0.4184 1.39703 +FS_25 Duct2.Fl_O 100.98 20.577 671.28 160.63 0.0000 82.04 18.245 648.69 366.9 0.4184 1.39703 +FS_3 HPC.Fl_O 100.98 106.287 1122.09 271.56 0.0000 20.54 99.622 1102.50 119.9 0.3083 1.37305 +FS_36 Bld3.Fl_O 91.89 106.287 1122.09 271.56 0.0000 18.69 99.622 1102.50 109.1 0.3083 1.37305 +FS_4 Burner.Fl_O 93.27 100.441 2088.20 538.64 0.0150 27.38 99.795 2084.97 483.4 0.0991 1.31447 +FS_45 HPT.Fl_O 102.36 36.881 1615.45 405.49 0.0137 71.98 34.773 1591.74 439.1 0.2979 1.33479 +FS_48 Duct3.Fl_O 102.36 36.697 1615.45 405.49 0.0137 72.34 34.600 1591.74 441.4 0.2979 1.33479 +FS_5 LPT.Fl_O 102.36 7.622 1118.20 273.60 0.0137 289.79 6.978 1092.14 1477.4 0.3616 1.36392 +FS_7 Duct4.Fl_O 102.36 7.545 1118.20 273.60 0.0137 292.72 7.213 1104.84 2018.9 0.2575 1.36392 +FS_9 Core_Nozz.Fl_O 102.36 7.545 1118.20 273.60 0.0137 292.72 4.364 964.61 862.9 0.9274 1.36392 +FS_15 BypBld.Fl_O 604.64 9.681 523.16 125.03 0.0000 921.85 8.347 501.44 3795.6 0.4650 1.40044 +FS_17 Duct5.Fl_O 604.64 9.608 523.16 125.03 0.0000 928.82 8.284 501.44 3824.3 0.4650 1.40044 +FS_19 Byp_Nozz.Fl_O 604.64 9.608 523.16 125.03 0.0000 928.82 5.073 435.76 2706.4 1.0000 1.40044 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1482.28 1.462 0.9105 3371.298 1.1261 0.9152 -14015.1 39.30 19.67 +LPC 154.34 2.136 0.8539 3176.871 1.2831 0.8686 -5086.5 24.95 16.45 +HPC 82.04 5.165 0.8659 6249.164 1.6716 0.8922 -15848.4 26.52 26.68 +HPT 27.38 2.723 0.9149 155.575 1.2472 0.9046 15848.6 +LPT 72.34 4.815 0.9209 79.383 1.4447 0.9042 19101.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2841.99 1.322 0.9406 0.855 2.0394 0.5215 1.4369 0.9679 3943.9586 +LPC 165.54 1.348 0.8895 0.867 1.6166 0.9323 3.2631 0.9600 3662.6571 +HPC 195.04 20.255 0.8543 0.983 2.1330 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.056 0.9332 101.609 5.0561 1.4085 0.4249 0.9803 1.5311 +LPT 150.32 6.322 0.9197 97.869 6.3217 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4461.17 17459.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 831.35 199.46 33.134 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 831.35 199.46 33.134 +Duct1 0.0025 0.3957 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 831.35 199.46 33.134 +Duct2 0.0025 0.4184 365.99 +Duct3 0.0050 0.2979 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3616 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.5342 1122.09 271.56 106.287 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.5537 1122.09 271.56 106.287 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 523.16 125.03 9.681 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9880 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7109.3 11708.4 15848.6 +LP_Shaft 3190.6 31443.0 19101.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2088.20 0.9940 0.0550 1.38211 0.01504 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.202 0.9974 1.0000 0.9975 2706.36 1.000 1021.2 21111.7 +Core_Nozz 1.729 0.9999 1.0000 0.9999 862.88 0.927 1398.5 4449.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 299 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 30000.0 0.00 648.47 5401.5 0.6472 3495.69 6.6919 796.07 12.637 1880.9 1836.8 1447.0 + core size:20.95 Q: 281.77 Maximum Thrust: 13503.5 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 648.47 6.654 464.56 110.99 0.0000 1355.39 4.364 411.69 4099.8 0.8000 1.40124 +FS_2 Inlet.Fl_O 648.47 6.621 464.56 110.99 0.0000 1362.21 5.826 447.85 5943.4 0.4311 1.40124 +FS_21 Fan.Fl_O 648.47 8.918 509.98 121.87 0.0000 1059.60 7.786 490.55 4515.2 0.4445 1.40066 +FS_13 Splitter.Fl_O2 564.16 8.918 509.98 121.87 0.0000 921.85 7.689 488.80 3795.6 0.4649 1.40066 +FS_22 Splitter.Fl_O1 84.30 8.918 509.98 121.87 0.0000 137.76 8.206 497.99 719.5 0.3466 1.40066 +FS_23 Duct1.Fl_O 84.30 8.896 509.98 121.87 0.0000 138.10 8.186 497.99 721.3 0.3466 1.40066 +FS_24 LPC.Fl_O 84.30 17.421 637.90 152.59 0.0000 78.87 15.608 618.23 366.0 0.3996 1.39820 +FS_25 Duct2.Fl_O 84.30 17.378 637.90 152.59 0.0000 79.07 15.569 618.23 366.9 0.3996 1.39820 +FS_3 HPC.Fl_O 84.30 84.087 1048.30 253.03 0.0000 20.95 78.585 1029.01 119.9 0.3147 1.37769 +FS_36 Bld3.Fl_O 76.72 84.087 1048.30 253.03 0.0000 19.06 78.585 1029.01 109.1 0.3147 1.37769 +FS_4 Burner.Fl_O 77.69 79.462 1880.95 478.54 0.0127 27.36 78.952 1877.98 483.4 0.0987 1.32360 +FS_45 HPT.Fl_O 85.28 28.923 1447.04 359.18 0.0115 72.37 27.251 1425.08 439.1 0.2985 1.34508 +FS_48 Duct3.Fl_O 85.28 28.778 1447.04 359.18 0.0115 72.74 27.115 1425.08 441.4 0.2985 1.34508 +FS_5 LPT.Fl_O 85.28 6.379 1011.87 246.08 0.0115 274.41 5.902 990.73 1477.4 0.3382 1.37219 +FS_7 Duct4.Fl_O 85.28 6.315 1011.87 246.08 0.0115 277.18 6.067 1000.95 2018.9 0.2420 1.37219 +FS_9 Core_Nozz.Fl_O 85.28 6.315 1011.87 246.08 0.0115 277.18 4.364 914.77 862.9 0.7512 1.37219 +FS_15 BypBld.Fl_O 564.16 8.918 509.98 121.87 0.0000 921.85 7.689 488.80 3795.6 0.4649 1.40066 +FS_17 Duct5.Fl_O 564.16 8.851 509.98 121.87 0.0000 928.81 7.632 488.80 3824.3 0.4649 1.40066 +FS_19 Byp_Nozz.Fl_O 564.16 8.851 509.98 121.87 0.0000 928.81 4.673 424.76 2706.3 1.0000 1.40066 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1362.21 1.347 0.9101 3053.329 1.0978 0.9139 -9981.3 46.99 21.40 +LPC 138.10 1.958 0.8435 2914.184 1.2508 0.8575 -3664.4 22.64 13.00 +HPC 79.07 4.839 0.8647 6198.934 1.6434 0.8905 -11980.2 31.44 31.68 +HPT 27.36 2.747 0.9154 158.511 1.2564 0.9048 11980.2 +LPT 72.74 4.511 0.9160 75.964 1.4301 0.8988 13645.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2611.86 1.241 0.9403 0.774 2.0750 0.5215 1.4369 0.9679 3943.9586 +LPC 148.13 1.294 0.8786 0.796 1.5395 0.9323 3.2631 0.9600 3662.6571 +HPC 187.97 18.746 0.8530 0.975 2.1677 0.4206 0.2163 1.0137 6357.1603 +HPT 30.10 5.113 0.9338 103.527 5.1127 1.4085 0.4249 0.9803 1.5311 +LPT 151.14 5.898 0.9148 93.654 5.8983 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4099.81 16044.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 783.26 187.74 27.151 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 783.26 187.74 27.151 +Duct1 0.0025 0.3466 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 783.26 187.74 27.151 +Duct2 0.0025 0.3996 365.99 +Duct3 0.0050 0.2985 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3382 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.9507 1048.30 253.03 84.087 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.6368 1048.30 253.03 84.087 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 509.98 121.87 8.918 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6919 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6874.6 9152.7 11980.2 +LP_Shaft 2889.7 24802.2 13645.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1880.95 0.9940 0.0550 0.97103 0.01266 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.028 0.9976 1.0000 0.9975 2706.36 1.000 1008.3 18517.5 +Core_Nozz 1.447 0.9999 1.0000 0.9999 862.88 0.751 1105.0 2928.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 300 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 30000.0 0.00 580.11 2700.8 0.7751 2093.40 7.8874 796.07 9.051 1615.2 1579.5 1233.4 + core size:21.56 Q: 281.77 Maximum Thrust: 13503.5 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 580.11 6.654 464.56 110.99 0.0000 1212.52 4.364 411.69 3667.7 0.8000 1.40124 +FS_2 Inlet.Fl_O 580.11 6.621 464.56 110.99 0.0000 1218.63 6.005 451.76 5943.4 0.3758 1.40124 +FS_21 Fan.Fl_O 580.11 8.017 494.00 118.04 0.0000 1037.81 7.048 476.12 4515.2 0.4327 1.40091 +FS_13 Splitter.Fl_O2 514.84 8.017 494.00 118.04 0.0000 921.03 6.915 473.52 3795.6 0.4644 1.40091 +FS_22 Splitter.Fl_O1 65.27 8.017 494.00 118.04 0.0000 116.77 7.570 485.95 719.5 0.2874 1.40091 +FS_23 Duct1.Fl_O 65.27 7.997 494.00 118.04 0.0000 117.07 7.551 485.95 721.3 0.2874 1.40091 +FS_24 LPC.Fl_O 65.27 13.734 593.44 141.90 0.0000 74.71 12.469 577.31 366.0 0.3741 1.39914 +FS_25 Duct2.Fl_O 65.27 13.699 593.44 141.90 0.0000 74.90 12.438 577.31 366.9 0.3741 1.39914 +FS_3 HPC.Fl_O 65.27 60.227 950.37 228.68 0.0000 21.56 56.032 931.52 119.9 0.3245 1.38378 +FS_36 Bld3.Fl_O 59.40 60.227 950.37 228.68 0.0000 19.62 56.032 931.52 109.1 0.3245 1.38378 +FS_4 Burner.Fl_O 59.98 56.914 1615.17 403.83 0.0098 27.33 56.549 1612.55 483.4 0.0981 1.33749 +FS_45 HPT.Fl_O 65.85 20.476 1233.44 302.19 0.0089 72.89 19.275 1213.85 439.1 0.2992 1.35978 +FS_48 Duct3.Fl_O 65.85 20.374 1233.44 302.19 0.0089 73.25 19.179 1213.85 441.4 0.2992 1.35978 +FS_5 LPT.Fl_O 65.85 5.430 895.24 216.43 0.0089 234.18 5.141 881.86 1477.4 0.2820 1.38127 +FS_7 Duct4.Fl_O 65.85 5.375 895.24 216.43 0.0089 236.54 5.224 888.20 2018.9 0.2039 1.38127 +FS_9 Core_Nozz.Fl_O 65.85 5.375 895.24 216.43 0.0089 236.54 4.364 845.11 862.9 0.5565 1.38127 +FS_15 BypBld.Fl_O 514.84 8.017 494.00 118.04 0.0000 921.03 6.915 473.52 3795.6 0.4644 1.40091 +FS_17 Duct5.Fl_O 514.84 7.957 494.00 118.04 0.0000 927.99 6.863 473.52 3824.3 0.4644 1.40091 +FS_19 Byp_Nozz.Fl_O 514.84 7.957 494.00 118.04 0.0000 927.99 4.364 415.94 2706.3 0.9671 1.40091 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1218.63 1.211 0.8882 2616.864 1.0634 0.8912 -5787.4 57.36 24.01 +LPC 117.07 1.717 0.8305 2537.675 1.2013 0.8429 -2203.3 22.50 9.65 +HPC 74.90 4.396 0.8626 6119.140 1.6015 0.8873 -8014.8 38.92 39.50 +HPT 27.33 2.780 0.9164 162.864 1.2693 0.9054 8014.9 +LPT 73.25 3.752 0.9116 70.517 1.3778 0.8954 7990.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2336.55 1.147 0.9176 0.664 2.2551 0.5215 1.4369 0.9679 3943.9586 +LPC 125.57 1.220 0.8650 0.693 1.4940 0.9323 3.2631 0.9600 3662.6571 +HPC 178.06 16.700 0.8509 0.963 2.2524 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.188 0.9348 106.369 5.1883 1.4085 0.4249 0.9803 1.5311 +LPT 152.21 4.839 0.9104 86.939 4.8395 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3667.67 14353.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 719.46 172.27 20.516 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 719.46 172.27 20.516 +Duct1 0.0025 0.2874 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 719.46 172.27 20.516 +Duct2 0.0025 0.3741 365.99 +Duct3 0.0050 0.2992 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2820 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.2846 950.37 228.68 60.227 +Duct5 0.0075 0.4644 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.5900 950.37 228.68 60.227 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 494.00 118.04 8.017 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8874 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6545.4 6431.3 8014.9 +LP_Shaft 2476.6 16946.0 7990.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1615.17 0.9940 0.0550 0.58150 0.00979 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.823 0.9975 1.0000 0.9975 2706.36 0.967 964.9 15440.7 +Core_Nozz 1.232 0.9999 1.0000 0.9999 862.88 0.556 788.4 1613.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 301 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 11/ 21/ 1/ 9 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 30000.0 0.00 512.43 675.2 1.5760 1064.08 9.7507 796.07 5.969 1320.3 1294.1 1000.6 + core size:22.45 Q: 281.77 Maximum Thrust: 13503.5 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 512.43 6.654 464.56 110.99 0.0000 1071.06 4.364 411.69 3239.8 0.8000 1.40124 +FS_2 Inlet.Fl_O 512.43 6.621 464.56 110.99 0.0000 1076.45 6.153 454.91 5943.4 0.3251 1.40124 +FS_21 Fan.Fl_O 512.43 7.228 479.61 114.59 0.0000 1001.89 6.423 463.68 4515.2 0.4139 1.40110 +FS_13 Splitter.Fl_O2 464.77 7.228 479.61 114.59 0.0000 908.70 6.266 460.40 3795.6 0.4561 1.40110 +FS_22 Splitter.Fl_O1 47.66 7.228 479.61 114.59 0.0000 93.19 6.977 474.79 719.5 0.2251 1.40110 +FS_23 Duct1.Fl_O 47.66 7.210 479.61 114.59 0.0000 93.43 6.960 474.79 721.3 0.2251 1.40110 +FS_24 LPC.Fl_O 47.66 10.443 545.22 130.32 0.0000 68.77 9.643 532.94 366.0 0.3393 1.40000 +FS_25 Duct2.Fl_O 47.66 10.417 545.22 130.32 0.0000 68.94 9.619 532.94 366.9 0.3393 1.40000 +FS_3 HPC.Fl_O 47.66 39.716 840.70 201.74 0.0000 22.45 36.694 822.22 119.9 0.3392 1.39002 +FS_36 Bld3.Fl_O 43.38 39.716 840.70 201.74 0.0000 20.43 36.694 822.22 109.1 0.3392 1.39002 +FS_4 Burner.Fl_O 43.67 37.532 1320.29 324.20 0.0068 27.28 37.292 1318.07 483.4 0.0973 1.35581 +FS_45 HPT.Fl_O 47.96 13.346 1000.60 242.27 0.0062 73.35 12.554 983.96 439.1 0.2994 1.37643 +FS_48 Duct3.Fl_O 47.96 13.280 1000.60 242.27 0.0062 73.72 12.491 983.96 441.4 0.2994 1.37643 +FS_5 LPT.Fl_O 47.96 4.875 781.85 188.12 0.0062 177.50 4.731 775.28 1477.4 0.2087 1.38895 +FS_7 Duct4.Fl_O 47.96 4.827 781.85 188.12 0.0062 179.29 4.750 778.33 2018.9 0.1525 1.38895 +FS_9 Core_Nozz.Fl_O 47.96 4.827 781.85 188.12 0.0062 179.29 4.364 760.08 862.9 0.3835 1.38895 +FS_15 BypBld.Fl_O 464.77 7.228 479.61 114.59 0.0000 908.70 6.266 460.40 3795.6 0.4561 1.40110 +FS_17 Duct5.Fl_O 464.77 7.174 479.61 114.59 0.0000 915.57 6.219 460.40 3824.3 0.4561 1.40110 +FS_19 Byp_Nozz.Fl_O 464.77 7.174 479.61 114.59 0.0000 915.57 4.364 415.98 2706.4 0.8731 1.40110 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1076.45 1.092 0.7847 2080.997 1.0324 0.7874 -2613.6 81.05 25.91 +LPC 93.43 1.448 0.8174 2048.072 1.1368 0.8268 -1060.4 26.55 7.83 +HPC 68.94 3.813 0.8526 6010.353 1.5419 0.8772 -4816.6 50.59 51.62 +HPT 27.28 2.812 0.9180 169.592 1.2852 0.9067 4816.6 +LPT 73.72 2.724 0.9021 62.261 1.2798 0.8888 3674.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2063.95 1.064 0.8107 0.528 2.6330 0.5215 1.4369 0.9679 3943.9586 +LPC 100.21 1.137 0.8514 0.559 1.5243 0.9323 3.2631 0.9600 3662.6571 +HPC 163.90 14.002 0.8411 0.945 2.3856 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.265 0.9364 110.763 5.2651 1.4085 0.4249 0.9803 1.5311 +LPT 153.18 3.405 0.9009 76.760 3.4046 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3239.77 12679.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 649.23 155.32 14.709 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 649.23 155.32 14.709 +Duct1 0.0025 0.2251 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 649.23 155.32 14.709 +Duct2 0.0025 0.3393 365.99 +Duct3 0.0050 0.2994 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2087 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.6683 840.70 201.74 39.716 +Duct5 0.0075 0.4561 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.6216 840.70 201.74 39.716 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 479.61 114.59 7.228 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.7507 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6162.2 4105.2 4816.6 +LP_Shaft 1969.5 9797.8 3674.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1320.29 0.9940 0.0550 0.29558 0.00681 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.644 0.9975 1.0000 0.9975 2706.36 0.873 871.2 12584.4 +Core_Nozz 1.106 0.9999 1.0000 0.9999 862.88 0.384 516.4 769.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 302 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 4/ 14/ 1/ 2 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 30000.0 0.00 832.93 13894.7 0.6451 8962.97 5.0412 845.83 22.707 2487.5 2424.3 1944.9 + core size:19.92 Q: 318.10 Maximum Thrust: 13894.7 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 832.93 7.001 471.37 112.62 0.0000 1666.72 4.364 411.69 4956.3 0.8500 1.40119 +FS_2 Inlet.Fl_O 832.93 6.966 471.37 112.62 0.0000 1675.11 5.561 441.92 5943.4 0.5763 1.40119 +FS_21 Fan.Fl_O 832.93 11.456 554.46 132.54 0.0000 1104.75 9.849 531.02 4515.2 0.4697 1.39982 +FS_13 Splitter.Fl_O2 695.06 11.456 554.46 132.54 0.0000 921.88 9.877 531.46 3795.6 0.4651 1.39982 +FS_22 Splitter.Fl_O1 137.88 11.456 554.46 132.54 0.0000 182.87 9.691 528.58 719.5 0.4947 1.39982 +FS_23 Duct1.Fl_O 137.88 11.427 554.46 132.54 0.0000 183.33 9.667 528.58 721.3 0.4947 1.39982 +FS_24 LPC.Fl_O 137.88 28.444 743.68 178.14 0.0000 85.30 24.890 716.10 366.0 0.4415 1.39451 +FS_25 Duct2.Fl_O 137.88 28.373 743.68 178.14 0.0000 85.51 24.828 716.10 366.9 0.4415 1.39451 +FS_3 HPC.Fl_O 137.88 158.978 1267.35 308.54 0.0000 19.92 149.633 1247.00 119.9 0.2991 1.36392 +FS_36 Bld3.Fl_O 125.47 158.978 1267.35 308.54 0.0000 18.13 149.633 1247.00 109.1 0.2991 1.36392 +FS_4 Burner.Fl_O 127.96 150.234 2487.50 658.52 0.0198 27.41 149.265 2483.78 483.4 0.0998 1.30050 +FS_45 HPT.Fl_O 140.36 56.335 1944.94 499.48 0.0181 70.91 53.214 1918.39 439.1 0.2950 1.31743 +FS_48 Duct3.Fl_O 140.36 56.053 1944.94 499.48 0.0181 71.26 52.948 1918.39 441.4 0.2950 1.31743 +FS_5 LPT.Fl_O 140.36 11.510 1354.32 336.52 0.0181 289.61 10.538 1323.89 1477.4 0.3638 1.34614 +FS_7 Duct4.Fl_O 140.36 11.395 1354.32 336.52 0.0181 292.53 10.894 1338.74 2018.9 0.2591 1.34614 +FS_9 Core_Nozz.Fl_O 140.36 11.395 1354.32 336.52 0.0181 292.53 6.095 1150.56 862.9 1.0000 1.34614 +FS_15 BypBld.Fl_O 695.06 11.456 554.46 132.54 0.0000 921.88 9.877 531.46 3795.6 0.4651 1.39982 +FS_17 Duct5.Fl_O 695.06 11.370 554.46 132.54 0.0000 928.85 9.803 531.46 3824.3 0.4651 1.39982 +FS_19 Byp_Nozz.Fl_O 695.06 11.370 554.46 132.54 0.0000 928.85 6.004 461.88 2706.4 1.0000 1.39982 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.644 0.8675 3944.235 1.1763 0.8765 -23469.8 24.71 17.45 +LPC 183.33 2.489 0.8683 3636.711 1.3413 0.8839 -8895.2 28.34 23.26 +HPC 85.51 5.603 0.8652 6324.635 1.7042 0.8922 -25439.1 20.16 20.22 +HPT 27.41 2.667 0.9135 151.845 1.2312 0.9036 25439.1 +LPT 71.26 4.870 0.9326 85.260 1.4361 0.9185 32364.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8962 1.000 2.3709 0.5215 1.4369 0.9679 3943.9586 +LPC 196.64 1.456 0.9044 0.993 1.7654 0.9323 3.2631 0.9600 3662.6571 +HPC 203.30 22.280 0.8535 0.995 2.0429 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.923 0.9318 99.173 4.9230 1.4085 0.4249 0.9803 1.5311 +LPT 148.08 6.399 0.9314 105.115 6.3986 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4956.32 21897.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 930.51 223.78 47.506 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 930.51 223.78 47.506 +Duct1 0.0025 0.4947 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 930.51 223.78 47.506 +Duct2 0.0025 0.4415 365.99 +Duct3 0.0050 0.2950 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3638 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.8256 1267.35 308.54 158.978 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.5831 1267.35 308.54 158.978 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 554.46 132.54 11.456 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0412 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7573.2 17642.2 25439.1 +LP_Shaft 3760.1 45207.4 32364.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2487.50 0.9940 0.0550 2.48971 0.01984 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.605 0.9954 1.0000 0.9975 2706.36 1.000 1051.4 27152.6 +Core_Nozz 2.611 0.9968 1.0000 0.9999 862.88 1.000 1638.0 8639.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 303 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 30000.0 0.00 812.05 12504.8 0.6343 7931.79 5.3051 845.83 20.810 2398.4 2337.9 1868.8 + core size:20.02 Q: 318.10 Maximum Thrust: 13894.7 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 812.05 7.001 471.37 112.62 0.0000 1624.94 4.364 411.69 4832.1 0.8500 1.40119 +FS_2 Inlet.Fl_O 812.05 6.966 471.37 112.62 0.0000 1633.12 5.655 444.04 5943.4 0.5539 1.40119 +FS_21 Fan.Fl_O 812.05 11.197 548.18 131.03 0.0000 1095.67 9.658 525.49 4515.2 0.4645 1.39994 +FS_13 Splitter.Fl_O2 683.26 11.197 548.18 131.03 0.0000 921.89 9.654 525.43 3795.6 0.4651 1.39994 +FS_22 Splitter.Fl_O1 128.79 11.197 548.18 131.03 0.0000 173.77 9.675 525.76 719.5 0.4616 1.39994 +FS_23 Duct1.Fl_O 128.79 11.169 548.18 131.03 0.0000 174.21 9.651 525.76 721.3 0.4616 1.39994 +FS_24 LPC.Fl_O 128.79 26.044 720.78 172.59 0.0000 85.67 22.756 693.72 366.0 0.4439 1.39532 +FS_25 Duct2.Fl_O 128.79 25.978 720.78 172.59 0.0000 85.89 22.699 693.72 366.9 0.4439 1.39532 +FS_3 HPC.Fl_O 128.79 145.697 1231.35 299.32 0.0000 20.02 137.048 1211.29 119.9 0.3004 1.36617 +FS_36 Bld3.Fl_O 117.20 145.697 1231.35 299.32 0.0000 18.21 137.048 1211.29 109.1 0.3004 1.36617 +FS_4 Burner.Fl_O 119.40 137.684 2398.45 631.38 0.0188 27.41 136.796 2394.84 483.4 0.0997 1.30327 +FS_45 HPT.Fl_O 131.00 51.120 1868.75 477.40 0.0171 71.48 48.239 1842.56 439.1 0.2972 1.32105 +FS_48 Duct3.Fl_O 131.00 50.864 1868.75 477.40 0.0171 71.84 47.998 1842.56 441.4 0.2972 1.32105 +FS_5 LPT.Fl_O 131.00 10.523 1302.29 322.43 0.0171 289.87 9.633 1272.74 1477.4 0.3637 1.34996 +FS_7 Duct4.Fl_O 131.00 10.418 1302.29 322.43 0.0171 292.80 9.959 1287.16 2018.9 0.2589 1.34996 +FS_9 Core_Nozz.Fl_O 131.00 10.418 1302.29 322.43 0.0171 292.80 5.566 1104.62 862.9 1.0000 1.34996 +FS_15 BypBld.Fl_O 683.26 11.197 548.18 131.03 0.0000 921.89 9.654 525.43 3795.6 0.4651 1.39994 +FS_17 Duct5.Fl_O 683.26 11.114 548.18 131.03 0.0000 928.86 9.582 525.43 3824.3 0.4651 1.39994 +FS_19 Byp_Nozz.Fl_O 683.26 11.114 548.18 131.03 0.0000 928.86 5.869 456.64 2706.4 1.0000 1.39994 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1633.12 1.607 0.8925 3742.753 1.1629 0.8995 -21149.7 28.21 17.74 +LPC 174.21 2.332 0.8660 3470.651 1.3149 0.8808 -7573.6 28.81 22.11 +HPC 85.89 5.608 0.8642 6333.886 1.7083 0.8914 -23091.9 20.57 20.60 +HPT 27.41 2.693 0.9139 152.462 1.2359 0.9041 23092.0 +LPT 71.84 4.833 0.9281 82.538 1.4350 0.9131 28723.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3131.13 1.423 0.9220 0.949 2.1755 0.5215 1.4369 0.9679 3943.9586 +LPC 186.86 1.408 0.9020 0.948 1.7502 0.9323 3.2631 0.9600 3662.6571 +HPC 204.18 22.304 0.8525 0.996 2.0708 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.985 0.9323 99.576 4.9855 1.4085 0.4249 0.9803 1.5311 +LPT 149.27 6.348 0.9269 101.758 6.3475 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4832.07 21348.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 902.74 216.95 43.517 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 902.74 216.95 43.517 +Duct1 0.0025 0.4616 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 902.74 216.95 43.517 +Duct2 0.0025 0.4439 365.99 +Duct3 0.0050 0.2972 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3637 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.5078 1231.35 299.32 145.697 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 7.0836 1231.35 299.32 145.697 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 548.18 131.03 11.197 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3051 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7466.7 16243.1 23092.0 +LP_Shaft 3568.0 42280.1 28723.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2398.45 0.9940 0.0550 2.20328 0.01880 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.547 0.9958 1.0000 0.9975 2706.36 1.000 1045.4 26273.0 +Core_Nozz 2.387 0.9984 1.0000 0.9999 862.88 1.000 1607.1 7580.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 304 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 30000.0 0.00 788.40 11115.8 0.6295 6997.34 5.5102 845.83 19.173 2306.3 2248.7 1792.5 + core size:20.17 Q: 318.10 Maximum Thrust: 13894.7 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 788.40 7.001 471.37 112.62 0.0000 1577.60 4.364 411.69 4691.3 0.8500 1.40119 +FS_2 Inlet.Fl_O 788.40 6.966 471.37 112.62 0.0000 1585.55 5.753 446.23 5943.4 0.5299 1.40119 +FS_21 Fan.Fl_O 788.40 10.879 542.42 129.65 0.0000 1089.18 9.404 520.30 4515.2 0.4609 1.40006 +FS_13 Splitter.Fl_O2 667.30 10.879 542.42 129.65 0.0000 921.87 9.379 519.91 3795.6 0.4651 1.40006 +FS_22 Splitter.Fl_O1 121.10 10.879 542.42 129.65 0.0000 167.30 9.528 522.25 719.5 0.4393 1.40006 +FS_23 Duct1.Fl_O 121.10 10.851 542.42 129.65 0.0000 167.72 9.504 522.25 721.3 0.4393 1.40006 +FS_24 LPC.Fl_O 121.10 24.494 706.51 169.14 0.0000 84.80 21.476 680.63 366.0 0.4380 1.39579 +FS_25 Duct2.Fl_O 121.10 24.433 706.51 169.14 0.0000 85.01 21.422 680.63 366.9 0.4380 1.39579 +FS_3 HPC.Fl_O 121.10 134.234 1200.53 291.45 0.0000 20.17 126.133 1180.56 119.9 0.3028 1.36811 +FS_36 Bld3.Fl_O 110.20 134.234 1200.53 291.45 0.0000 18.36 126.133 1180.56 109.1 0.3028 1.36811 +FS_4 Burner.Fl_O 112.15 126.851 2306.30 603.49 0.0176 27.40 126.034 2302.81 483.4 0.0995 1.30649 +FS_45 HPT.Fl_O 123.05 46.869 1792.49 455.47 0.0161 71.72 44.209 1766.96 439.1 0.2979 1.32498 +FS_48 Duct3.Fl_O 123.05 46.634 1792.49 455.47 0.0161 72.08 43.988 1766.96 441.4 0.2979 1.32498 +FS_5 LPT.Fl_O 123.05 9.659 1246.70 307.51 0.0161 290.23 8.840 1218.09 1477.4 0.3636 1.35415 +FS_7 Duct4.Fl_O 123.05 9.563 1246.70 307.51 0.0161 293.17 9.141 1232.06 2018.9 0.2589 1.35415 +FS_9 Core_Nozz.Fl_O 123.05 9.563 1246.70 307.51 0.0161 293.17 5.104 1055.67 862.9 1.0000 1.35415 +FS_15 BypBld.Fl_O 667.30 10.879 542.42 129.65 0.0000 921.87 9.379 519.91 3795.6 0.4651 1.40006 +FS_17 Duct5.Fl_O 667.30 10.797 542.42 129.65 0.0000 928.84 9.309 519.91 3824.3 0.4651 1.40006 +FS_19 Byp_Nozz.Fl_O 667.30 10.797 542.42 129.65 0.0000 928.84 5.701 451.83 2706.4 1.0000 1.40006 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1585.55 1.562 0.9023 3613.825 1.1507 0.9083 -18991.9 31.67 18.33 +LPC 167.72 2.257 0.8630 3368.844 1.3025 0.8778 -6766.7 27.99 20.44 +HPC 85.01 5.494 0.8649 6311.422 1.6992 0.8918 -20956.6 22.19 22.28 +HPT 27.40 2.707 0.9145 153.385 1.2397 0.9046 20956.4 +LPT 72.08 4.828 0.9260 81.372 1.4378 0.9104 25758.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3040.10 1.391 0.9322 0.916 2.0967 0.5215 1.4369 0.9679 3943.9586 +LPC 179.90 1.385 0.8990 0.920 1.7146 0.9323 3.2631 0.9600 3662.6571 +HPC 202.11 21.775 0.8532 0.993 2.0968 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.016 0.9328 100.178 5.0165 1.4085 0.4249 0.9803 1.5311 +LPT 149.78 6.340 0.9248 100.321 6.3398 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4691.32 20726.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 882.39 211.95 40.519 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 882.39 211.95 40.519 +Duct1 0.0025 0.4393 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 882.39 211.95 40.519 +Duct2 0.0025 0.4380 365.99 +Duct3 0.0050 0.2979 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.2386 1200.53 291.45 134.234 +Duct5 0.0075 0.4651 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.6606 1200.53 291.45 134.234 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 542.42 129.65 10.879 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5102 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7366.1 14942.1 20956.4 +LP_Shaft 3445.1 39269.7 25758.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2306.30 0.9940 0.0550 1.94371 0.01764 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.474 0.9962 1.0000 0.9975 2706.36 1.000 1039.9 25187.1 +Core_Nozz 2.191 0.9994 1.0000 0.9999 862.88 1.000 1573.3 6655.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 305 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 30000.0 0.00 737.51 8336.8 0.6340 5285.19 5.9879 845.83 15.978 2116.3 2065.0 1638.4 + core size:20.54 Q: 318.10 Maximum Thrust: 13894.7 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 737.51 7.001 471.37 112.62 0.0000 1475.77 4.364 411.69 4388.5 0.8500 1.40119 +FS_2 Inlet.Fl_O 737.51 6.966 471.37 112.62 0.0000 1483.19 5.941 450.36 5943.4 0.4822 1.40119 +FS_21 Fan.Fl_O 737.51 10.193 530.94 126.89 0.0000 1075.81 8.852 509.95 4515.2 0.4534 1.40029 +FS_13 Splitter.Fl_O2 631.97 10.193 530.94 126.89 0.0000 921.86 8.788 508.90 3795.6 0.4650 1.40029 +FS_22 Splitter.Fl_O1 105.54 10.193 530.94 126.89 0.0000 153.95 9.149 514.79 719.5 0.3958 1.40029 +FS_23 Duct1.Fl_O 105.54 10.168 530.94 126.89 0.0000 154.34 9.127 514.79 721.3 0.3958 1.40029 +FS_24 LPC.Fl_O 105.54 21.749 681.53 163.10 0.0000 81.75 19.290 658.68 366.0 0.4179 1.39665 +FS_25 Duct2.Fl_O 105.54 21.695 681.53 163.10 0.0000 81.95 19.242 658.68 366.9 0.4179 1.39665 +FS_3 HPC.Fl_O 105.54 111.867 1137.90 275.56 0.0000 20.54 104.851 1118.07 119.9 0.3085 1.37206 +FS_36 Bld3.Fl_O 96.04 111.867 1137.90 275.56 0.0000 18.69 104.851 1118.07 109.1 0.3085 1.37206 +FS_4 Burner.Fl_O 97.51 105.715 2116.31 546.86 0.0153 27.38 105.034 2113.05 483.4 0.0992 1.31341 +FS_45 HPT.Fl_O 107.01 38.835 1638.40 411.87 0.0139 71.97 36.615 1614.43 439.1 0.2980 1.33352 +FS_48 Duct3.Fl_O 107.01 38.641 1638.40 411.87 0.0139 72.33 36.432 1614.43 441.4 0.2980 1.33352 +FS_5 LPT.Fl_O 107.01 7.996 1134.27 277.78 0.0139 290.85 7.315 1107.68 1477.4 0.3633 1.36274 +FS_7 Duct4.Fl_O 107.01 7.916 1134.27 277.78 0.0139 293.79 7.565 1120.65 2018.9 0.2586 1.36274 +FS_9 Core_Nozz.Fl_O 107.01 7.916 1134.27 277.78 0.0139 293.79 4.364 966.12 862.9 0.9704 1.36274 +FS_15 BypBld.Fl_O 631.97 10.193 530.94 126.89 0.0000 921.86 8.788 508.90 3795.6 0.4650 1.40029 +FS_17 Duct5.Fl_O 631.97 10.117 530.94 126.89 0.0000 928.83 8.723 508.90 3824.3 0.4650 1.40029 +FS_19 Byp_Nozz.Fl_O 631.97 10.117 530.94 126.89 0.0000 928.83 5.342 442.25 2706.4 1.0000 1.40029 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1483.19 1.463 0.9105 3373.687 1.1264 0.9152 -14893.5 39.22 19.65 +LPC 154.34 2.139 0.8537 3178.795 1.2836 0.8685 -5407.0 24.83 16.37 +HPC 81.95 5.156 0.8659 6247.495 1.6696 0.8921 -16791.6 26.63 26.79 +HPT 27.38 2.722 0.9149 155.672 1.2463 0.9046 16791.7 +LPT 72.33 4.833 0.9209 79.457 1.4445 0.9041 20300.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2843.78 1.322 0.9406 0.855 2.0391 0.5215 1.4369 0.9679 3943.9586 +LPC 165.55 1.349 0.8893 0.868 1.6139 0.9323 3.2631 0.9600 3662.6571 +HPC 194.82 20.214 0.8543 0.983 2.1332 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.053 0.9332 101.672 5.0533 1.4085 0.4249 0.9803 1.5311 +LPT 150.30 6.346 0.9197 97.960 6.3464 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4388.48 19388.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 843.65 202.46 34.905 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 843.65 202.46 34.905 +Duct1 0.0025 0.3958 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 843.65 202.46 34.905 +Duct2 0.0025 0.4179 365.99 +Duct3 0.0050 0.2980 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3633 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.6939 1137.90 275.56 111.867 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.8047 1137.90 275.56 111.867 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 530.94 126.89 10.193 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9879 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7161.5 12314.8 16791.7 +LP_Shaft 3216.2 33151.1 20300.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2116.31 0.9940 0.0550 1.46811 0.01529 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.318 0.9970 1.0000 0.9975 2706.36 1.000 1028.8 22854.8 +Core_Nozz 1.814 0.9999 1.0000 0.9999 862.88 0.970 1464.4 4870.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 306 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 30000.0 0.00 679.05 5557.7 0.6678 3711.30 6.6878 845.83 12.665 1905.0 1860.5 1466.8 + core size:20.97 Q: 318.10 Maximum Thrust: 13894.7 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 679.05 7.001 471.37 112.62 0.0000 1358.78 4.364 411.69 4040.6 0.8500 1.40119 +FS_2 Inlet.Fl_O 679.05 6.966 471.37 112.62 0.0000 1365.62 6.125 454.32 5943.4 0.4325 1.40119 +FS_21 Fan.Fl_O 679.05 9.410 517.90 123.77 0.0000 1059.68 8.216 498.17 4515.2 0.4445 1.40053 +FS_13 Splitter.Fl_O2 590.72 9.410 517.90 123.77 0.0000 921.84 8.114 496.39 3795.6 0.4650 1.40053 +FS_22 Splitter.Fl_O1 88.33 9.410 517.90 123.77 0.0000 137.84 8.658 505.71 719.5 0.3469 1.40053 +FS_23 Duct1.Fl_O 88.33 9.387 517.90 123.77 0.0000 138.19 8.636 505.71 721.3 0.3469 1.40053 +FS_24 LPC.Fl_O 88.33 18.473 648.92 155.24 0.0000 78.60 16.565 629.08 366.0 0.3979 1.39785 +FS_25 Duct2.Fl_O 88.33 18.426 648.92 155.24 0.0000 78.80 16.523 629.08 366.9 0.3979 1.39785 +FS_3 HPC.Fl_O 88.33 88.675 1063.99 256.96 0.0000 20.97 82.861 1044.41 119.9 0.3152 1.37671 +FS_36 Bld3.Fl_O 80.38 88.675 1063.99 256.96 0.0000 19.08 82.861 1044.41 109.1 0.3152 1.37671 +FS_4 Burner.Fl_O 81.41 83.798 1905.01 485.38 0.0128 27.36 83.260 1902.01 483.4 0.0988 1.32253 +FS_45 HPT.Fl_O 89.36 30.526 1466.81 364.52 0.0117 72.35 28.763 1444.62 439.1 0.2985 1.34388 +FS_48 Duct3.Fl_O 89.36 30.373 1466.81 364.52 0.0117 72.71 28.619 1444.62 441.4 0.2985 1.34388 +FS_5 LPT.Fl_O 89.36 6.603 1022.15 248.70 0.0117 279.20 6.090 999.96 1477.4 0.3452 1.37143 +FS_7 Duct4.Fl_O 89.36 6.537 1022.15 248.70 0.0117 282.02 6.271 1010.71 2018.9 0.2467 1.37143 +FS_9 Core_Nozz.Fl_O 89.36 6.537 1022.15 248.70 0.0117 282.02 4.364 915.48 863.0 0.7875 1.37143 +FS_15 BypBld.Fl_O 590.72 9.410 517.90 123.77 0.0000 921.84 8.114 496.39 3795.6 0.4650 1.40053 +FS_17 Duct5.Fl_O 590.72 9.340 517.90 123.77 0.0000 928.81 8.053 496.39 3824.3 0.4650 1.40053 +FS_19 Byp_Nozz.Fl_O 590.72 9.340 517.90 123.77 0.0000 928.81 4.931 431.37 2706.3 1.0000 1.40053 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1365.62 1.351 0.9104 3063.578 1.0987 0.9142 -10708.7 46.70 21.31 +LPC 138.19 1.968 0.8427 2922.720 1.2530 0.8569 -3933.3 22.20 12.79 +HPC 78.80 4.812 0.8647 6193.831 1.6396 0.8904 -12711.2 31.81 32.06 +HPT 27.36 2.745 0.9155 158.730 1.2554 0.9049 12711.4 +LPT 72.71 4.600 0.9154 76.257 1.4350 0.8978 14642.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2618.40 1.244 0.9405 0.777 2.0712 0.5215 1.4369 0.9679 3943.9586 +LPC 148.22 1.297 0.8778 0.798 1.5299 0.9323 3.2631 0.9600 3662.6571 +HPC 187.33 18.624 0.8530 0.974 2.1702 0.4206 0.2163 1.0137 6357.1603 +HPT 30.10 5.107 0.9338 103.669 5.1075 1.4085 0.4249 0.9803 1.5311 +LPT 151.07 6.022 0.9142 94.015 6.0218 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4040.61 17851.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 796.00 190.84 28.718 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 796.00 190.84 28.718 +Duct1 0.0025 0.3469 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 796.00 190.84 28.718 +Duct2 0.0025 0.3979 365.99 +Duct3 0.0050 0.2985 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3452 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.0915 1063.99 256.96 88.675 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.8580 1063.99 256.96 88.675 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 517.90 123.77 9.410 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6878 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6928.0 9636.5 12711.4 +LP_Shaft 2920.6 26331.7 14642.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1905.01 0.9940 0.0550 1.03092 0.01283 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.140 0.9975 1.0000 0.9975 2706.36 1.000 1016.1 20191.1 +Core_Nozz 1.498 0.9999 1.0000 0.9999 862.88 0.787 1158.7 3218.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 307 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 30000.0 0.00 608.94 2779.0 0.7989 2220.28 7.8787 845.83 9.095 1634.9 1599.0 1249.7 + core size:21.60 Q: 318.10 Maximum Thrust: 13894.7 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 608.94 7.001 471.37 112.62 0.0000 1218.50 4.364 411.69 3623.5 0.8500 1.40119 +FS_2 Inlet.Fl_O 608.94 6.966 471.37 112.62 0.0000 1224.64 6.311 458.23 5943.4 0.3780 1.40119 +FS_21 Fan.Fl_O 608.94 8.474 501.92 119.94 0.0000 1038.86 7.448 483.71 4515.2 0.4333 1.40079 +FS_13 Splitter.Fl_O2 540.36 8.474 501.92 119.94 0.0000 921.86 7.306 481.07 3795.6 0.4649 1.40079 +FS_22 Splitter.Fl_O1 68.58 8.474 501.92 119.94 0.0000 117.01 7.999 493.71 719.5 0.2881 1.40079 +FS_23 Duct1.Fl_O 68.58 8.453 501.92 119.94 0.0000 117.30 7.979 493.71 721.3 0.2881 1.40079 +FS_24 LPC.Fl_O 68.58 14.648 604.93 144.66 0.0000 74.31 13.316 588.70 366.0 0.3717 1.39897 +FS_25 Duct2.Fl_O 68.58 14.611 604.93 144.66 0.0000 74.50 13.282 588.70 366.9 0.3717 1.39897 +FS_3 HPC.Fl_O 68.58 63.679 965.76 232.49 0.0000 21.60 59.226 946.55 119.9 0.3253 1.38283 +FS_36 Bld3.Fl_O 62.41 63.679 965.76 232.49 0.0000 19.65 59.226 946.55 109.1 0.3253 1.38283 +FS_4 Burner.Fl_O 63.03 60.176 1634.89 409.24 0.0099 27.33 59.790 1632.25 483.4 0.0981 1.33646 +FS_45 HPT.Fl_O 69.20 21.670 1249.67 306.42 0.0090 72.85 20.400 1229.89 439.1 0.2991 1.35870 +FS_48 Duct3.Fl_O 69.20 21.561 1249.67 306.42 0.0090 73.21 20.298 1229.89 441.4 0.2991 1.35870 +FS_5 LPT.Fl_O 69.20 5.544 899.66 217.54 0.0090 241.60 5.229 885.26 1477.4 0.2919 1.38094 +FS_7 Duct4.Fl_O 69.20 5.488 899.66 217.54 0.0090 244.04 5.323 892.11 2018.9 0.2107 1.38094 +FS_9 Core_Nozz.Fl_O 69.20 5.488 899.66 217.54 0.0090 244.04 4.364 844.42 863.0 0.5845 1.38094 +FS_15 BypBld.Fl_O 540.36 8.474 501.92 119.94 0.0000 921.86 7.306 481.07 3795.6 0.4649 1.40079 +FS_17 Duct5.Fl_O 540.36 8.410 501.92 119.94 0.0000 928.82 7.252 481.07 3824.3 0.4649 1.40079 +FS_19 Byp_Nozz.Fl_O 540.36 8.410 501.92 119.94 0.0000 928.82 4.441 418.05 2706.3 1.0000 1.40079 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1224.64 1.216 0.8899 2637.302 1.0648 0.8930 -6303.3 56.73 23.89 +LPC 117.30 1.733 0.8289 2555.788 1.2052 0.8416 -2399.0 21.57 9.33 +HPC 74.50 4.358 0.8623 6111.643 1.5965 0.8870 -8522.7 39.55 40.16 +HPT 27.33 2.777 0.9164 163.238 1.2684 0.9055 8522.9 +LPT 73.21 3.889 0.9118 71.121 1.3891 0.8952 8702.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2348.07 1.151 0.9194 0.669 2.2442 0.5215 1.4369 0.9679 3943.9586 +LPC 125.81 1.225 0.8634 0.698 1.4752 0.9323 3.2631 0.9600 3662.6571 +HPC 177.10 16.524 0.8507 0.961 2.2593 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.182 0.9348 106.614 5.1823 1.4085 0.4249 0.9803 1.5311 +LPT 152.13 5.030 0.9107 87.683 5.0304 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3623.46 16008.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 732.39 175.40 21.800 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 732.39 175.40 21.800 +Duct1 0.0025 0.2881 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 732.39 175.40 21.800 +Duct2 0.0025 0.3717 365.99 +Duct3 0.0050 0.2991 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2919 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.4005 965.76 232.49 63.679 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.7721 965.76 232.49 63.679 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 501.92 119.94 8.474 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8787 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6600.3 6781.9 8522.9 +LP_Shaft 2514.2 18179.7 8702.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1634.89 0.9940 0.0550 0.61674 0.00988 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.927 0.9975 1.0000 0.9975 2706.36 1.000 1000.3 17007.3 +Core_Nozz 1.258 0.9999 1.0000 0.9999 862.88 0.584 827.7 1780.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 308 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 10/ 30/ 2/ 7 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 30000.0 0.00 541.93 694.7 1.6313 1133.31 9.7786 845.83 6.028 1339.2 1312.9 1015.9 + core size:22.50 Q: 318.10 Maximum Thrust: 13894.7 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 541.93 7.001 471.37 112.62 0.0000 1084.42 4.364 411.69 3224.7 0.8500 1.40119 +FS_2 Inlet.Fl_O 541.93 6.966 471.37 112.62 0.0000 1089.88 6.460 461.31 5943.4 0.3298 1.40119 +FS_21 Fan.Fl_O 541.93 7.635 487.29 116.43 0.0000 1011.04 6.767 470.74 4515.2 0.4186 1.40100 +FS_13 Splitter.Fl_O2 491.65 7.635 487.29 116.43 0.0000 917.24 6.596 467.30 3795.6 0.4618 1.40100 +FS_22 Splitter.Fl_O1 50.28 7.635 487.29 116.43 0.0000 93.80 7.367 482.32 719.5 0.2266 1.40100 +FS_23 Duct1.Fl_O 50.28 7.616 487.29 116.43 0.0000 94.04 7.348 482.32 721.3 0.2266 1.40100 +FS_24 LPC.Fl_O 50.28 11.193 556.86 133.11 0.0000 68.40 10.346 544.48 366.0 0.3372 1.39977 +FS_25 Duct2.Fl_O 50.28 11.165 556.86 133.11 0.0000 68.57 10.320 544.48 366.9 0.3372 1.39977 +FS_3 HPC.Fl_O 50.28 42.201 856.33 205.56 0.0000 22.50 38.976 837.45 119.9 0.3400 1.38926 +FS_36 Bld3.Fl_O 45.75 42.201 856.33 205.56 0.0000 20.47 38.976 837.45 109.1 0.3400 1.38926 +FS_4 Burner.Fl_O 46.07 39.880 1339.24 329.18 0.0069 27.28 39.625 1336.99 483.4 0.0973 1.35461 +FS_45 HPT.Fl_O 50.59 14.190 1015.92 246.12 0.0063 73.33 13.348 999.07 439.1 0.2994 1.37542 +FS_48 Duct3.Fl_O 50.59 14.119 1015.92 246.12 0.0063 73.70 13.281 999.07 441.4 0.2994 1.37542 +FS_5 LPT.Fl_O 50.59 4.930 784.24 188.72 0.0063 185.44 4.770 777.02 1477.4 0.2186 1.38879 +FS_7 Duct4.Fl_O 50.59 4.881 784.24 188.72 0.0063 187.31 4.796 780.38 2018.9 0.1595 1.38879 +FS_9 Core_Nozz.Fl_O 50.59 4.881 784.24 188.72 0.0063 187.31 4.364 760.02 862.9 0.4046 1.38879 +FS_15 BypBld.Fl_O 491.65 7.635 487.29 116.43 0.0000 917.24 6.596 467.30 3795.6 0.4618 1.40100 +FS_17 Duct5.Fl_O 491.65 7.578 487.29 116.43 0.0000 924.17 6.546 467.30 3824.3 0.4618 1.40100 +FS_19 Byp_Nozz.Fl_O 491.65 7.578 487.29 116.43 0.0000 924.17 4.364 416.06 2706.4 0.9237 1.40100 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1089.88 1.096 0.7875 2117.235 1.0338 0.7903 -2922.7 79.79 26.28 +LPC 94.04 1.470 0.8154 2082.366 1.1428 0.8252 -1186.6 24.74 7.44 +HPC 68.57 3.780 0.8517 6003.542 1.5378 0.8762 -5153.9 51.29 52.34 +HPT 27.28 2.810 0.9180 169.984 1.2843 0.9068 5153.9 +LPT 73.70 2.864 0.9028 63.325 1.2954 0.8890 4109.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2089.69 1.067 0.8135 0.537 2.6261 0.5215 1.4369 0.9679 3943.9586 +LPC 100.87 1.144 0.8493 0.569 1.4919 0.9323 3.2631 0.9600 3662.6571 +HPC 163.02 13.850 0.8402 0.944 2.3895 0.4206 0.2163 1.0137 6357.1603 +HPT 30.01 5.261 0.9365 111.019 5.2610 1.4085 0.4249 0.9803 1.5311 +LPT 153.14 3.600 0.9017 78.072 3.5999 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3224.74 14246.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 662.32 158.47 15.712 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 662.32 158.47 15.712 +Duct1 0.0025 0.2266 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 662.32 158.47 15.712 +Duct2 0.0025 0.3372 365.99 +Duct3 0.0050 0.2994 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2186 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.7598 856.33 205.56 42.201 +Duct5 0.0075 0.4618 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.7653 856.33 205.56 42.201 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 487.29 116.43 7.635 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.7786 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6220.7 4351.4 5153.9 +LP_Shaft 2018.4 10693.0 4109.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1339.24 0.9940 0.0550 0.31481 0.00688 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.737 0.9975 1.0000 0.9975 2706.36 0.924 921.7 14085.1 +Core_Nozz 1.118 0.9999 1.0000 0.9999 862.88 0.405 544.7 856.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 309 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 9/ 19/ 1/ 7 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 35000.0 0.00 554.39 9899.9 0.5295 5241.56 5.0385 583.98 22.744 2245.4 2188.1 1746.7 + core size:19.97 Q: 125.59 Maximum Thrust: 9899.9 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 554.39 4.411 422.30 100.88 0.0000 1666.72 3.458 393.85 5768.9 0.6000 1.40130 +FS_2 Inlet.Fl_O 554.39 4.389 422.30 100.88 0.0000 1675.11 3.503 395.92 5943.4 0.5763 1.40130 +FS_21 Fan.Fl_O 554.39 7.217 496.81 118.71 0.0000 1104.88 6.204 475.77 4515.2 0.4696 1.40087 +FS_13 Splitter.Fl_O2 462.58 7.217 496.81 118.71 0.0000 921.90 6.222 476.17 3795.6 0.4650 1.40087 +FS_22 Splitter.Fl_O1 91.81 7.217 496.81 118.71 0.0000 182.97 6.104 473.55 719.5 0.4949 1.40087 +FS_23 Duct1.Fl_O 91.81 7.199 496.81 118.71 0.0000 183.43 6.089 473.55 721.3 0.4949 1.40087 +FS_24 LPC.Fl_O 91.81 17.894 666.60 159.50 0.0000 85.48 15.647 641.64 366.0 0.4423 1.39720 +FS_25 Duct2.Fl_O 91.81 17.849 666.60 159.50 0.0000 85.70 15.608 641.64 366.9 0.4423 1.39720 +FS_3 HPC.Fl_O 91.81 100.319 1143.47 276.96 0.0000 19.97 94.395 1124.74 119.9 0.2990 1.37170 +FS_36 Bld3.Fl_O 83.55 100.319 1143.47 276.96 0.0000 18.17 94.395 1124.74 109.1 0.2990 1.37170 +FS_4 Burner.Fl_O 85.00 94.801 2245.43 585.59 0.0174 27.42 94.189 2242.01 483.4 0.0995 1.30826 +FS_45 HPT.Fl_O 93.26 35.461 1746.73 442.62 0.0159 70.93 33.496 1722.33 439.1 0.2940 1.32713 +FS_48 Duct3.Fl_O 93.26 35.284 1746.73 442.62 0.0159 71.29 33.329 1722.33 441.4 0.2940 1.32713 +FS_5 LPT.Fl_O 93.26 7.189 1204.55 296.44 0.0159 290.53 6.579 1176.69 1477.4 0.3636 1.35696 +FS_7 Duct4.Fl_O 93.26 7.118 1204.55 296.44 0.0159 293.46 6.803 1190.29 2018.9 0.2589 1.35696 +FS_9 Core_Nozz.Fl_O 93.26 7.118 1204.55 296.44 0.0159 293.46 3.797 1018.84 862.9 1.0000 1.35696 +FS_15 BypBld.Fl_O 462.58 7.217 496.81 118.71 0.0000 921.90 6.222 476.17 3795.6 0.4650 1.40087 +FS_17 Duct5.Fl_O 462.58 7.163 496.81 118.71 0.0000 928.87 6.176 476.17 3824.3 0.4650 1.40087 +FS_19 Byp_Nozz.Fl_O 462.58 7.163 496.81 118.71 0.0000 928.87 3.782 413.79 2706.4 1.0000 1.40087 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.644 0.8675 3944.235 1.1764 0.8765 -13991.4 24.72 17.46 +LPC 183.43 2.486 0.8685 3636.473 1.3418 0.8841 -5298.6 28.51 23.41 +HPC 85.70 5.620 0.8649 6329.322 1.7154 0.8925 -15257.3 19.99 20.04 +HPT 27.42 2.673 0.9132 151.424 1.2373 0.9031 15257.7 +LPT 71.29 4.908 0.9319 85.156 1.4501 0.9172 19289.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.448 0.8962 1.000 2.3713 0.5215 1.4369 0.9679 3943.9586 +LPC 196.77 1.455 0.9046 0.993 1.7700 0.9323 3.2631 0.9600 3662.6571 +HPC 203.73 22.359 0.8533 0.996 2.0431 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.939 0.9315 98.898 4.9385 1.4085 0.4249 0.9803 1.5311 +LPT 148.13 6.451 0.9307 104.987 6.4511 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5768.89 10062.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 836.08 200.61 29.931 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 836.08 200.61 29.931 +Duct1 0.0025 0.4949 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 836.08 200.61 29.931 +Duct2 0.0025 0.4423 365.99 +Duct3 0.0050 0.2940 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.2133 1143.47 276.96 100.319 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.0495 1143.47 276.96 100.319 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 496.81 118.71 7.217 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0385 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7175.4 11168.0 15257.7 +LP_Shaft 3559.0 28465.4 19289.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2245.43 0.9940 0.0550 1.45599 0.01743 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.071 0.9975 1.0000 0.9975 2706.36 1.000 995.1 15185.4 +Core_Nozz 2.058 0.9997 1.0000 0.9999 862.88 1.000 1547.0 4777.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 310 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 35000.0 0.00 540.08 8910.0 0.5191 4624.93 5.3073 583.98 20.802 2162.2 2107.3 1675.8 + core size:20.06 Q: 125.59 Maximum Thrust: 9899.9 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 540.08 4.411 422.30 100.88 0.0000 1623.71 3.458 393.85 5620.0 0.6000 1.40130 +FS_2 Inlet.Fl_O 540.08 4.389 422.30 100.88 0.0000 1631.88 3.564 397.87 5943.4 0.5532 1.40130 +FS_21 Fan.Fl_O 540.08 7.049 491.03 117.33 0.0000 1095.62 6.080 470.68 4515.2 0.4643 1.40095 +FS_13 Splitter.Fl_O2 454.46 7.049 491.03 117.33 0.0000 921.91 6.077 470.63 3795.6 0.4649 1.40095 +FS_22 Splitter.Fl_O1 85.63 7.049 491.03 117.33 0.0000 173.71 6.091 470.94 719.5 0.4612 1.40095 +FS_23 Duct1.Fl_O 85.63 7.031 491.03 117.33 0.0000 174.14 6.076 470.94 721.3 0.4612 1.40095 +FS_24 LPC.Fl_O 85.63 16.358 645.66 154.46 0.0000 85.83 14.285 621.21 366.0 0.4445 1.39796 +FS_25 Duct2.Fl_O 85.63 16.317 645.66 154.46 0.0000 86.04 14.249 621.21 366.9 0.4445 1.39796 +FS_3 HPC.Fl_O 85.63 91.753 1109.74 268.45 0.0000 20.06 86.282 1091.30 119.9 0.3003 1.37383 +FS_36 Bld3.Fl_O 77.92 91.753 1109.74 268.45 0.0000 18.26 86.282 1091.30 109.1 0.3003 1.37383 +FS_4 Burner.Fl_O 79.21 86.707 2162.17 560.83 0.0165 27.41 86.147 2158.86 483.4 0.0994 1.31120 +FS_45 HPT.Fl_O 86.91 32.109 1675.79 422.60 0.0150 71.50 30.299 1651.75 439.1 0.2962 1.33099 +FS_48 Duct3.Fl_O 86.91 31.948 1675.79 422.60 0.0150 71.86 30.148 1651.75 441.4 0.2962 1.33099 +FS_5 LPT.Fl_O 86.91 6.557 1156.53 283.77 0.0150 290.89 5.998 1129.51 1477.4 0.3636 1.36059 +FS_7 Duct4.Fl_O 86.91 6.491 1156.53 283.77 0.0150 293.83 6.203 1142.70 2018.9 0.2589 1.36059 +FS_9 Core_Nozz.Fl_O 86.91 6.491 1156.53 283.77 0.0150 293.83 3.460 976.81 862.9 1.0000 1.36059 +FS_15 BypBld.Fl_O 454.46 7.049 491.03 117.33 0.0000 921.91 6.077 470.63 3795.6 0.4649 1.40095 +FS_17 Duct5.Fl_O 454.46 6.996 491.03 117.33 0.0000 928.88 6.032 470.63 3824.3 0.4649 1.40095 +FS_19 Byp_Nozz.Fl_O 454.46 6.996 491.03 117.33 0.0000 928.88 3.694 408.98 2706.3 1.0000 1.40095 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1631.88 1.606 0.8928 3739.077 1.1628 0.8997 -12573.3 28.31 17.77 +LPC 174.14 2.327 0.8661 3467.536 1.3149 0.8809 -4498.0 28.97 22.21 +HPC 86.04 5.623 0.8639 6338.210 1.7188 0.8918 -13810.1 20.44 20.46 +HPT 27.41 2.700 0.9137 152.082 1.2422 0.9034 13810.0 +LPT 71.86 4.873 0.9274 82.418 1.4490 0.9118 17071.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3129.01 1.422 0.9223 0.948 2.1737 0.5215 1.4369 0.9679 3943.9586 +LPC 186.79 1.407 0.9021 0.947 1.7536 0.9323 3.2631 0.9600 3662.6571 +HPC 204.56 22.371 0.8523 0.997 2.0718 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 5.002 0.9320 99.327 5.0021 1.4085 0.4249 0.9803 1.5311 +LPT 149.33 6.402 0.9262 101.611 6.4022 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5620.04 9802.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 810.42 194.35 27.369 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 810.42 194.35 27.369 +Duct1 0.0025 0.4612 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 810.42 194.35 27.369 +Duct2 0.0025 0.4445 365.99 +Duct3 0.0050 0.2962 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.9970 1109.74 268.45 91.753 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.7096 1109.74 268.45 91.753 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 491.03 117.33 7.049 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3073 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7071.7 10256.6 13810.0 +LP_Shaft 3373.9 26575.4 17071.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2162.17 0.9940 0.0550 1.28470 0.01649 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.023 0.9975 1.0000 0.9975 2706.36 1.000 989.3 14613.9 +Core_Nozz 1.877 0.9999 1.0000 0.9999 862.88 1.000 1516.6 4099.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 311 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 35000.0 0.00 523.71 7919.9 0.5144 4074.31 5.5164 583.98 19.128 2078.0 2025.8 1606.4 + core size:20.21 Q: 125.59 Maximum Thrust: 9899.9 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 523.71 4.411 422.30 100.88 0.0000 1574.49 3.458 393.85 5449.7 0.6000 1.40130 +FS_2 Inlet.Fl_O 523.71 4.389 422.30 100.88 0.0000 1582.41 3.628 399.91 5943.4 0.5283 1.40130 +FS_21 Fan.Fl_O 523.71 6.838 485.65 116.04 0.0000 1089.08 5.912 465.82 4515.2 0.4607 1.40102 +FS_13 Splitter.Fl_O2 443.34 6.838 485.65 116.04 0.0000 921.95 5.896 465.46 3795.6 0.4650 1.40102 +FS_22 Splitter.Fl_O1 80.37 6.838 485.65 116.04 0.0000 167.13 5.991 467.61 719.5 0.4385 1.40102 +FS_23 Duct1.Fl_O 80.37 6.821 485.65 116.04 0.0000 167.55 5.976 467.61 721.3 0.4385 1.40102 +FS_24 LPC.Fl_O 80.37 15.342 632.25 151.23 0.0000 85.00 13.442 608.87 366.0 0.4389 1.39836 +FS_25 Duct2.Fl_O 80.37 15.303 632.25 151.23 0.0000 85.21 13.408 608.87 366.9 0.4389 1.39836 +FS_3 HPC.Fl_O 80.37 84.368 1080.82 261.17 0.0000 20.21 79.258 1062.51 119.9 0.3025 1.37565 +FS_36 Bld3.Fl_O 73.14 84.368 1080.82 261.17 0.0000 18.39 79.258 1062.51 109.1 0.3025 1.37565 +FS_4 Burner.Fl_O 74.27 79.728 2078.03 535.99 0.0155 27.40 79.214 2074.82 483.4 0.0992 1.31450 +FS_45 HPT.Fl_O 81.50 29.372 1606.41 403.19 0.0141 71.76 27.705 1582.99 439.1 0.2969 1.33497 +FS_48 Duct3.Fl_O 81.50 29.226 1606.41 403.19 0.0141 72.12 27.566 1582.99 441.4 0.2969 1.33497 +FS_5 LPT.Fl_O 81.50 6.040 1107.90 271.04 0.0141 289.81 5.530 1082.06 1477.4 0.3615 1.36433 +FS_7 Duct4.Fl_O 81.50 5.980 1107.90 271.04 0.0141 292.74 5.717 1094.66 2018.9 0.2575 1.36433 +FS_9 Core_Nozz.Fl_O 81.50 5.980 1107.90 271.04 0.0141 292.74 3.458 955.59 862.9 0.9275 1.36433 +FS_15 BypBld.Fl_O 443.34 6.838 485.65 116.04 0.0000 921.95 5.896 465.46 3795.6 0.4650 1.40102 +FS_17 Duct5.Fl_O 443.34 6.787 485.65 116.04 0.0000 928.91 5.852 465.46 3824.3 0.4650 1.40102 +FS_19 Byp_Nozz.Fl_O 443.34 6.787 485.65 116.04 0.0000 928.91 3.584 404.49 2706.4 1.0000 1.40102 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1582.41 1.558 0.9027 3606.223 1.1500 0.9086 -11236.3 31.94 18.39 +LPC 167.55 2.249 0.8632 3362.824 1.3019 0.8778 -4001.3 28.21 20.56 +HPC 85.21 5.513 0.8647 6316.166 1.7095 0.8922 -12501.8 21.99 22.05 +HPT 27.40 2.714 0.9144 152.977 1.2462 0.9041 12501.7 +LPT 72.12 4.839 0.9256 81.188 1.4500 0.9097 15237.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3034.07 1.388 0.9326 0.914 2.0941 0.5215 1.4369 0.9679 3943.9586 +LPC 179.72 1.383 0.8991 0.918 1.7193 0.9323 3.2631 0.9600 3662.6571 +HPC 202.58 21.863 0.8530 0.994 2.0969 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 5.035 0.9327 99.912 5.0350 1.4085 0.4249 0.9803 1.5311 +LPT 149.87 6.355 0.9244 100.094 6.3547 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5449.66 9505.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 791.35 189.71 25.421 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 791.35 189.71 25.421 +Duct1 0.0025 0.4385 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 791.35 189.71 25.421 +Duct2 0.0025 0.4389 365.99 +Duct3 0.0050 0.2969 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3615 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.8129 1080.82 261.17 84.368 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.4202 1080.82 261.17 84.368 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 485.65 116.04 6.838 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5164 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6973.5 9415.7 12501.7 +LP_Shaft 3254.0 24594.2 15237.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2078.03 0.9940 0.0550 1.13175 0.01547 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.963 0.9975 1.0000 0.9975 2706.36 1.000 983.9 13899.0 +Core_Nozz 1.729 0.9999 1.0000 0.9999 862.88 0.927 1392.2 3526.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 312 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 35000.0 0.00 486.13 5939.7 0.5177 3075.04 6.0012 583.98 15.816 1909.0 1862.2 1468.9 + core size:20.52 Q: 125.59 Maximum Thrust: 9899.9 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 486.13 4.411 422.30 100.88 0.0000 1461.52 3.458 393.85 5058.6 0.6000 1.40130 +FS_2 Inlet.Fl_O 486.13 4.389 422.30 100.88 0.0000 1468.87 3.758 403.95 5943.4 0.4759 1.40130 +FS_21 Fan.Fl_O 486.13 6.356 474.19 113.30 0.0000 1074.67 5.522 455.47 4515.2 0.4526 1.40116 +FS_13 Splitter.Fl_O2 416.70 6.356 474.19 113.30 0.0000 921.17 5.482 454.52 3795.6 0.4644 1.40116 +FS_22 Splitter.Fl_O1 69.44 6.356 474.19 113.30 0.0000 153.50 5.710 459.85 719.5 0.3942 1.40116 +FS_23 Duct1.Fl_O 69.44 6.341 474.19 113.30 0.0000 153.88 5.696 459.85 721.3 0.3942 1.40116 +FS_24 LPC.Fl_O 69.44 13.322 605.21 144.73 0.0000 82.74 11.773 584.24 366.0 0.4240 1.39896 +FS_25 Duct2.Fl_O 69.44 13.288 605.21 144.73 0.0000 82.95 11.743 584.24 366.9 0.4240 1.39896 +FS_3 HPC.Fl_O 69.44 69.763 1020.71 246.14 0.0000 20.52 65.397 1002.71 119.9 0.3073 1.37942 +FS_36 Bld3.Fl_O 63.19 69.763 1020.71 246.14 0.0000 18.67 65.397 1002.71 109.1 0.3073 1.37942 +FS_4 Burner.Fl_O 64.04 65.926 1909.03 486.88 0.0135 27.39 65.501 1906.03 483.4 0.0989 1.32189 +FS_45 HPT.Fl_O 70.29 24.119 1468.88 365.29 0.0123 72.07 22.737 1446.87 439.1 0.2974 1.34333 +FS_48 Duct3.Fl_O 70.29 23.998 1468.88 365.29 0.0123 72.44 22.623 1446.87 441.4 0.2974 1.34333 +FS_5 LPT.Fl_O 70.29 5.203 1020.26 248.34 0.0123 278.47 4.801 998.26 1477.4 0.3442 1.37114 +FS_7 Duct4.Fl_O 70.29 5.151 1020.26 248.34 0.0123 281.28 4.942 1008.92 2018.9 0.2460 1.37114 +FS_9 Core_Nozz.Fl_O 70.29 5.151 1020.26 248.34 0.0123 281.28 3.458 915.26 862.9 0.7818 1.37114 +FS_15 BypBld.Fl_O 416.70 6.356 474.19 113.30 0.0000 921.17 5.482 454.52 3795.6 0.4644 1.40116 +FS_17 Duct5.Fl_O 416.70 6.309 474.19 113.30 0.0000 928.13 5.441 454.52 3824.3 0.4644 1.40116 +FS_19 Byp_Nozz.Fl_O 416.70 6.309 474.19 113.30 0.0000 928.13 3.458 399.17 2706.3 0.9678 1.40116 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1468.87 1.448 0.9107 3337.422 1.1229 0.9153 -8543.6 40.39 19.91 +LPC 153.88 2.101 0.8557 3149.526 1.2763 0.8699 -3087.7 26.20 17.15 +HPC 82.95 5.250 0.8656 6266.313 1.6865 0.8923 -9963.0 25.57 25.71 +HPT 27.39 2.733 0.9148 154.922 1.2536 0.9043 9963.4 +LPT 72.44 4.613 0.9215 78.575 1.4397 0.9051 11630.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2816.20 1.312 0.9409 0.846 2.0414 0.5215 1.4369 0.9679 3943.9586 +LPC 165.06 1.337 0.8914 0.860 1.6445 0.9323 3.2631 0.9600 3662.6571 +HPC 197.19 20.646 0.8539 0.986 2.1342 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.080 0.9331 101.182 5.0797 1.4085 0.4249 0.9803 1.5311 +LPT 150.51 6.040 0.9203 96.873 6.0396 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5058.64 8823.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 752.28 180.22 21.562 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 752.28 180.22 21.562 +Duct1 0.0025 0.3942 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 752.28 180.22 21.562 +Duct2 0.0025 0.4240 365.99 +Duct3 0.0050 0.2974 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3442 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.4302 1020.71 246.14 69.763 +Duct5 0.0075 0.4644 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.8190 1020.71 246.14 69.763 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 474.19 113.30 6.356 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.0012 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6768.9 7730.7 9963.4 +LP_Shaft 3011.5 20284.2 11630.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1909.03 0.9940 0.0550 0.85418 0.01352 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.824 0.9975 1.0000 0.9975 2706.36 0.968 945.9 12250.9 +Core_Nozz 1.490 0.9999 1.0000 0.9999 862.88 0.782 1150.0 2512.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 313 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 35000.0 0.00 440.45 3960.0 0.5426 2148.82 6.6878 583.98 12.364 1718.4 1677.4 1314.3 + core size:20.88 Q: 125.59 Maximum Thrust: 9899.9 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 440.45 4.411 422.30 100.88 0.0000 1324.17 3.458 393.85 4583.2 0.6000 1.40130 +FS_2 Inlet.Fl_O 440.45 4.389 422.30 100.88 0.0000 1330.83 3.890 407.96 5943.4 0.4186 1.40130 +FS_21 Fan.Fl_O 440.45 5.824 461.44 110.24 0.0000 1048.31 5.103 444.31 4515.2 0.4383 1.40127 +FS_13 Splitter.Fl_O2 383.16 5.824 461.44 110.24 0.0000 911.95 5.042 442.78 3795.6 0.4583 1.40127 +FS_22 Splitter.Fl_O1 57.29 5.824 461.44 110.24 0.0000 136.36 5.369 450.83 719.5 0.3425 1.40127 +FS_23 Duct1.Fl_O 57.29 5.809 461.44 110.24 0.0000 136.70 5.356 450.83 721.3 0.3425 1.40127 +FS_24 LPC.Fl_O 57.29 11.010 570.78 136.46 0.0000 80.22 9.818 552.42 366.0 0.4078 1.39952 +FS_25 Duct2.Fl_O 57.29 10.982 570.78 136.46 0.0000 80.42 9.794 552.42 366.9 0.4078 1.39952 +FS_3 HPC.Fl_O 57.29 54.537 948.69 228.27 0.0000 20.88 50.995 931.16 119.9 0.3129 1.38388 +FS_36 Bld3.Fl_O 52.14 54.537 948.69 228.27 0.0000 19.00 50.995 931.16 109.1 0.3129 1.38388 +FS_4 Burner.Fl_O 52.73 51.538 1718.36 432.77 0.0114 27.37 51.206 1715.60 483.4 0.0985 1.33144 +FS_45 HPT.Fl_O 57.89 18.660 1314.32 323.69 0.0104 72.58 17.575 1293.89 439.1 0.2985 1.35369 +FS_48 Duct3.Fl_O 57.89 18.566 1314.32 323.69 0.0104 72.94 17.487 1293.89 441.4 0.2985 1.35369 +FS_5 LPT.Fl_O 57.89 4.539 934.63 226.47 0.0104 251.59 4.258 918.37 1477.4 0.3058 1.37782 +FS_7 Duct4.Fl_O 57.89 4.494 934.63 226.47 0.0104 254.13 4.347 926.14 2018.9 0.2202 1.37782 +FS_9 Core_Nozz.Fl_O 57.89 4.494 934.63 226.47 0.0104 254.13 3.458 869.65 862.9 0.6268 1.37782 +FS_15 BypBld.Fl_O 383.16 5.824 461.44 110.24 0.0000 911.95 5.042 442.78 3795.6 0.4583 1.40127 +FS_17 Duct5.Fl_O 383.16 5.780 461.44 110.24 0.0000 918.84 5.004 442.78 3824.3 0.4583 1.40127 +FS_19 Byp_Nozz.Fl_O 383.16 5.780 461.44 110.24 0.0000 918.84 3.458 398.29 2706.4 0.8889 1.40127 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1330.83 1.327 0.9107 2980.171 1.0927 0.9142 -5837.7 47.64 21.22 +LPC 136.70 1.895 0.8468 2850.995 1.2370 0.8599 -2124.7 25.11 14.04 +HPC 80.42 4.966 0.8649 6220.653 1.6621 0.8909 -7442.2 29.78 29.99 +HPT 27.37 2.762 0.9153 157.423 1.2630 0.9045 7442.2 +LPT 72.94 4.090 0.9186 74.175 1.4062 0.9027 7962.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2551.69 1.228 0.9409 0.756 2.0682 0.5215 1.4369 0.9679 3943.9586 +LPC 146.63 1.274 0.8820 0.778 1.5912 0.9323 3.2631 0.9600 3662.6571 +HPC 191.20 19.333 0.8532 0.979 2.1682 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.147 0.9337 102.816 5.1471 1.4085 0.4249 0.9803 1.5311 +LPT 151.57 5.311 0.9174 91.448 5.3108 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4583.25 7994.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 704.23 168.59 17.363 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 704.23 168.59 17.363 +Duct1 0.0025 0.3425 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 704.23 168.59 17.363 +Duct2 0.0025 0.4078 365.99 +Duct3 0.0050 0.2985 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3058 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.0052 948.69 228.27 54.537 +Duct5 0.0075 0.4583 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.1511 948.69 228.27 54.537 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 461.44 110.24 5.824 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6878 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6525.7 5989.7 7442.2 +LP_Shaft 2689.1 15551.5 7962.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1718.36 0.9940 0.0550 0.59689 0.01145 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.672 0.9975 1.0000 0.9975 2706.36 0.889 867.8 10335.1 +Core_Nozz 1.300 0.9999 1.0000 0.9999 862.88 0.627 900.0 1619.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 314 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 35000.0 0.00 382.00 1980.0 0.6439 1274.89 7.7639 583.98 8.692 1471.5 1438.2 1116.8 + core size:21.43 Q: 125.59 Maximum Thrust: 9899.9 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 382.00 4.411 422.30 100.88 0.0000 1148.46 3.458 393.85 3975.1 0.6000 1.40130 +FS_2 Inlet.Fl_O 382.00 4.389 422.30 100.88 0.0000 1154.24 4.027 412.03 5943.4 0.3524 1.40130 +FS_21 Fan.Fl_O 382.00 5.231 446.62 106.70 0.0000 995.95 4.656 431.99 4515.2 0.4108 1.40133 +FS_13 Splitter.Fl_O2 338.42 5.231 446.62 106.70 0.0000 882.31 4.582 429.99 3795.6 0.4390 1.40133 +FS_22 Splitter.Fl_O1 43.59 5.231 446.62 106.70 0.0000 113.64 4.955 439.76 719.5 0.2789 1.40133 +FS_23 Duct1.Fl_O 43.59 5.218 446.62 106.70 0.0000 113.93 4.943 439.76 721.3 0.2789 1.40133 +FS_24 LPC.Fl_O 43.59 8.444 525.56 125.60 0.0000 76.37 7.627 510.50 366.0 0.3839 1.40039 +FS_25 Duct2.Fl_O 43.59 8.423 525.56 125.60 0.0000 76.56 7.608 510.50 366.9 0.3839 1.40039 +FS_3 HPC.Fl_O 43.59 38.340 852.96 204.74 0.0000 21.43 35.707 836.11 119.9 0.3215 1.38943 +FS_36 Bld3.Fl_O 39.67 38.340 852.96 204.74 0.0000 19.50 35.707 836.11 109.1 0.3215 1.38943 +FS_4 Burner.Fl_O 40.02 36.232 1471.52 364.82 0.0089 27.34 35.999 1469.09 483.4 0.0978 1.34551 +FS_45 HPT.Fl_O 43.94 12.956 1116.83 272.03 0.0081 73.14 12.191 1098.68 439.1 0.2994 1.36773 +FS_48 Duct3.Fl_O 43.94 12.891 1116.83 272.03 0.0081 73.51 12.130 1098.68 441.4 0.2994 1.36773 +FS_5 LPT.Fl_O 43.94 4.027 840.12 202.68 0.0081 204.10 3.867 830.71 1477.4 0.2425 1.38483 +FS_7 Duct4.Fl_O 43.94 3.987 840.12 202.68 0.0081 206.16 3.902 835.12 2018.9 0.1764 1.38483 +FS_9 Core_Nozz.Fl_O 43.94 3.987 840.12 202.68 0.0081 206.16 3.458 807.49 862.8 0.4577 1.38483 +FS_15 BypBld.Fl_O 338.42 5.231 446.62 106.70 0.0000 882.31 4.582 429.99 3795.6 0.4390 1.40133 +FS_17 Duct5.Fl_O 338.42 5.191 446.62 106.70 0.0000 888.97 4.547 429.99 3824.3 0.4390 1.40133 +FS_19 Byp_Nozz.Fl_O 338.42 5.191 446.62 106.70 0.0000 888.97 3.458 397.54 2706.4 0.7844 1.40133 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1154.24 1.192 0.8952 2475.695 1.0576 0.8978 -3145.7 57.01 22.15 +LPC 113.93 1.618 0.8357 2407.358 1.1768 0.8466 -1166.1 27.75 11.06 +HPC 76.56 4.552 0.8631 6150.372 1.6229 0.8885 -4880.3 36.50 36.95 +HPT 27.34 2.796 0.9162 161.393 1.2761 0.9050 4880.3 +LPT 73.51 3.201 0.9083 66.845 1.3294 0.8938 4311.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2213.09 1.134 0.9248 0.628 2.2150 0.5215 1.4369 0.9679 3943.9586 +LPC 122.20 1.190 0.8705 0.657 1.5922 0.9323 3.2631 0.9600 3662.6571 +HPC 182.00 17.420 0.8515 0.967 2.2284 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.228 0.9346 105.409 5.2282 1.4085 0.4249 0.9803 1.5311 +LPT 152.74 4.071 0.9072 82.412 4.0709 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3975.07 6933.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 640.86 153.30 12.806 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 640.86 153.30 12.806 +Duct1 0.0025 0.2789 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 640.86 153.30 12.806 +Duct2 0.0025 0.3839 365.99 +Duct3 0.0050 0.2994 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2425 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.5256 852.96 204.74 38.340 +Duct5 0.0075 0.4390 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.3974 852.96 204.74 38.340 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 446.62 106.70 5.231 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.7639 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6191.1 4140.1 4880.3 +LP_Shaft 2233.9 10137.5 4311.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1471.52 0.9940 0.0550 0.35414 0.00893 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.501 0.9975 1.0000 0.9975 2706.36 0.784 765.1 8047.1 +Core_Nozz 1.153 0.9999 1.0000 0.9999 862.88 0.458 634.4 866.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 315 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 11/ 21/ 1/ 9 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 35000.0 0.00 322.38 495.0 1.2480 617.75 9.3686 583.98 5.545 1179.2 1155.3 888.4 + core size:22.38 Q: 125.59 Maximum Thrust: 9899.9 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 322.38 4.411 422.30 100.88 0.0000 969.20 3.458 393.85 3354.6 0.6000 1.40130 +FS_2 Inlet.Fl_O 322.38 4.389 422.30 100.88 0.0000 974.07 4.139 415.27 5943.4 0.2905 1.40130 +FS_21 Fan.Fl_O 322.38 4.727 433.43 103.54 0.0000 916.15 4.298 421.77 4515.2 0.3711 1.40134 +FS_13 Splitter.Fl_O2 291.29 4.727 433.43 103.54 0.0000 827.79 4.222 419.61 3795.6 0.4051 1.40134 +FS_22 Splitter.Fl_O1 31.09 4.727 433.43 103.54 0.0000 88.36 4.580 429.53 719.5 0.2127 1.40134 +FS_23 Duct1.Fl_O 31.09 4.715 433.43 103.54 0.0000 88.58 4.569 429.53 721.3 0.2127 1.40134 +FS_24 LPC.Fl_O 31.09 6.298 478.97 114.44 0.0000 69.72 5.801 467.82 366.0 0.3446 1.40110 +FS_25 Duct2.Fl_O 31.09 6.282 478.97 114.44 0.0000 69.90 5.786 467.82 366.9 0.3446 1.40110 +FS_3 HPC.Fl_O 31.09 24.458 744.26 178.28 0.0000 22.38 22.612 727.90 119.9 0.3373 1.39449 +FS_36 Bld3.Fl_O 28.29 24.458 744.26 178.28 0.0000 20.36 22.612 727.90 109.1 0.3373 1.39449 +FS_4 Burner.Fl_O 28.46 23.113 1179.17 287.49 0.0061 27.29 22.966 1177.15 483.4 0.0969 1.36518 +FS_45 HPT.Fl_O 31.26 8.179 888.39 214.23 0.0055 73.51 7.691 873.35 439.1 0.2993 1.38387 +FS_48 Duct3.Fl_O 31.26 8.139 888.39 214.23 0.0055 73.88 7.653 873.35 441.4 0.2993 1.38387 +FS_5 LPT.Fl_O 31.26 3.727 732.19 175.92 0.0055 146.48 3.652 728.04 1477.4 0.1707 1.39159 +FS_7 Duct4.Fl_O 31.26 3.689 732.19 175.92 0.0055 147.96 3.649 729.95 2018.9 0.1251 1.39159 +FS_9 Core_Nozz.Fl_O 31.26 3.689 732.19 175.92 0.0055 147.96 3.458 718.95 862.9 0.3066 1.39159 +FS_15 BypBld.Fl_O 291.29 4.727 433.43 103.54 0.0000 827.79 4.222 419.61 3795.6 0.4051 1.40134 +FS_17 Duct5.Fl_O 291.29 4.692 433.43 103.54 0.0000 834.05 4.190 419.61 3824.3 0.4051 1.40134 +FS_19 Byp_Nozz.Fl_O 291.29 4.692 433.43 103.54 0.0000 834.05 3.458 397.15 2706.4 0.6748 1.40134 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 974.07 1.077 0.8164 1867.281 1.0263 0.8183 -1214.9 84.05 21.57 +LPC 88.58 1.336 0.8222 1843.156 1.1051 0.8293 -479.5 36.56 9.38 +HPC 69.90 3.893 0.8545 6027.842 1.5539 0.8791 -2808.1 49.04 50.01 +HPT 27.29 2.826 0.9179 168.687 1.2922 0.9061 2808.1 +LPT 73.88 2.184 0.8966 56.529 1.2133 0.8859 1694.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1867.65 1.054 0.8434 0.473 2.5538 0.5215 1.4369 0.9679 3943.9586 +LPC 95.01 1.103 0.8564 0.503 1.6951 0.9323 3.2631 0.9600 3662.6571 +HPC 166.17 14.376 0.8430 0.948 2.3776 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.297 0.9363 110.173 5.2972 1.4085 0.4249 0.9803 1.5311 +LPT 153.52 2.651 0.8954 69.694 2.6514 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3354.61 5851.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 572.15 136.78 8.945 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 572.15 136.78 8.945 +Duct1 0.0025 0.2127 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 572.15 136.78 8.945 +Duct2 0.0025 0.3446 365.99 +Duct3 0.0050 0.2993 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1707 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.0882 744.26 178.28 24.458 +Duct5 0.0075 0.4051 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 1.7100 744.26 178.28 24.458 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 433.43 103.54 4.727 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.3686 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 5792.6 2546.1 2808.1 +LP_Shaft 1684.9 5282.0 1694.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1179.17 0.9940 0.0550 0.17160 0.00606 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.357 0.9975 1.0000 0.9975 2706.36 0.675 657.9 5955.9 +Core_Nozz 1.067 0.9999 1.0000 0.9999 862.88 0.307 401.8 390.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:53 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 316 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 4/ 14/ 1/ 2 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 35000.0 0.00 595.72 10189.8 0.5686 5794.14 5.0391 681.31 22.737 2296.6 2238.0 1788.6 + core size:19.96 Q: 170.94 Maximum Thrust: 10189.8 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 595.72 4.797 432.58 103.34 0.0000 1666.72 3.458 393.85 5313.4 0.7000 1.40133 +FS_2 Inlet.Fl_O 595.72 4.773 432.58 103.34 0.0000 1675.11 3.810 405.55 5943.4 0.5763 1.40133 +FS_21 Fan.Fl_O 595.72 7.849 508.89 121.61 0.0000 1104.80 6.748 487.35 4515.2 0.4696 1.40068 +FS_13 Splitter.Fl_O2 497.08 7.849 508.89 121.61 0.0000 921.86 6.768 487.75 3795.6 0.4649 1.40068 +FS_22 Splitter.Fl_O1 98.64 7.849 508.89 121.61 0.0000 182.94 6.639 485.08 719.5 0.4948 1.40068 +FS_23 Duct1.Fl_O 98.64 7.830 508.89 121.61 0.0000 183.40 6.622 485.08 721.3 0.4948 1.40068 +FS_24 LPC.Fl_O 98.64 19.470 682.80 163.41 0.0000 85.43 17.029 657.29 366.0 0.4420 1.39661 +FS_25 Duct2.Fl_O 98.64 19.421 682.80 163.41 0.0000 85.64 16.986 657.29 366.9 0.4420 1.39661 +FS_3 HPC.Fl_O 98.64 109.068 1169.65 283.60 0.0000 19.96 102.634 1150.58 119.9 0.2990 1.37005 +FS_36 Bld3.Fl_O 89.77 109.068 1169.65 283.60 0.0000 18.16 102.634 1150.58 109.1 0.2990 1.37005 +FS_4 Burner.Fl_O 91.38 103.070 2296.56 600.85 0.0179 27.42 102.405 2293.08 483.4 0.0996 1.30655 +FS_45 HPT.Fl_O 100.25 38.575 1788.56 454.50 0.0163 70.93 36.438 1763.70 439.1 0.2942 1.32497 +FS_48 Duct3.Fl_O 100.25 38.382 1788.56 454.50 0.0163 71.28 36.255 1763.70 441.4 0.2942 1.32497 +FS_5 LPT.Fl_O 100.25 7.835 1236.06 304.79 0.0163 290.29 7.170 1207.65 1477.4 0.3636 1.35465 +FS_7 Duct4.Fl_O 100.25 7.757 1236.06 304.79 0.0163 293.23 7.414 1221.51 2018.9 0.2589 1.35465 +FS_9 Core_Nozz.Fl_O 100.25 7.757 1236.06 304.79 0.0163 293.23 4.139 1046.45 862.9 1.0000 1.35465 +FS_15 BypBld.Fl_O 497.08 7.849 508.89 121.61 0.0000 921.86 6.768 487.75 3795.6 0.4649 1.40068 +FS_17 Duct5.Fl_O 497.08 7.790 508.89 121.61 0.0000 928.82 6.717 487.75 3824.3 0.4649 1.40068 +FS_19 Byp_Nozz.Fl_O 497.08 7.790 508.89 121.61 0.0000 928.82 4.113 423.86 2706.4 1.0000 1.40068 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.645 0.8675 3944.235 1.1764 0.8765 -15401.3 24.71 17.45 +LPC 183.40 2.487 0.8684 3636.497 1.3417 0.8841 -5834.6 28.46 23.36 +HPC 85.64 5.616 0.8650 6328.039 1.7130 0.8924 -16774.1 20.03 20.08 +HPT 27.42 2.672 0.9132 151.506 1.2359 0.9033 16774.0 +LPT 71.28 4.899 0.9321 85.172 1.4470 0.9174 21235.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8963 1.000 2.3708 0.5215 1.4369 0.9679 3943.9586 +LPC 196.72 1.456 0.9046 0.993 1.7686 0.9323 3.2631 0.9600 3662.6571 +HPC 203.61 22.339 0.8533 0.995 2.0428 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.935 0.9315 98.952 4.9351 1.4085 0.4249 0.9803 1.5311 +LPT 148.12 6.439 0.9309 105.006 6.4387 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5313.42 12614.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 855.98 205.48 32.554 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 855.98 205.48 32.554 +Duct1 0.0025 0.4948 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 855.98 205.48 32.554 +Duct2 0.0025 0.4420 365.99 +Duct3 0.0050 0.2942 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.4526 1169.65 283.60 109.068 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.4255 1169.65 283.60 109.068 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 508.89 121.61 7.849 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0391 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7260.6 12133.9 16774.0 +LP_Shaft 3602.0 30963.8 21235.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2296.56 0.9940 0.0550 1.60948 0.01793 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.253 0.9972 1.0000 0.9975 2706.36 1.000 1007.2 17334.8 +Core_Nozz 2.243 0.9992 1.0000 0.9999 862.88 1.000 1566.6 5469.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:54 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 317 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 35000.0 0.00 580.63 9170.4 0.5584 5120.51 5.3042 681.31 20.820 2212.5 2156.4 1716.7 + core size:20.05 Q: 170.94 Maximum Thrust: 10189.8 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 580.63 4.797 432.58 103.34 0.0000 1624.48 3.458 393.85 5178.8 0.7000 1.40133 +FS_2 Inlet.Fl_O 580.63 4.773 432.58 103.34 0.0000 1632.66 3.875 407.51 5943.4 0.5536 1.40133 +FS_21 Fan.Fl_O 580.63 7.670 503.06 120.21 0.0000 1095.68 6.615 482.21 4515.2 0.4644 1.40077 +FS_13 Splitter.Fl_O2 488.53 7.670 503.06 120.21 0.0000 921.88 6.613 482.16 3795.6 0.4649 1.40077 +FS_22 Splitter.Fl_O1 92.10 7.670 503.06 120.21 0.0000 173.80 6.627 482.45 719.5 0.4616 1.40077 +FS_23 Duct1.Fl_O 92.10 7.650 503.06 120.21 0.0000 174.24 6.610 482.45 721.3 0.4616 1.40077 +FS_24 LPC.Fl_O 92.10 17.811 661.50 158.27 0.0000 85.82 15.553 636.47 366.0 0.4445 1.39739 +FS_25 Duct2.Fl_O 92.10 17.766 661.50 158.27 0.0000 86.04 15.514 636.47 366.9 0.4445 1.39739 +FS_3 HPC.Fl_O 92.10 99.874 1135.71 275.00 0.0000 20.05 93.923 1116.92 119.9 0.3003 1.37219 +FS_36 Bld3.Fl_O 83.81 99.874 1135.71 275.00 0.0000 18.25 93.923 1116.92 109.1 0.3003 1.37219 +FS_4 Burner.Fl_O 85.23 94.381 2212.49 575.72 0.0170 27.41 93.773 2209.11 483.4 0.0994 1.30946 +FS_45 HPT.Fl_O 93.52 34.972 1716.73 434.11 0.0154 71.50 33.001 1692.23 439.1 0.2964 1.32878 +FS_48 Duct3.Fl_O 93.52 34.797 1716.73 434.11 0.0154 71.86 32.836 1692.23 441.4 0.2964 1.32878 +FS_5 LPT.Fl_O 93.52 7.154 1187.34 291.86 0.0154 290.69 6.545 1159.77 1477.4 0.3637 1.35833 +FS_7 Duct4.Fl_O 93.52 7.082 1187.34 291.86 0.0154 293.62 6.769 1173.22 2018.9 0.2589 1.35833 +FS_9 Core_Nozz.Fl_O 93.52 7.082 1187.34 291.86 0.0154 293.62 3.777 1003.73 862.9 1.0000 1.35833 +FS_15 BypBld.Fl_O 488.53 7.670 503.06 120.21 0.0000 921.88 6.613 482.16 3795.6 0.4649 1.40077 +FS_17 Duct5.Fl_O 488.53 7.612 503.06 120.21 0.0000 928.85 6.563 482.16 3824.3 0.4649 1.40077 +FS_19 Byp_Nozz.Fl_O 488.53 7.612 503.06 120.21 0.0000 928.85 4.019 418.99 2706.4 1.0000 1.40077 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1632.66 1.607 0.8926 3741.123 1.1629 0.8996 -13863.1 28.24 17.75 +LPC 174.24 2.328 0.8661 3469.166 1.3150 0.8809 -4960.1 28.96 22.23 +HPC 86.04 5.622 0.8639 6337.923 1.7169 0.8917 -15210.8 20.46 20.48 +HPT 27.41 2.699 0.9137 152.169 1.2409 0.9036 15210.9 +LPT 71.86 4.864 0.9275 82.459 1.4459 0.9120 18822.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3130.16 1.422 0.9222 0.949 2.1743 0.5215 1.4369 0.9679 3943.9586 +LPC 186.89 1.407 0.9021 0.947 1.7538 0.9323 3.2631 0.9600 3662.6571 +HPC 204.54 22.365 0.8523 0.997 2.0721 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.998 0.9321 99.384 4.9982 1.4085 0.4249 0.9803 1.5311 +LPT 149.31 6.390 0.9263 101.662 6.3904 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5178.79 12295.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 830.00 199.13 29.795 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 830.00 199.13 29.795 +Duct1 0.0025 0.4616 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 830.00 199.13 29.795 +Duct2 0.0025 0.4445 365.99 +Duct3 0.0050 0.2964 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3637 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.2235 1135.71 275.00 99.874 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.0656 1135.71 275.00 99.874 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 503.06 120.21 7.670 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3042 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7157.6 11161.5 15210.9 +LP_Shaft 3416.6 28934.5 18822.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2212.49 0.9940 0.0550 1.42236 0.01697 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.201 0.9973 1.0000 0.9975 2706.36 1.000 1001.4 16724.6 +Core_Nozz 2.048 0.9998 1.0000 0.9999 862.88 1.000 1536.2 4741.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:54 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 318 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 35000.0 0.00 563.64 8151.9 0.5541 4516.54 5.5106 681.31 19.177 2126.8 2073.5 1646.2 + core size:20.20 Q: 170.94 Maximum Thrust: 10189.8 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 563.64 4.797 432.58 103.34 0.0000 1576.97 3.458 393.85 5027.3 0.7000 1.40133 +FS_2 Inlet.Fl_O 563.64 4.773 432.58 103.34 0.0000 1584.91 3.942 409.53 5943.4 0.5296 1.40133 +FS_21 Fan.Fl_O 563.64 7.450 497.75 118.94 0.0000 1089.18 6.440 477.43 4515.2 0.4607 1.40085 +FS_13 Splitter.Fl_O2 477.07 7.450 497.75 118.94 0.0000 921.89 6.423 477.07 3795.6 0.4649 1.40085 +FS_22 Splitter.Fl_O1 86.57 7.450 497.75 118.94 0.0000 167.29 6.525 479.22 719.5 0.4391 1.40085 +FS_23 Duct1.Fl_O 86.57 7.432 497.75 118.94 0.0000 167.71 6.509 479.22 721.3 0.4391 1.40085 +FS_24 LPC.Fl_O 86.57 16.757 648.46 155.13 0.0000 84.89 14.688 624.57 366.0 0.4383 1.39787 +FS_25 Duct2.Fl_O 86.57 16.715 648.46 155.13 0.0000 85.11 14.651 624.57 366.9 0.4383 1.39787 +FS_3 HPC.Fl_O 86.57 91.989 1106.77 267.70 0.0000 20.20 86.420 1088.10 119.9 0.3026 1.37402 +FS_36 Bld3.Fl_O 78.78 91.989 1106.77 267.70 0.0000 18.39 86.420 1088.10 109.1 0.3026 1.37402 +FS_4 Burner.Fl_O 80.04 86.930 2126.83 550.29 0.0159 27.40 86.369 2123.56 483.4 0.0993 1.31265 +FS_45 HPT.Fl_O 87.83 32.054 1646.24 414.26 0.0145 71.74 30.235 1622.36 439.1 0.2970 1.33275 +FS_48 Duct3.Fl_O 87.83 31.894 1646.24 414.26 0.0145 72.10 30.084 1622.36 441.4 0.2970 1.33275 +FS_5 LPT.Fl_O 87.83 6.565 1136.32 278.44 0.0145 291.02 6.005 1109.66 1477.4 0.3636 1.36223 +FS_7 Duct4.Fl_O 87.83 6.499 1136.32 278.44 0.0145 293.96 6.211 1122.67 2018.9 0.2588 1.36223 +FS_9 Core_Nozz.Fl_O 87.83 6.499 1136.32 278.44 0.0145 293.96 3.463 959.12 862.9 1.0000 1.36223 +FS_15 BypBld.Fl_O 477.07 7.450 497.75 118.94 0.0000 921.89 6.423 477.07 3795.6 0.4649 1.40085 +FS_17 Duct5.Fl_O 477.07 7.394 497.75 118.94 0.0000 928.85 6.375 477.07 3824.3 0.4649 1.40085 +FS_19 Byp_Nozz.Fl_O 477.07 7.394 497.75 118.94 0.0000 928.85 3.904 414.57 2706.4 1.0000 1.40085 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1584.91 1.561 0.9024 3612.284 1.1507 0.9084 -12443.7 31.73 18.34 +LPC 167.71 2.255 0.8631 3367.503 1.3028 0.8778 -4433.4 28.08 20.50 +HPC 85.11 5.503 0.8648 6313.671 1.7068 0.8922 -13788.2 22.09 22.16 +HPT 27.40 2.712 0.9144 153.078 1.2446 0.9042 13788.1 +LPT 72.10 4.858 0.9255 81.306 1.4487 0.9096 16877.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3038.87 1.390 0.9323 0.916 2.0961 0.5215 1.4369 0.9679 3943.9586 +LPC 179.89 1.385 0.8991 0.919 1.7166 0.9323 3.2631 0.9600 3662.6571 +HPC 202.33 21.818 0.8531 0.993 2.0966 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 5.029 0.9328 99.978 5.0292 1.4085 0.4249 0.9803 1.5311 +LPT 149.81 6.382 0.9243 100.240 6.3825 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5027.31 11935.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 811.15 194.53 27.743 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 811.15 194.53 27.743 +Duct1 0.0025 0.4391 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 811.15 194.53 27.743 +Duct2 0.0025 0.4383 365.99 +Duct3 0.0050 0.2970 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.0301 1106.77 267.70 91.989 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.7615 1106.77 267.70 91.989 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 497.75 118.94 7.450 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5106 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7059.6 10257.9 13788.1 +LP_Shaft 3298.9 26869.9 16877.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2126.83 0.9940 0.0550 1.25459 0.01592 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.138 0.9974 1.0000 0.9975 2706.36 1.000 996.1 15978.4 +Core_Nozz 1.879 0.9999 1.0000 0.9999 862.88 1.000 1503.6 4109.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:54 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 319 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 35000.0 0.00 525.49 6113.9 0.5588 3416.26 5.9887 681.31 15.938 1953.3 1905.6 1505.2 + core size:20.54 Q: 170.94 Maximum Thrust: 10189.8 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 525.49 4.797 432.58 103.34 0.0000 1470.23 3.458 393.85 4687.0 0.7000 1.40133 +FS_2 Inlet.Fl_O 525.49 4.773 432.58 103.34 0.0000 1477.63 4.077 413.48 5943.4 0.4797 1.40133 +FS_21 Fan.Fl_O 525.49 6.952 486.60 116.27 0.0000 1075.89 6.037 467.34 4515.2 0.4533 1.40101 +FS_13 Splitter.Fl_O2 450.30 6.952 486.60 116.27 0.0000 921.94 5.994 466.38 3795.6 0.4650 1.40101 +FS_22 Splitter.Fl_O1 75.19 6.952 486.60 116.27 0.0000 153.95 6.241 471.79 719.5 0.3957 1.40101 +FS_23 Duct1.Fl_O 75.19 6.935 486.60 116.27 0.0000 154.33 6.225 471.79 721.3 0.3957 1.40101 +FS_24 LPC.Fl_O 75.19 14.714 623.06 149.02 0.0000 82.31 13.023 601.76 366.0 0.4213 1.39860 +FS_25 Duct2.Fl_O 75.19 14.677 623.06 149.02 0.0000 82.52 12.991 601.76 366.9 0.4213 1.39860 +FS_3 HPC.Fl_O 75.19 76.452 1047.22 252.76 0.0000 20.54 71.658 1028.77 119.9 0.3078 1.37776 +FS_36 Bld3.Fl_O 68.42 76.452 1047.22 252.76 0.0000 18.69 71.658 1028.77 109.1 0.3078 1.37776 +FS_4 Burner.Fl_O 69.37 72.248 1953.30 499.56 0.0139 27.38 71.782 1950.24 483.4 0.0989 1.31996 +FS_45 HPT.Fl_O 76.14 26.470 1505.24 375.18 0.0126 72.02 24.956 1482.82 439.1 0.2973 1.34115 +FS_48 Duct3.Fl_O 76.14 26.337 1505.24 375.18 0.0126 72.38 24.831 1482.82 441.4 0.2973 1.34115 +FS_5 LPT.Fl_O 76.14 5.556 1040.64 253.57 0.0126 285.25 5.104 1017.01 1477.4 0.3541 1.36962 +FS_7 Duct4.Fl_O 76.14 5.501 1040.64 253.57 0.0126 288.13 5.267 1028.50 2018.9 0.2526 1.36962 +FS_9 Core_Nozz.Fl_O 76.14 5.501 1040.64 253.57 0.0126 288.13 3.458 917.13 862.9 0.8479 1.36962 +FS_15 BypBld.Fl_O 450.30 6.952 486.60 116.27 0.0000 921.94 5.994 466.38 3795.6 0.4650 1.40101 +FS_17 Duct5.Fl_O 450.30 6.900 486.60 116.27 0.0000 928.91 5.949 466.38 3824.3 0.4650 1.40101 +FS_19 Byp_Nozz.Fl_O 450.30 6.900 486.60 116.27 0.0000 928.91 3.644 405.28 2706.4 1.0000 1.40101 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1477.63 1.457 0.9105 3359.081 1.1249 0.9151 -9616.0 39.78 19.80 +LPC 154.33 2.122 0.8550 3167.126 1.2804 0.8694 -3484.3 25.58 16.83 +HPC 82.52 5.209 0.8657 6258.092 1.6808 0.8923 -11036.3 26.04 26.19 +HPT 27.38 2.729 0.9148 155.195 1.2518 0.9045 11036.3 +LPT 72.38 4.740 0.9211 79.069 1.4464 0.9043 13100.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2833.13 1.318 0.9406 0.852 2.0421 0.5215 1.4369 0.9679 3943.9586 +LPC 165.54 1.344 0.8906 0.865 1.6311 0.9323 3.2631 0.9600 3662.6571 +HPC 196.18 20.458 0.8541 0.984 2.1343 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.070 0.9332 101.361 5.0704 1.4085 0.4249 0.9803 1.5311 +LPT 150.39 6.217 0.9199 97.482 6.2171 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4687.04 11127.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 773.32 185.33 23.727 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 773.32 185.33 23.727 +Duct1 0.0025 0.3957 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 773.32 185.33 23.727 +Duct2 0.0025 0.4213 365.99 +Duct3 0.0050 0.2973 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3541 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.6317 1047.22 252.76 76.452 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.1356 1047.22 252.76 76.452 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 486.60 116.27 6.952 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9887 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6859.0 8450.8 11036.3 +LP_Shaft 3067.7 22429.0 13100.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1953.30 0.9940 0.0550 0.94896 0.01387 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.996 0.9976 1.0000 0.9975 2706.36 1.000 984.8 14287.3 +Core_Nozz 1.591 0.9999 1.0000 0.9999 862.88 0.848 1248.4 2954.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:54 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 320 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 35000.0 0.00 480.89 4076.1 0.5886 2399.28 6.7050 681.31 12.540 1760.2 1718.6 1348.9 + core size:20.91 Q: 170.94 Maximum Thrust: 10189.8 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 480.89 4.797 432.58 103.34 0.0000 1345.45 3.458 393.85 4289.2 0.7000 1.40133 +FS_2 Inlet.Fl_O 480.89 4.773 432.58 103.34 0.0000 1352.22 4.210 417.30 5943.4 0.4271 1.40133 +FS_21 Fan.Fl_O 480.89 6.380 473.78 113.20 0.0000 1058.74 5.572 455.76 4515.2 0.4439 1.40116 +FS_13 Splitter.Fl_O2 418.48 6.380 473.78 113.20 0.0000 921.33 5.502 454.12 3795.6 0.4645 1.40116 +FS_22 Splitter.Fl_O1 62.41 6.380 473.78 113.20 0.0000 137.41 5.873 462.70 719.5 0.3456 1.40116 +FS_23 Duct1.Fl_O 62.41 6.364 473.78 113.20 0.0000 137.75 5.859 462.70 721.3 0.3456 1.40116 +FS_24 LPC.Fl_O 62.41 12.296 589.93 141.05 0.0000 79.56 10.990 571.33 366.0 0.4037 1.39920 +FS_25 Duct2.Fl_O 62.41 12.265 589.93 141.05 0.0000 79.76 10.963 571.33 366.9 0.4037 1.39920 +FS_3 HPC.Fl_O 62.41 60.156 975.87 234.99 0.0000 20.91 56.234 957.82 119.9 0.3137 1.38221 +FS_36 Bld3.Fl_O 56.80 60.156 975.87 234.99 0.0000 19.03 56.234 957.82 109.1 0.3137 1.38221 +FS_4 Burner.Fl_O 57.46 56.848 1760.24 444.46 0.0117 27.37 56.482 1757.43 483.4 0.0985 1.32935 +FS_45 HPT.Fl_O 63.08 20.632 1348.89 332.86 0.0107 72.46 19.437 1328.10 439.1 0.2982 1.35140 +FS_48 Duct3.Fl_O 63.08 20.529 1348.89 332.86 0.0107 72.82 19.339 1328.10 441.4 0.2982 1.35140 +FS_5 LPT.Fl_O 63.08 4.761 948.95 230.10 0.0107 263.37 4.436 930.71 1477.4 0.3222 1.37675 +FS_7 Duct4.Fl_O 63.08 4.713 948.95 230.10 0.0107 266.03 4.544 939.47 2018.9 0.2312 1.37675 +FS_9 Core_Nozz.Fl_O 63.08 4.713 948.95 230.10 0.0107 266.03 3.458 871.54 862.8 0.6838 1.37675 +FS_15 BypBld.Fl_O 418.48 6.380 473.78 113.20 0.0000 921.33 5.502 454.12 3795.6 0.4645 1.40116 +FS_17 Duct5.Fl_O 418.48 6.332 473.78 113.20 0.0000 928.29 5.461 454.12 3824.3 0.4645 1.40116 +FS_19 Byp_Nozz.Fl_O 418.48 6.332 473.78 113.20 0.0000 928.29 3.458 398.41 2706.3 0.9710 1.40116 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1352.22 1.337 0.9095 3024.445 1.0953 0.9132 -6711.2 47.72 21.61 +LPC 137.75 1.932 0.8453 2889.934 1.2451 0.8589 -2459.8 23.80 13.54 +HPC 79.76 4.905 0.8648 6209.779 1.6542 0.8908 -8295.4 30.54 30.76 +HPT 27.37 2.755 0.9153 157.850 1.2609 0.9046 8295.4 +LPT 72.82 4.312 0.9173 75.204 1.4215 0.9005 9171.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2592.71 1.234 0.9396 0.767 2.0840 0.5215 1.4369 0.9679 3943.9586 +LPC 147.76 1.286 0.8805 0.789 1.5644 0.9323 3.2631 0.9600 3662.6571 +HPC 189.61 19.050 0.8532 0.977 2.1669 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.131 0.9337 103.095 5.1314 1.4085 0.4249 0.9803 1.5311 +LPT 151.32 5.620 0.9161 92.718 5.6199 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4289.24 10183.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 726.32 173.93 19.281 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 726.32 173.93 19.281 +Duct1 0.0025 0.3456 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 726.32 173.93 19.281 +Duct2 0.0025 0.4037 365.99 +Duct3 0.0050 0.2982 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3222 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.1845 975.87 234.99 60.156 +Duct5 0.0075 0.4645 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.4327 975.87 234.99 60.156 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 473.78 113.20 6.380 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.7050 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6622.6 6578.7 8295.4 +LP_Shaft 2762.1 17439.4 9171.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1760.24 0.9940 0.0550 0.66647 0.01173 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.831 0.9975 1.0000 0.9975 2706.36 0.971 948.1 12332.3 +Core_Nozz 1.363 0.9999 1.0000 0.9999 862.88 0.684 982.9 1927.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:54 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 321 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 35000.0 0.00 424.77 2037.9 0.7037 1434.14 7.8614 681.31 8.908 1510.5 1476.6 1148.9 + core size:21.49 Q: 170.94 Maximum Thrust: 10189.8 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 424.77 4.797 432.58 103.34 0.0000 1188.41 3.458 393.85 3788.6 0.7000 1.40133 +FS_2 Inlet.Fl_O 424.77 4.773 432.58 103.34 0.0000 1194.40 4.349 421.20 5943.4 0.3669 1.40133 +FS_21 Fan.Fl_O 424.77 5.730 458.71 109.59 0.0000 1024.53 5.058 442.62 4515.2 0.4256 1.40128 +FS_13 Splitter.Fl_O2 376.83 5.730 458.71 109.59 0.0000 908.92 4.967 440.32 3795.6 0.4563 1.40128 +FS_22 Splitter.Fl_O1 47.93 5.730 458.71 109.59 0.0000 115.62 5.417 451.40 719.5 0.2842 1.40128 +FS_23 Duct1.Fl_O 47.93 5.716 458.71 109.59 0.0000 115.91 5.403 451.40 721.3 0.2842 1.40128 +FS_24 LPC.Fl_O 47.93 9.568 546.15 130.54 0.0000 75.55 8.665 530.89 366.0 0.3790 1.39998 +FS_25 Duct2.Fl_O 47.93 9.544 546.15 130.54 0.0000 75.74 8.643 530.89 366.9 0.3790 1.39998 +FS_3 HPC.Fl_O 47.93 42.733 881.22 211.66 0.0000 21.49 39.779 863.74 119.9 0.3227 1.38794 +FS_36 Bld3.Fl_O 43.62 42.733 881.22 211.66 0.0000 19.55 39.779 863.74 109.1 0.3227 1.38794 +FS_4 Burner.Fl_O 44.02 40.382 1510.47 375.32 0.0091 27.34 40.123 1507.99 483.4 0.0979 1.34327 +FS_45 HPT.Fl_O 48.33 14.482 1148.86 280.26 0.0083 73.00 13.630 1130.34 439.1 0.2990 1.36556 +FS_48 Duct3.Fl_O 48.33 14.409 1148.86 280.26 0.0083 73.36 13.562 1130.34 441.4 0.2990 1.36556 +FS_5 LPT.Fl_O 48.33 4.146 847.38 204.50 0.0083 218.97 3.955 836.36 1477.4 0.2617 1.38434 +FS_7 Duct4.Fl_O 48.33 4.105 847.38 204.50 0.0083 221.18 4.004 841.55 2018.9 0.1898 1.38434 +FS_9 Core_Nozz.Fl_O 48.33 4.105 847.38 204.50 0.0083 221.18 3.458 807.90 862.9 0.5035 1.38434 +FS_15 BypBld.Fl_O 376.83 5.730 458.71 109.59 0.0000 908.92 4.967 440.32 3795.6 0.4563 1.40128 +FS_17 Duct5.Fl_O 376.83 5.687 458.71 109.59 0.0000 915.78 4.930 440.32 3824.3 0.4563 1.40128 +FS_19 Byp_Nozz.Fl_O 376.83 5.687 458.71 109.59 0.0000 915.78 3.458 397.79 2706.4 0.8737 1.40128 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1194.40 1.200 0.8891 2557.003 1.0604 0.8920 -3759.9 57.82 23.55 +LPC 115.91 1.674 0.8334 2483.088 1.1906 0.8451 -1420.8 24.84 10.34 +HPC 75.74 4.477 0.8630 6134.869 1.6135 0.8880 -5501.5 37.59 38.11 +HPT 27.34 2.788 0.9163 161.979 1.2738 0.9051 5501.5 +LPT 73.36 3.475 0.9101 68.895 1.3558 0.8948 5180.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2290.09 1.140 0.9185 0.648 2.2527 0.5215 1.4369 0.9679 3943.9586 +LPC 124.33 1.207 0.8681 0.678 1.5389 0.9323 3.2631 0.9600 3662.6571 +HPC 180.05 17.075 0.8514 0.965 2.2380 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.209 0.9347 105.791 5.2094 1.4085 0.4249 0.9803 1.5311 +LPT 152.44 4.453 0.9090 84.938 4.4530 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3788.61 8994.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 664.23 158.93 14.406 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 664.23 158.93 14.406 +Duct1 0.0025 0.2842 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 664.23 158.93 14.406 +Duct2 0.0025 0.3790 365.99 +Duct3 0.0050 0.2990 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2617 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.6777 881.22 211.66 42.733 +Duct5 0.0075 0.4563 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.6364 881.22 211.66 42.733 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 458.71 109.59 5.730 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8614 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6295.3 4589.9 5501.5 +LP_Shaft 2335.2 11652.2 5180.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1510.47 0.9940 0.0550 0.39837 0.00913 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.645 0.9975 1.0000 0.9975 2706.36 0.874 852.4 9984.0 +Core_Nozz 1.187 0.9999 1.0000 0.9999 862.88 0.504 698.1 1048.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:54 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 322 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 11/ 21/ 1/ 9 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 35000.0 0.00 368.11 509.5 1.4091 717.91 9.6198 681.31 5.797 1225.4 1200.8 925.2 + core size:22.39 Q: 170.94 Maximum Thrust: 10189.8 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 368.11 4.797 432.58 103.34 0.0000 1029.89 3.458 393.85 3283.3 0.7000 1.40133 +FS_2 Inlet.Fl_O 368.11 4.773 432.58 103.34 0.0000 1035.08 4.463 424.34 5943.4 0.3110 1.40133 +FS_21 Fan.Fl_O 368.11 5.173 445.35 106.39 0.0000 969.03 4.640 431.68 4515.2 0.3971 1.40133 +FS_13 Splitter.Fl_O2 333.44 5.173 445.35 106.39 0.0000 877.79 4.539 428.98 3795.6 0.4361 1.40133 +FS_22 Splitter.Fl_O1 34.66 5.173 445.35 106.39 0.0000 91.25 5.001 441.06 719.5 0.2201 1.40133 +FS_23 Duct1.Fl_O 34.66 5.160 445.35 106.39 0.0000 91.48 4.989 441.06 721.3 0.2201 1.40133 +FS_24 LPC.Fl_O 34.66 7.205 499.76 119.42 0.0000 69.40 6.642 488.26 366.0 0.3428 1.40082 +FS_25 Duct2.Fl_O 34.66 7.187 499.76 119.42 0.0000 69.58 6.625 488.26 366.9 0.3428 1.40082 +FS_3 HPC.Fl_O 34.66 27.806 774.77 185.68 0.0000 22.39 25.704 757.76 119.9 0.3377 1.39317 +FS_36 Bld3.Fl_O 31.54 27.806 774.77 185.68 0.0000 20.38 25.704 757.76 109.1 0.3377 1.39317 +FS_4 Burner.Fl_O 31.74 26.277 1225.44 299.45 0.0063 27.29 26.109 1223.35 483.4 0.0971 1.36207 +FS_45 HPT.Fl_O 34.86 9.324 925.23 223.39 0.0058 73.39 8.769 909.69 439.1 0.2990 1.38146 +FS_48 Duct3.Fl_O 34.86 9.277 925.23 223.39 0.0058 73.76 8.726 909.69 441.4 0.2990 1.38146 +FS_5 LPT.Fl_O 34.86 3.788 741.26 178.16 0.0058 161.70 3.695 736.11 1477.4 0.1892 1.39109 +FS_7 Duct4.Fl_O 34.86 3.750 741.26 178.16 0.0058 163.33 3.700 738.49 2018.9 0.1384 1.39109 +FS_9 Core_Nozz.Fl_O 34.86 3.750 741.26 178.16 0.0058 163.33 3.458 724.55 862.8 0.3433 1.39109 +FS_15 BypBld.Fl_O 333.44 5.173 445.35 106.39 0.0000 877.79 4.539 428.98 3795.6 0.4361 1.40133 +FS_17 Duct5.Fl_O 333.44 5.134 445.35 106.39 0.0000 884.42 4.505 428.98 3824.3 0.4361 1.40133 +FS_19 Byp_Nozz.Fl_O 333.44 5.134 445.35 106.39 0.0000 884.42 3.458 397.67 2706.4 0.7730 1.40133 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1035.08 1.084 0.7896 1986.816 1.0295 0.7921 -1592.1 83.25 24.31 +LPC 91.48 1.396 0.8207 1958.120 1.1222 0.8290 -639.0 31.01 8.63 +HPC 69.58 3.869 0.8541 6021.979 1.5503 0.8786 -3249.5 49.42 50.41 +HPT 27.29 2.818 0.9179 168.861 1.2895 0.9063 3249.5 +LPT 73.76 2.449 0.8999 59.651 1.2482 0.8879 2231.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1984.62 1.058 0.8158 0.504 2.6194 0.5215 1.4369 0.9679 3943.9586 +LPC 98.12 1.121 0.8549 0.535 1.6020 0.9323 3.2631 0.9600 3662.6571 +HPC 165.41 14.263 0.8426 0.947 2.3785 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.279 0.9363 110.286 5.2795 1.4085 0.4249 0.9803 1.5311 +LPT 153.26 3.022 0.8987 73.543 3.0216 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3283.26 7794.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 596.41 142.61 10.208 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 596.41 142.61 10.208 +Duct1 0.0025 0.2201 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 596.41 142.61 10.208 +Duct2 0.0025 0.3428 365.99 +Duct3 0.0050 0.2990 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1892 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.2132 774.77 185.68 27.806 +Duct5 0.0075 0.4361 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 1.9064 774.77 185.68 27.806 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 445.35 106.39 5.173 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.6198 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 5911.2 2887.2 3249.5 +LP_Shaft 1814.4 6458.1 2231.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1225.44 0.9940 0.0550 0.19942 0.00632 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.485 0.9975 1.0000 0.9975 2706.36 0.773 754.1 7815.1 +Core_Nozz 1.084 0.9999 1.0000 0.9999 862.88 0.343 451.6 489.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:54 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 323 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 35000.0 0.00 619.65 10406.8 0.5882 6121.19 5.0395 729.97 22.732 2325.0 2265.7 1811.9 + core size:19.95 Q: 196.23 Maximum Thrust: 10406.8 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 619.65 5.023 438.31 104.71 0.0000 1666.72 3.458 393.85 5158.3 0.7500 1.40134 +FS_2 Inlet.Fl_O 619.65 4.997 438.31 104.71 0.0000 1675.11 3.989 410.92 5943.4 0.5763 1.40134 +FS_21 Fan.Fl_O 619.65 8.218 515.63 123.22 0.0000 1104.77 7.065 493.80 4515.2 0.4696 1.40057 +FS_13 Splitter.Fl_O2 517.05 8.218 515.63 123.22 0.0000 921.84 7.086 494.21 3795.6 0.4650 1.40057 +FS_22 Splitter.Fl_O1 102.60 8.218 515.63 123.22 0.0000 182.92 6.952 491.51 719.5 0.4947 1.40057 +FS_23 Duct1.Fl_O 102.60 8.198 515.63 123.22 0.0000 183.38 6.934 491.51 721.3 0.4947 1.40057 +FS_24 LPC.Fl_O 102.60 20.391 691.83 165.59 0.0000 85.40 17.836 666.02 366.0 0.4419 1.39629 +FS_25 Duct2.Fl_O 102.60 20.340 691.83 165.59 0.0000 85.62 17.792 666.02 366.9 0.4419 1.39629 +FS_3 HPC.Fl_O 102.60 114.171 1184.18 287.29 0.0000 19.95 107.439 1164.91 119.9 0.2990 1.36914 +FS_36 Bld3.Fl_O 93.36 114.171 1184.18 287.29 0.0000 18.16 107.439 1164.91 109.1 0.2990 1.36914 +FS_4 Burner.Fl_O 95.07 107.892 2325.02 609.38 0.0182 27.42 107.196 2321.50 483.4 0.0996 1.30559 +FS_45 HPT.Fl_O 104.30 40.392 1811.88 461.15 0.0166 70.93 38.154 1786.76 439.1 0.2944 1.32379 +FS_48 Duct3.Fl_O 104.30 40.190 1811.88 461.15 0.0166 71.28 37.963 1786.76 441.4 0.2944 1.32379 +FS_5 LPT.Fl_O 104.30 8.212 1253.65 309.47 0.0166 290.17 7.516 1224.94 1477.4 0.3636 1.35336 +FS_7 Duct4.Fl_O 104.30 8.130 1253.65 309.47 0.0166 293.10 7.772 1238.95 2018.9 0.2589 1.35336 +FS_9 Core_Nozz.Fl_O 104.30 8.130 1253.65 309.47 0.0166 293.10 4.340 1061.89 862.9 1.0000 1.35336 +FS_15 BypBld.Fl_O 517.05 8.218 515.63 123.22 0.0000 921.84 7.086 494.21 3795.6 0.4650 1.40057 +FS_17 Duct5.Fl_O 517.05 8.157 515.63 123.22 0.0000 928.81 7.033 494.21 3824.3 0.4650 1.40057 +FS_19 Byp_Nozz.Fl_O 517.05 8.157 515.63 123.22 0.0000 928.81 4.307 429.47 2706.4 1.0000 1.40057 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.645 0.8675 3944.235 1.1764 0.8765 -16232.6 24.71 17.45 +LPC 183.38 2.487 0.8684 3636.515 1.3417 0.8841 -6150.6 28.43 23.33 +HPC 85.62 5.613 0.8651 6327.194 1.7117 0.8923 -17665.5 20.05 20.10 +HPT 27.42 2.671 0.9132 151.549 1.2351 0.9034 17665.7 +LPT 71.28 4.894 0.9321 85.181 1.4453 0.9176 22383.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8963 1.000 2.3707 0.5215 1.4369 0.9679 3943.9586 +LPC 196.70 1.456 0.9045 0.993 1.7677 0.9323 3.2631 0.9600 3662.6571 +HPC 203.53 22.326 0.8534 0.995 2.0424 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.933 0.9316 98.979 4.9332 1.4085 0.4249 0.9803 1.5311 +LPT 148.12 6.432 0.9309 105.017 6.4317 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5158.35 14058.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 867.04 208.19 34.086 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 867.04 208.19 34.086 +Duct1 0.0025 0.4947 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 867.04 208.19 34.086 +Duct2 0.0025 0.4419 365.99 +Duct3 0.0050 0.2944 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.5909 1184.18 287.29 114.171 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.6429 1184.18 287.29 114.171 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 515.63 123.22 8.218 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0395 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7307.4 12696.9 17665.7 +LP_Shaft 3625.8 32422.8 22383.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2325.02 0.9940 0.0550 1.70033 0.01821 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.359 0.9968 1.0000 0.9975 2706.36 1.000 1013.8 18590.6 +Core_Nozz 2.351 0.9986 1.0000 0.9999 862.88 1.000 1577.5 5874.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:54 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 324 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 35000.0 0.00 604.03 9365.7 0.5779 5412.75 5.3033 729.97 20.826 2240.4 2183.6 1739.5 + core size:20.05 Q: 196.23 Maximum Thrust: 10406.8 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 604.03 5.023 438.31 104.71 0.0000 1624.72 3.458 393.85 5028.4 0.7500 1.40134 +FS_2 Inlet.Fl_O 604.03 4.997 438.31 104.71 0.0000 1632.90 4.057 412.90 5943.4 0.5538 1.40134 +FS_21 Fan.Fl_O 604.03 8.032 509.75 121.81 0.0000 1095.70 6.927 488.62 4515.2 0.4644 1.40067 +FS_13 Splitter.Fl_O2 508.20 8.032 509.75 121.81 0.0000 921.87 6.925 488.57 3795.6 0.4650 1.40067 +FS_22 Splitter.Fl_O1 95.83 8.032 509.75 121.81 0.0000 173.83 6.939 488.86 719.5 0.4617 1.40067 +FS_23 Duct1.Fl_O 95.83 8.011 509.75 121.81 0.0000 174.27 6.922 488.86 721.3 0.4617 1.40067 +FS_24 LPC.Fl_O 95.83 18.657 670.31 160.40 0.0000 85.81 16.294 644.97 366.0 0.4445 1.39706 +FS_25 Duct2.Fl_O 95.83 18.611 670.31 160.40 0.0000 86.03 16.253 644.97 366.9 0.4445 1.39706 +FS_3 HPC.Fl_O 95.83 104.600 1150.08 278.64 0.0000 20.05 98.371 1131.10 119.9 0.3004 1.37129 +FS_36 Bld3.Fl_O 87.20 104.600 1150.08 278.64 0.0000 18.24 98.371 1131.10 109.1 0.3004 1.37129 +FS_4 Burner.Fl_O 88.71 98.847 2240.41 584.01 0.0172 27.41 98.210 2237.00 483.4 0.0995 1.30853 +FS_45 HPT.Fl_O 97.33 36.639 1739.49 440.54 0.0157 71.50 34.574 1714.74 439.1 0.2965 1.32758 +FS_48 Duct3.Fl_O 97.33 36.455 1739.49 440.54 0.0157 71.86 34.401 1714.74 441.4 0.2965 1.32758 +FS_5 LPT.Fl_O 97.33 7.502 1204.50 296.39 0.0157 290.55 6.865 1176.63 1477.4 0.3636 1.35707 +FS_7 Duct4.Fl_O 97.33 7.427 1204.50 296.39 0.0157 293.49 7.099 1190.23 2018.9 0.2589 1.35707 +FS_9 Core_Nozz.Fl_O 97.33 7.427 1204.50 296.39 0.0157 293.49 3.962 1018.75 862.9 1.0000 1.35707 +FS_15 BypBld.Fl_O 508.20 8.032 509.75 121.81 0.0000 921.87 6.925 488.57 3795.6 0.4650 1.40067 +FS_17 Duct5.Fl_O 508.20 7.971 509.75 121.81 0.0000 928.83 6.873 488.57 3824.3 0.4650 1.40067 +FS_19 Byp_Nozz.Fl_O 508.20 7.971 509.75 121.81 0.0000 928.83 4.209 424.57 2706.4 1.0000 1.40067 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1632.90 1.607 0.8926 3741.943 1.1630 0.8995 -14619.3 28.22 17.74 +LPC 174.27 2.329 0.8661 3469.846 1.3150 0.8810 -5231.6 28.95 22.22 +HPC 86.03 5.620 0.8639 6337.560 1.7157 0.8916 -16031.1 20.47 20.49 +HPT 27.41 2.698 0.9138 152.213 1.2401 0.9037 16031.2 +LPT 71.86 4.859 0.9276 82.476 1.4442 0.9121 19850.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3130.64 1.423 0.9221 0.949 2.1748 0.5215 1.4369 0.9679 3943.9586 +LPC 186.92 1.407 0.9021 0.947 1.7536 0.9323 3.2631 0.9600 3662.6571 +HPC 204.51 22.359 0.8523 0.997 2.0720 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.996 0.9321 99.413 4.9962 1.4085 0.4249 0.9803 1.5311 +LPT 149.30 6.384 0.9264 101.683 6.3837 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5028.38 13704.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 840.87 201.78 31.208 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 840.87 201.78 31.208 +Duct1 0.0025 0.4617 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 840.87 201.78 31.208 +Duct2 0.0025 0.4445 365.99 +Duct3 0.0050 0.2965 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.3540 1150.08 278.64 104.600 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.2706 1150.08 278.64 104.600 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 509.75 121.81 8.032 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3033 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7204.7 11686.5 16031.2 +LP_Shaft 3439.9 30308.2 19850.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2240.41 0.9940 0.0550 1.50354 0.01724 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.305 0.9970 1.0000 0.9975 2706.36 1.000 1008.0 17955.1 +Core_Nozz 2.148 0.9995 1.0000 0.9999 862.88 1.000 1547.0 5115.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:54 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 325 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 35000.0 0.00 586.43 8325.5 0.5736 4775.52 5.5090 729.97 19.186 2153.9 2099.9 1668.2 + core size:20.20 Q: 196.23 Maximum Thrust: 10406.8 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 586.43 5.023 438.31 104.71 0.0000 1577.36 3.458 393.85 4881.8 0.7500 1.40134 +FS_2 Inlet.Fl_O 586.43 4.997 438.31 104.71 0.0000 1585.30 4.127 414.94 5943.4 0.5297 1.40134 +FS_21 Fan.Fl_O 586.43 7.803 504.38 120.53 0.0000 1089.20 6.745 483.79 4515.2 0.4608 1.40075 +FS_13 Splitter.Fl_O2 496.33 7.803 504.38 120.53 0.0000 921.86 6.727 483.43 3795.6 0.4649 1.40075 +FS_22 Splitter.Fl_O1 90.09 7.803 504.38 120.53 0.0000 167.34 6.833 485.60 719.5 0.4393 1.40075 +FS_23 Duct1.Fl_O 90.09 7.783 504.38 120.53 0.0000 167.76 6.816 485.60 721.3 0.4393 1.40075 +FS_24 LPC.Fl_O 90.09 17.555 657.11 157.22 0.0000 84.89 15.387 632.91 366.0 0.4383 1.39756 +FS_25 Duct2.Fl_O 90.09 17.511 657.11 157.22 0.0000 85.11 15.348 632.91 366.9 0.4383 1.39756 +FS_3 HPC.Fl_O 90.09 96.363 1120.90 271.26 0.0000 20.20 90.532 1102.03 119.9 0.3027 1.37313 +FS_36 Bld3.Fl_O 81.99 96.363 1120.90 271.26 0.0000 18.38 90.532 1102.03 109.1 0.3027 1.37313 +FS_4 Burner.Fl_O 83.31 91.063 2153.90 558.25 0.0162 27.40 90.476 2150.59 483.4 0.0993 1.31166 +FS_45 HPT.Fl_O 91.42 33.589 1668.23 420.40 0.0147 71.73 31.683 1644.11 439.1 0.2972 1.33154 +FS_48 Duct3.Fl_O 91.42 33.421 1668.23 420.40 0.0147 72.09 31.525 1644.11 441.4 0.2972 1.33154 +FS_5 LPT.Fl_O 91.42 6.885 1152.83 282.76 0.0147 290.93 6.298 1125.88 1477.4 0.3636 1.36101 +FS_7 Duct4.Fl_O 91.42 6.816 1152.83 282.76 0.0147 293.87 6.514 1139.03 2018.9 0.2589 1.36101 +FS_9 Core_Nozz.Fl_O 91.42 6.816 1152.83 282.76 0.0147 293.87 3.633 973.53 862.9 1.0000 1.36101 +FS_15 BypBld.Fl_O 496.33 7.803 504.38 120.53 0.0000 921.86 6.727 483.43 3795.6 0.4649 1.40075 +FS_17 Duct5.Fl_O 496.33 7.744 504.38 120.53 0.0000 928.83 6.677 483.43 3824.3 0.4649 1.40075 +FS_19 Byp_Nozz.Fl_O 496.33 7.744 504.38 120.53 0.0000 928.83 4.089 420.10 2706.4 1.0000 1.40075 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1585.30 1.561 0.9024 3613.238 1.1508 0.9083 -13127.4 31.69 18.33 +LPC 167.76 2.256 0.8631 3368.256 1.3028 0.8778 -4676.7 28.07 20.51 +HPC 85.11 5.503 0.8648 6313.623 1.7058 0.8922 -14537.3 22.10 22.17 +HPT 27.40 2.711 0.9145 153.123 1.2439 0.9042 14537.2 +LPT 72.09 4.854 0.9256 81.323 1.4471 0.9097 17804.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3039.63 1.391 0.9322 0.916 2.0964 0.5215 1.4369 0.9679 3943.9586 +LPC 179.94 1.385 0.8991 0.920 1.7167 0.9323 3.2631 0.9600 3662.6571 +HPC 202.33 21.816 0.8531 0.993 2.0968 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 5.027 0.9328 100.007 5.0272 1.4085 0.4249 0.9803 1.5311 +LPT 149.81 6.377 0.9244 100.261 6.3767 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4881.80 13304.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 821.82 197.13 29.063 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 821.82 197.13 29.063 +Duct1 0.0025 0.4393 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 821.82 197.13 29.063 +Duct2 0.0025 0.4383 365.99 +Duct3 0.0050 0.2972 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.1533 1120.90 271.26 96.363 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.9552 1120.90 271.26 96.363 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 504.38 120.53 7.803 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5090 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7106.5 10743.9 14537.2 +LP_Shaft 3321.5 28152.7 17804.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2153.90 0.9940 0.0550 1.32653 0.01618 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.240 0.9972 1.0000 0.9975 2706.36 1.000 1002.7 17176.5 +Core_Nozz 1.971 0.9999 1.0000 0.9999 862.88 1.000 1514.2 4453.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:54 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 326 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 35000.0 0.00 547.62 6244.1 0.5786 3612.70 5.9848 729.97 15.973 1977.4 1929.2 1525.0 + core size:20.54 Q: 196.23 Maximum Thrust: 10406.8 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 547.62 5.023 438.31 104.71 0.0000 1473.00 3.458 393.85 4558.8 0.7500 1.40134 +FS_2 Inlet.Fl_O 547.62 4.997 438.31 104.71 0.0000 1480.41 4.265 418.86 5943.4 0.4810 1.40134 +FS_21 Fan.Fl_O 547.62 7.295 493.37 117.89 0.0000 1075.95 6.335 473.84 4515.2 0.4534 1.40092 +FS_13 Splitter.Fl_O2 469.22 7.295 493.37 117.89 0.0000 921.91 6.290 472.87 3795.6 0.4649 1.40092 +FS_22 Splitter.Fl_O1 78.40 7.295 493.37 117.89 0.0000 154.04 6.547 478.33 719.5 0.3960 1.40092 +FS_23 Duct1.Fl_O 78.40 7.277 493.37 117.89 0.0000 154.43 6.531 478.33 721.3 0.3960 1.40092 +FS_24 LPC.Fl_O 78.40 15.492 632.46 151.28 0.0000 82.13 13.722 610.96 366.0 0.4201 1.39836 +FS_25 Duct2.Fl_O 78.40 15.453 632.46 151.28 0.0000 82.33 13.687 610.96 366.9 0.4201 1.39836 +FS_3 HPC.Fl_O 78.40 80.225 1061.33 256.29 0.0000 20.54 75.190 1042.65 119.9 0.3080 1.37688 +FS_36 Bld3.Fl_O 71.35 80.225 1061.33 256.29 0.0000 18.70 75.190 1042.65 109.1 0.3080 1.37688 +FS_4 Burner.Fl_O 72.35 75.813 1977.41 506.49 0.0141 27.38 75.325 1974.32 483.4 0.0990 1.31894 +FS_45 HPT.Fl_O 79.41 27.793 1525.01 380.58 0.0128 72.00 26.204 1502.37 439.1 0.2974 1.33999 +FS_48 Duct3.Fl_O 79.41 27.654 1525.01 380.58 0.0128 72.36 26.073 1502.37 441.4 0.2974 1.33999 +FS_5 LPT.Fl_O 79.41 5.775 1052.77 256.69 0.0128 287.90 5.294 1028.39 1477.4 0.3581 1.36872 +FS_7 Duct4.Fl_O 79.41 5.717 1052.77 256.69 0.0128 290.81 5.469 1040.26 2018.9 0.2552 1.36872 +FS_9 Core_Nozz.Fl_O 79.41 5.717 1052.77 256.69 0.0128 290.81 3.458 918.25 862.9 0.8848 1.36872 +FS_15 BypBld.Fl_O 469.22 7.295 493.37 117.89 0.0000 921.91 6.290 472.87 3795.6 0.4649 1.40092 +FS_17 Duct5.Fl_O 469.22 7.240 493.37 117.89 0.0000 928.87 6.243 472.87 3824.3 0.4649 1.40092 +FS_19 Byp_Nozz.Fl_O 469.22 7.240 493.37 117.89 0.0000 928.87 3.823 410.93 2706.4 1.0000 1.40092 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1480.41 1.460 0.9105 3366.219 1.1256 0.9151 -10215.1 39.51 19.74 +LPC 154.43 2.129 0.8546 3172.806 1.2819 0.8691 -3703.9 25.33 16.69 +HPC 82.33 5.191 0.8658 6254.570 1.6781 0.8923 -11648.4 26.24 26.40 +HPT 27.38 2.728 0.9148 155.317 1.2509 0.9046 11648.5 +LPT 72.36 4.789 0.9209 79.241 1.4486 0.9040 13918.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2838.41 1.320 0.9406 0.854 2.0409 0.5215 1.4369 0.9679 3943.9586 +LPC 165.64 1.346 0.8902 0.866 1.6254 0.9323 3.2631 0.9600 3662.6571 +HPC 195.73 20.376 0.8541 0.984 2.1342 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.066 0.9332 101.441 5.0665 1.4085 0.4249 0.9803 1.5311 +LPT 150.35 6.285 0.9197 97.694 6.2852 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4558.80 12424.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 784.46 188.03 24.942 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 784.46 188.03 24.942 +Duct1 0.0025 0.3960 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 784.46 188.03 24.942 +Duct2 0.0025 0.4201 365.99 +Duct3 0.0050 0.2974 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3581 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.7441 1061.33 256.29 80.225 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.3122 1061.33 256.29 80.225 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 493.37 117.89 7.295 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9848 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6906.7 8858.0 11648.5 +LP_Shaft 3094.5 23623.7 13918.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1977.41 0.9940 0.0550 1.00353 0.01407 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.094 0.9975 1.0000 0.9975 2706.36 1.000 991.7 15451.7 +Core_Nozz 1.653 0.9999 1.0000 0.9999 862.88 0.885 1303.5 3217.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:54 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 327 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 35000.0 0.00 502.31 4162.8 0.6102 2540.20 6.6972 729.97 12.603 1782.0 1739.9 1366.8 + core size:20.93 Q: 196.23 Maximum Thrust: 10406.8 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 502.31 5.023 438.31 104.71 0.0000 1351.10 3.458 393.85 4181.6 0.7500 1.40134 +FS_2 Inlet.Fl_O 502.31 4.997 438.31 104.71 0.0000 1357.91 4.402 422.67 5943.4 0.4294 1.40134 +FS_21 Fan.Fl_O 502.31 6.706 480.64 114.84 0.0000 1059.64 5.855 462.32 4515.2 0.4444 1.40108 +FS_13 Splitter.Fl_O2 437.05 6.706 480.64 114.84 0.0000 921.97 5.782 460.66 3795.6 0.4650 1.40108 +FS_22 Splitter.Fl_O1 65.26 6.706 480.64 114.84 0.0000 137.67 6.172 469.34 719.5 0.3463 1.40108 +FS_23 Duct1.Fl_O 65.26 6.689 480.64 114.84 0.0000 138.01 6.156 469.34 721.3 0.3463 1.40108 +FS_24 LPC.Fl_O 65.26 13.016 599.93 143.46 0.0000 79.24 11.646 581.19 366.0 0.4018 1.39904 +FS_25 Duct2.Fl_O 65.26 12.983 599.93 143.46 0.0000 79.44 11.617 581.19 366.9 0.4018 1.39904 +FS_3 HPC.Fl_O 65.26 63.299 990.10 238.53 0.0000 20.93 59.164 971.79 119.9 0.3141 1.38133 +FS_36 Bld3.Fl_O 59.39 63.299 990.10 238.53 0.0000 19.05 59.164 971.79 109.1 0.3141 1.38133 +FS_4 Burner.Fl_O 60.09 59.818 1781.99 450.55 0.0119 27.36 59.433 1779.15 483.4 0.0986 1.32829 +FS_45 HPT.Fl_O 65.96 21.731 1366.78 337.62 0.0108 72.42 20.474 1345.79 439.1 0.2981 1.35023 +FS_48 Duct3.Fl_O 65.96 21.622 1366.78 337.62 0.0108 72.78 20.371 1345.79 441.4 0.2981 1.35023 +FS_5 LPT.Fl_O 65.96 4.896 957.03 232.15 0.0108 268.98 4.545 937.77 1477.4 0.3301 1.37615 +FS_7 Duct4.Fl_O 65.96 4.847 957.03 232.15 0.0108 271.69 4.664 947.05 2018.9 0.2366 1.37615 +FS_9 Core_Nozz.Fl_O 65.96 4.847 957.03 232.15 0.0108 271.69 3.458 872.30 862.9 0.7154 1.37615 +FS_15 BypBld.Fl_O 437.05 6.706 480.64 114.84 0.0000 921.97 5.782 460.66 3795.6 0.4650 1.40108 +FS_17 Duct5.Fl_O 437.05 6.656 480.64 114.84 0.0000 928.94 5.738 460.66 3824.3 0.4650 1.40108 +FS_19 Byp_Nozz.Fl_O 437.05 6.656 480.64 114.84 0.0000 928.94 3.515 400.31 2706.3 1.0000 1.40108 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1357.91 1.342 0.9097 3040.085 1.0966 0.9134 -7201.7 47.38 21.53 +LPC 138.01 1.946 0.8445 2903.131 1.2482 0.8583 -2642.2 23.25 13.30 +HPC 79.44 4.875 0.8648 6204.807 1.6504 0.8907 -8778.0 30.93 31.16 +HPT 27.36 2.753 0.9154 158.081 1.2599 0.9046 8778.0 +LPT 72.78 4.417 0.9165 75.593 1.4282 0.8994 9844.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2603.60 1.238 0.9399 0.771 2.0805 0.5215 1.4369 0.9679 3943.9586 +LPC 148.03 1.290 0.8796 0.793 1.5527 0.9323 3.2631 0.9600 3662.6571 +HPC 188.86 18.915 0.8531 0.976 2.1667 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.125 0.9337 103.245 5.1251 1.4085 0.4249 0.9803 1.5311 +LPT 151.23 5.766 0.9154 93.196 5.7661 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4181.55 11396.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 737.88 176.73 20.355 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 737.88 176.73 20.355 +Duct1 0.0025 0.3463 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 737.88 176.73 20.355 +Duct2 0.0025 0.4018 365.99 +Duct3 0.0050 0.2981 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3301 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.2841 990.10 238.53 63.299 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.5892 990.10 238.53 63.299 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 480.64 114.84 6.706 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6972 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6673.2 6908.7 8778.0 +LP_Shaft 2794.7 18500.3 9844.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1781.99 0.9940 0.0550 0.70561 0.01188 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.925 0.9975 1.0000 0.9975 2706.36 1.000 978.8 13450.2 +Core_Nozz 1.402 0.9999 1.0000 0.9999 862.88 0.715 1028.7 2109.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:54 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 328 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 35000.0 0.00 447.05 2081.5 0.7310 1521.57 7.8827 729.97 8.992 1529.9 1495.8 1164.8 + core size:21.52 Q: 196.23 Maximum Thrust: 10406.8 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 447.05 5.023 438.31 104.71 0.0000 1202.47 3.458 393.85 3721.5 0.7500 1.40134 +FS_2 Inlet.Fl_O 447.05 4.997 438.31 104.71 0.0000 1208.52 4.541 426.46 5943.4 0.3721 1.40134 +FS_21 Fan.Fl_O 447.05 6.024 465.43 111.20 0.0000 1033.16 5.304 448.77 4515.2 0.4302 1.40124 +FS_13 Splitter.Fl_O2 396.72 6.024 465.43 111.20 0.0000 916.85 5.205 446.35 3795.6 0.4615 1.40124 +FS_22 Splitter.Fl_O1 50.33 6.024 465.43 111.20 0.0000 116.31 5.691 457.91 719.5 0.2861 1.40124 +FS_23 Duct1.Fl_O 50.33 6.009 465.43 111.20 0.0000 116.60 5.676 457.91 721.3 0.2861 1.40124 +FS_24 LPC.Fl_O 50.33 10.199 556.84 133.11 0.0000 75.14 9.248 541.48 366.0 0.3766 1.39977 +FS_25 Duct2.Fl_O 50.33 10.173 556.84 133.11 0.0000 75.33 9.225 541.48 366.9 0.3766 1.39977 +FS_3 HPC.Fl_O 50.33 45.162 895.79 215.24 0.0000 21.52 42.030 877.98 119.9 0.3234 1.38710 +FS_36 Bld3.Fl_O 45.80 45.162 895.79 215.24 0.0000 19.59 42.030 877.98 109.1 0.3234 1.38710 +FS_4 Burner.Fl_O 46.22 42.678 1529.88 380.57 0.0092 27.33 42.405 1527.37 483.4 0.0979 1.34219 +FS_45 HPT.Fl_O 50.75 15.324 1164.79 284.36 0.0084 72.94 14.424 1146.09 439.1 0.2989 1.36449 +FS_48 Duct3.Fl_O 50.75 15.247 1164.79 284.36 0.0084 73.30 14.352 1146.09 441.4 0.2989 1.36449 +FS_5 LPT.Fl_O 50.75 4.218 851.15 205.44 0.0084 226.51 4.009 839.25 1477.4 0.2716 1.38409 +FS_7 Duct4.Fl_O 50.75 4.176 851.15 205.44 0.0084 228.80 4.066 844.87 2018.9 0.1967 1.38409 +FS_9 Core_Nozz.Fl_O 50.75 4.176 851.15 205.44 0.0084 228.80 3.458 807.65 862.8 0.5287 1.38409 +FS_15 BypBld.Fl_O 396.72 6.024 465.43 111.20 0.0000 916.85 5.205 446.35 3795.6 0.4615 1.40124 +FS_17 Duct5.Fl_O 396.72 5.979 465.43 111.20 0.0000 923.78 5.166 446.35 3824.3 0.4615 1.40124 +FS_19 Byp_Nozz.Fl_O 396.72 5.979 465.43 111.20 0.0000 923.78 3.458 397.87 2706.3 0.9199 1.40124 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1208.52 1.205 0.8878 2589.663 1.0619 0.8908 -4107.0 57.76 23.91 +LPC 116.60 1.697 0.8320 2513.066 1.1964 0.8441 -1560.0 23.62 10.00 +HPC 75.33 4.439 0.8629 6127.213 1.6087 0.8878 -5848.1 38.18 38.73 +HPT 27.33 2.785 0.9163 162.313 1.2728 0.9051 5848.3 +LPT 73.30 3.615 0.9109 69.753 1.3685 0.8952 5666.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2317.17 1.143 0.9172 0.657 2.2586 0.5215 1.4369 0.9679 3943.9586 +LPC 125.07 1.214 0.8666 0.686 1.5157 0.9323 3.2631 0.9600 3662.6571 +HPC 179.09 16.899 0.8512 0.964 2.2439 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.202 0.9347 106.010 5.2015 1.4085 0.4249 0.9803 1.5311 +LPT 152.32 4.648 0.9097 85.997 4.6476 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3721.53 10142.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 676.34 161.85 15.299 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 676.34 161.85 15.299 +Duct1 0.0025 0.2861 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 676.34 161.85 15.299 +Duct2 0.0025 0.3766 365.99 +Duct3 0.0050 0.2989 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2716 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.7615 895.79 215.24 45.162 +Duct5 0.0075 0.4615 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.7680 895.79 215.24 45.162 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 465.43 111.20 6.024 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8827 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6348.7 4838.1 5848.3 +LP_Shaft 2380.6 12502.4 5666.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1529.88 0.9940 0.0550 0.42266 0.00923 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.729 0.9975 1.0000 0.9975 2706.36 0.920 897.6 11068.3 +Core_Nozz 1.208 0.9999 1.0000 0.9999 862.88 0.529 732.8 1155.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:54 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 329 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 10/ 20/ 1/ 8 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 35000.0 0.00 391.47 520.3 1.4780 769.08 9.6963 729.97 5.895 1246.0 1221.0 941.6 + core size:22.42 Q: 196.23 Maximum Thrust: 10406.8 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 391.47 5.023 438.31 104.71 0.0000 1052.98 3.458 393.85 3258.9 0.7500 1.40134 +FS_2 Inlet.Fl_O 391.47 4.997 438.31 104.71 0.0000 1058.29 4.657 429.54 5943.4 0.3189 1.40134 +FS_21 Fan.Fl_O 391.47 5.435 451.89 107.96 0.0000 988.02 4.849 437.37 4515.2 0.4067 1.40132 +FS_13 Splitter.Fl_O2 354.88 5.435 451.89 107.96 0.0000 895.65 4.736 434.42 3795.6 0.4476 1.40132 +FS_22 Splitter.Fl_O1 36.60 5.435 451.89 107.96 0.0000 92.37 5.250 447.43 719.5 0.2229 1.40132 +FS_23 Duct1.Fl_O 36.60 5.421 451.89 107.96 0.0000 92.60 5.237 447.43 721.3 0.2229 1.40132 +FS_24 LPC.Fl_O 36.60 7.718 510.57 122.01 0.0000 69.14 7.120 498.92 366.0 0.3413 1.40065 +FS_25 Duct2.Fl_O 36.60 7.699 510.57 122.01 0.0000 69.31 7.102 498.92 366.9 0.3413 1.40065 +FS_3 HPC.Fl_O 36.60 29.609 789.98 189.38 0.0000 22.42 27.365 772.61 119.9 0.3383 1.39243 +FS_36 Bld3.Fl_O 33.31 29.609 789.98 189.38 0.0000 20.40 27.365 772.61 109.1 0.3383 1.39243 +FS_4 Burner.Fl_O 33.52 27.981 1245.96 304.77 0.0064 27.29 27.802 1243.84 483.4 0.0971 1.36071 +FS_45 HPT.Fl_O 36.81 9.935 941.60 227.47 0.0058 73.37 9.345 925.83 439.1 0.2990 1.38038 +FS_48 Duct3.Fl_O 36.81 9.886 941.60 227.47 0.0058 73.74 9.298 925.83 441.4 0.2990 1.38038 +FS_5 LPT.Fl_O 36.81 3.824 744.41 178.93 0.0058 169.51 3.720 738.70 1477.4 0.1987 1.39091 +FS_7 Duct4.Fl_O 36.81 3.785 744.41 178.93 0.0058 171.22 3.730 741.35 2018.9 0.1453 1.39091 +FS_9 Core_Nozz.Fl_O 36.81 3.785 744.41 178.93 0.0058 171.22 3.458 725.71 862.8 0.3628 1.39091 +FS_15 BypBld.Fl_O 354.88 5.435 451.89 107.96 0.0000 895.65 4.736 434.42 3795.6 0.4476 1.40132 +FS_17 Duct5.Fl_O 354.88 5.394 451.89 107.96 0.0000 902.42 4.701 434.42 3824.3 0.4476 1.40132 +FS_19 Byp_Nozz.Fl_O 354.88 5.394 451.89 107.96 0.0000 902.42 3.458 397.84 2706.4 0.8228 1.40132 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1058.29 1.088 0.7853 2037.361 1.0310 0.7879 -1800.5 82.22 25.26 +LPC 92.60 1.424 0.8193 2006.513 1.1299 0.8282 -727.7 28.69 8.24 +HPC 69.31 3.846 0.8535 6017.151 1.5472 0.8780 -3488.3 49.89 50.90 +HPT 27.29 2.816 0.9179 169.130 1.2885 0.9064 3488.3 +LPT 73.74 2.585 0.9011 61.035 1.2649 0.8885 2528.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2029.12 1.061 0.8113 0.517 2.6313 0.5215 1.4369 0.9679 3943.9586 +LPC 99.33 1.130 0.8534 0.548 1.5620 0.9323 3.2631 0.9600 3662.6571 +HPC 164.78 14.156 0.8420 0.947 2.3813 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.275 0.9363 110.462 5.2749 1.4085 0.4249 0.9803 1.5311 +LPT 153.22 3.212 0.9000 75.248 3.2117 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3258.90 8881.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 608.80 145.59 10.909 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 608.80 145.59 10.909 +Duct1 0.0025 0.2229 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 608.80 145.59 10.909 +Duct2 0.0025 0.3413 365.99 +Duct3 0.0050 0.2990 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1987 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.2810 789.98 189.38 29.609 +Duct5 0.0075 0.4476 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.0129 789.98 189.38 29.609 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 451.89 107.96 5.435 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.6963 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 5970.0 3068.9 3488.3 +LP_Shaft 1872.9 7089.6 2528.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1245.96 0.9940 0.0550 0.21363 0.00641 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.560 0.9975 1.0000 0.9975 2706.36 0.823 802.9 8855.6 +Core_Nozz 1.095 0.9999 1.0000 0.9999 862.88 0.363 477.7 546.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:54 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 330 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 35000.0 0.00 645.92 10670.3 0.6079 6486.06 5.0401 778.64 22.726 2355.4 2295.4 1836.8 + core size:19.95 Q: 223.27 Maximum Thrust: 10670.3 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 645.92 5.272 444.43 106.17 0.0000 1666.72 3.458 393.85 5041.0 0.8000 1.40134 +FS_2 Inlet.Fl_O 645.92 5.246 444.43 106.17 0.0000 1675.11 4.187 416.66 5943.4 0.5763 1.40134 +FS_21 Fan.Fl_O 645.92 8.627 522.82 124.95 0.0000 1104.75 7.416 500.70 4515.2 0.4696 1.40044 +FS_13 Splitter.Fl_O2 538.98 8.627 522.82 124.95 0.0000 921.85 7.438 501.12 3795.6 0.4650 1.40044 +FS_22 Splitter.Fl_O1 106.94 8.627 522.82 124.95 0.0000 182.90 7.297 498.39 719.5 0.4947 1.40044 +FS_23 Duct1.Fl_O 106.94 8.605 522.82 124.95 0.0000 183.36 7.279 498.39 721.3 0.4947 1.40044 +FS_24 LPC.Fl_O 106.94 21.408 701.47 167.92 0.0000 85.37 18.729 675.34 366.0 0.4417 1.39596 +FS_25 Duct2.Fl_O 106.94 21.355 701.47 167.92 0.0000 85.58 18.682 675.34 366.9 0.4417 1.39596 +FS_3 HPC.Fl_O 106.94 119.812 1199.67 291.23 0.0000 19.95 112.752 1180.20 119.9 0.2990 1.36816 +FS_36 Bld3.Fl_O 97.31 119.812 1199.67 291.23 0.0000 18.15 112.752 1180.20 109.1 0.2990 1.36816 +FS_4 Burner.Fl_O 99.12 113.222 2355.37 618.50 0.0185 27.42 112.492 2351.82 483.4 0.0996 1.30456 +FS_45 HPT.Fl_O 108.74 42.401 1836.76 468.27 0.0168 70.92 40.051 1811.37 439.1 0.2945 1.32255 +FS_48 Duct3.Fl_O 108.74 42.189 1836.76 468.27 0.0168 71.28 39.851 1811.37 441.4 0.2945 1.32255 +FS_5 LPT.Fl_O 108.74 8.630 1272.43 314.48 0.0168 290.04 7.899 1243.40 1477.4 0.3636 1.35200 +FS_7 Duct4.Fl_O 108.74 8.543 1272.43 314.48 0.0168 292.97 8.167 1257.57 2018.9 0.2589 1.35200 +FS_9 Core_Nozz.Fl_O 108.74 8.543 1272.43 314.48 0.0168 292.97 4.562 1078.40 862.9 1.0000 1.35200 +FS_15 BypBld.Fl_O 538.98 8.627 522.82 124.95 0.0000 921.85 7.438 501.12 3795.6 0.4650 1.40044 +FS_17 Duct5.Fl_O 538.98 8.562 522.82 124.95 0.0000 928.81 7.382 501.12 3824.3 0.4650 1.40044 +FS_19 Byp_Nozz.Fl_O 538.98 8.562 522.82 124.95 0.0000 928.81 4.521 435.48 2706.3 1.0000 1.40044 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.645 0.8675 3944.235 1.1764 0.8766 -17158.0 24.71 17.45 +LPC 183.36 2.488 0.8683 3636.539 1.3417 0.8840 -6502.2 28.40 23.31 +HPC 85.58 5.611 0.8651 6326.387 1.7102 0.8923 -18656.5 20.07 20.13 +HPT 27.42 2.670 0.9133 151.595 1.2343 0.9034 18656.8 +LPT 71.28 4.889 0.9322 85.191 1.4435 0.9178 23660.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8963 1.000 2.3706 0.5215 1.4369 0.9679 3943.9586 +LPC 196.68 1.456 0.9045 0.993 1.7669 0.9323 3.2631 0.9600 3662.6571 +HPC 203.46 22.313 0.8534 0.995 2.0422 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.931 0.9316 99.010 4.9312 1.4085 0.4249 0.9803 1.5311 +LPT 148.11 6.425 0.9310 105.030 6.4247 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5040.99 15631.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 878.85 211.08 35.779 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 878.85 211.08 35.779 +Duct1 0.0025 0.4947 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 878.85 211.08 35.779 +Duct2 0.0025 0.4417 365.99 +Duct3 0.0050 0.2945 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.7428 1199.67 291.23 119.812 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.8816 1199.67 291.23 119.812 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 522.82 124.95 8.627 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0401 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7357.3 13318.5 18656.8 +LP_Shaft 3651.1 34035.6 23660.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2355.37 0.9940 0.0550 1.80168 0.01851 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.476 0.9962 1.0000 0.9975 2706.36 1.000 1020.9 19979.1 +Core_Nozz 2.471 0.9979 1.0000 0.9999 862.88 1.000 1589.0 6322.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:54 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 331 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 35000.0 0.00 629.71 9602.8 0.5975 5737.91 5.3029 778.64 20.829 2270.1 2212.6 1763.7 + core size:20.04 Q: 223.27 Maximum Thrust: 10670.3 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 629.71 5.272 444.43 106.17 0.0000 1624.89 3.458 393.85 4914.5 0.8000 1.40134 +FS_2 Inlet.Fl_O 629.71 5.246 444.43 106.17 0.0000 1633.07 4.258 418.66 5943.4 0.5538 1.40134 +FS_21 Fan.Fl_O 629.71 8.431 516.88 123.52 0.0000 1095.71 7.272 495.46 4515.2 0.4645 1.40055 +FS_13 Splitter.Fl_O2 529.80 8.431 516.88 123.52 0.0000 921.87 7.269 495.42 3795.6 0.4650 1.40055 +FS_22 Splitter.Fl_O1 99.91 8.431 516.88 123.52 0.0000 173.84 7.284 495.70 719.5 0.4617 1.40055 +FS_23 Duct1.Fl_O 99.91 8.410 516.88 123.52 0.0000 174.28 7.266 495.70 721.3 0.4617 1.40055 +FS_24 LPC.Fl_O 99.91 19.592 679.71 162.67 0.0000 85.79 17.111 654.05 366.0 0.4444 1.39672 +FS_25 Duct2.Fl_O 99.91 19.543 679.71 162.67 0.0000 86.00 17.069 654.05 366.9 0.4444 1.39672 +FS_3 HPC.Fl_O 99.91 109.807 1165.33 282.50 0.0000 20.04 103.272 1146.14 119.9 0.3004 1.37033 +FS_36 Bld3.Fl_O 90.92 109.807 1165.33 282.50 0.0000 18.24 103.272 1146.14 109.1 0.3004 1.37033 +FS_4 Burner.Fl_O 92.51 103.768 2270.08 592.84 0.0175 27.41 103.098 2266.63 483.4 0.0995 1.30753 +FS_45 HPT.Fl_O 101.50 38.475 1763.72 447.40 0.0160 71.49 36.307 1738.70 439.1 0.2967 1.32631 +FS_48 Duct3.Fl_O 101.50 38.283 1763.72 447.40 0.0160 71.85 36.126 1738.70 441.4 0.2967 1.32631 +FS_5 LPT.Fl_O 101.50 7.887 1222.79 301.23 0.0160 290.41 7.217 1194.60 1477.4 0.3636 1.35573 +FS_7 Duct4.Fl_O 101.50 7.808 1222.79 301.23 0.0160 293.34 7.463 1208.36 2018.9 0.2589 1.35573 +FS_9 Core_Nozz.Fl_O 101.50 7.808 1222.79 301.23 0.0160 293.34 4.166 1034.77 862.9 1.0000 1.35573 +FS_15 BypBld.Fl_O 529.80 8.431 516.88 123.52 0.0000 921.87 7.269 495.42 3795.6 0.4650 1.40055 +FS_17 Duct5.Fl_O 529.80 8.368 516.88 123.52 0.0000 928.83 7.215 495.42 3824.3 0.4650 1.40055 +FS_19 Byp_Nozz.Fl_O 529.80 8.368 516.88 123.52 0.0000 928.83 4.418 430.52 2706.4 1.0000 1.40055 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1633.07 1.607 0.8925 3742.526 1.1630 0.8995 -15458.8 28.21 17.74 +LPC 174.28 2.330 0.8661 3470.337 1.3150 0.8810 -5533.0 28.93 22.21 +HPC 86.00 5.619 0.8640 6336.988 1.7145 0.8916 -16939.3 20.48 20.51 +HPT 27.41 2.697 0.9138 152.257 1.2393 0.9038 16939.3 +LPT 71.85 4.854 0.9277 82.491 1.4424 0.9123 20991.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3130.99 1.423 0.9220 0.949 2.1753 0.5215 1.4369 0.9679 3943.9586 +LPC 186.93 1.407 0.9021 0.947 1.7531 0.9323 3.2631 0.9600 3662.6571 +HPC 204.46 22.351 0.8523 0.997 2.0717 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.994 0.9321 99.442 4.9941 1.4085 0.4249 0.9803 1.5311 +LPT 149.29 6.376 0.9265 101.701 6.3765 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4914.49 15239.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 852.43 204.61 32.767 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 852.43 204.61 32.767 +Duct1 0.0025 0.4617 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 852.43 204.61 32.767 +Duct2 0.0025 0.4444 365.99 +Duct3 0.0050 0.2967 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.4968 1165.33 282.50 109.807 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.4950 1165.33 282.50 109.807 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 516.88 123.52 8.431 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3029 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7254.4 12264.0 16939.3 +LP_Shaft 3464.4 31823.9 20991.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2270.08 0.9940 0.0550 1.59387 0.01753 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.420 0.9965 1.0000 0.9975 2706.36 1.000 1015.1 19314.7 +Core_Nozz 2.258 0.9991 1.0000 0.9999 862.88 1.000 1558.4 5527.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:54 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 332 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 35000.0 0.00 611.38 8536.3 0.5931 5062.80 5.5081 778.64 19.191 2182.5 2127.9 1691.5 + core size:20.19 Q: 223.27 Maximum Thrust: 10670.3 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 611.38 5.272 444.43 106.17 0.0000 1577.61 3.458 393.85 4771.5 0.8000 1.40134 +FS_2 Inlet.Fl_O 611.38 5.246 444.43 106.17 0.0000 1585.55 4.332 420.73 5943.4 0.5299 1.40134 +FS_21 Fan.Fl_O 611.38 8.191 511.46 122.22 0.0000 1089.21 7.081 490.58 4515.2 0.4608 1.40064 +FS_13 Splitter.Fl_O2 517.44 8.191 511.46 122.22 0.0000 921.85 7.063 490.21 3795.6 0.4649 1.40064 +FS_22 Splitter.Fl_O1 93.94 8.191 511.46 122.22 0.0000 167.36 7.173 492.40 719.5 0.4394 1.40064 +FS_23 Duct1.Fl_O 93.94 8.171 511.46 122.22 0.0000 167.78 7.156 492.40 721.3 0.4394 1.40064 +FS_24 LPC.Fl_O 93.94 18.433 666.31 159.43 0.0000 84.89 16.157 641.78 366.0 0.4383 1.39721 +FS_25 Duct2.Fl_O 93.94 18.387 666.31 159.43 0.0000 85.10 16.117 641.78 366.9 0.4383 1.39721 +FS_3 HPC.Fl_O 93.94 101.172 1135.87 275.04 0.0000 20.19 95.053 1116.79 119.9 0.3027 1.37218 +FS_36 Bld3.Fl_O 85.49 101.172 1135.87 275.04 0.0000 18.38 95.053 1116.79 109.1 0.3027 1.37218 +FS_4 Burner.Fl_O 86.89 95.608 2182.52 566.69 0.0165 27.40 94.992 2179.18 483.4 0.0994 1.31064 +FS_45 HPT.Fl_O 95.35 35.277 1691.51 426.93 0.0150 71.73 33.275 1667.12 439.1 0.2973 1.33028 +FS_48 Duct3.Fl_O 95.35 35.101 1691.51 426.93 0.0150 72.09 33.109 1667.12 441.4 0.2973 1.33028 +FS_5 LPT.Fl_O 95.35 7.238 1170.36 287.35 0.0150 290.81 6.622 1143.08 1477.4 0.3636 1.35973 +FS_7 Duct4.Fl_O 95.35 7.166 1170.36 287.35 0.0150 293.75 6.848 1156.39 2018.9 0.2589 1.35973 +FS_9 Core_Nozz.Fl_O 95.35 7.166 1170.36 287.35 0.0150 293.75 3.821 988.83 862.9 1.0000 1.35973 +FS_15 BypBld.Fl_O 517.44 8.191 511.46 122.22 0.0000 921.85 7.063 490.21 3795.6 0.4649 1.40064 +FS_17 Duct5.Fl_O 517.44 8.130 511.46 122.22 0.0000 928.81 7.010 490.21 3824.3 0.4649 1.40064 +FS_19 Byp_Nozz.Fl_O 517.44 8.130 511.46 122.22 0.0000 928.81 4.293 426.00 2706.4 1.0000 1.40064 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1585.55 1.562 0.9023 3613.832 1.1508 0.9083 -13883.7 31.67 18.33 +LPC 167.78 2.256 0.8632 3368.735 1.3028 0.8778 -4945.8 28.07 20.51 +HPC 85.10 5.502 0.8648 6313.510 1.7047 0.8921 -15366.0 22.11 22.18 +HPT 27.40 2.710 0.9145 153.174 1.2431 0.9043 15365.9 +LPT 72.09 4.850 0.9257 81.337 1.4453 0.9098 18829.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3040.10 1.391 0.9322 0.916 2.0966 0.5215 1.4369 0.9679 3943.9586 +LPC 179.97 1.385 0.8991 0.920 1.7167 0.9323 3.2631 0.9600 3662.6571 +HPC 202.32 21.813 0.8531 0.993 2.0969 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.025 0.9328 100.040 5.0251 1.4085 0.4249 0.9803 1.5311 +LPT 149.80 6.370 0.9245 100.278 6.3701 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4771.48 14796.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 833.15 199.90 30.515 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 833.15 199.90 30.515 +Duct1 0.0025 0.4394 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 833.15 199.90 30.515 +Duct2 0.0025 0.4383 365.99 +Duct3 0.0050 0.2973 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.2880 1135.87 275.04 101.172 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.1668 1135.87 275.04 101.172 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 511.46 122.22 8.191 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5081 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7155.9 11277.9 15365.9 +LP_Shaft 3345.2 29563.3 18829.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2182.52 0.9940 0.0550 1.40633 0.01645 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.351 0.9968 1.0000 0.9975 2706.36 1.000 1009.7 18498.5 +Core_Nozz 2.072 0.9998 1.0000 0.9999 862.88 1.000 1525.5 4833.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:54 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 333 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 35000.0 0.00 571.58 6402.1 0.5981 3829.13 5.9831 778.64 15.993 2003.0 1954.3 1546.0 + core size:20.55 Q: 223.27 Maximum Thrust: 10670.3 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 571.58 5.272 444.43 106.17 0.0000 1474.89 3.458 393.85 4460.8 0.8000 1.40134 +FS_2 Inlet.Fl_O 571.58 5.246 444.43 106.17 0.0000 1482.31 4.474 424.65 5943.4 0.4818 1.40134 +FS_21 Fan.Fl_O 571.58 7.669 500.50 119.60 0.0000 1075.95 6.659 480.69 4515.2 0.4534 1.40081 +FS_13 Splitter.Fl_O2 489.73 7.669 500.50 119.60 0.0000 921.87 6.612 479.71 3795.6 0.4649 1.40081 +FS_22 Splitter.Fl_O1 81.85 7.669 500.50 119.60 0.0000 154.08 6.882 485.24 719.5 0.3961 1.40081 +FS_23 Duct1.Fl_O 81.85 7.650 500.50 119.60 0.0000 154.46 6.865 485.24 721.3 0.3961 1.40081 +FS_24 LPC.Fl_O 81.85 16.328 642.14 153.61 0.0000 81.97 14.470 620.42 366.0 0.4192 1.39807 +FS_25 Duct2.Fl_O 81.85 16.287 642.14 153.61 0.0000 82.18 14.434 620.42 366.9 0.4192 1.39807 +FS_3 HPC.Fl_O 81.85 84.314 1076.02 259.97 0.0000 20.55 79.020 1057.10 119.9 0.3082 1.37595 +FS_36 Bld3.Fl_O 74.48 84.314 1076.02 259.97 0.0000 18.70 79.020 1057.10 109.1 0.3082 1.37595 +FS_4 Burner.Fl_O 75.55 79.677 2003.03 513.89 0.0143 27.38 79.164 1999.92 483.4 0.0990 1.31787 +FS_45 HPT.Fl_O 82.91 29.226 1546.01 386.33 0.0130 71.98 27.555 1523.13 439.1 0.2975 1.33876 +FS_48 Duct3.Fl_O 82.91 29.079 1546.01 386.33 0.0130 72.34 27.418 1523.13 441.4 0.2975 1.33876 +FS_5 LPT.Fl_O 82.91 6.028 1066.45 260.21 0.0130 289.87 5.519 1041.41 1477.4 0.3611 1.36771 +FS_7 Duct4.Fl_O 82.91 5.967 1066.45 260.21 0.0130 292.80 5.705 1053.62 2018.9 0.2572 1.36771 +FS_9 Core_Nozz.Fl_O 82.91 5.967 1066.45 260.21 0.0130 292.80 3.458 919.55 862.9 0.9246 1.36771 +FS_15 BypBld.Fl_O 489.73 7.669 500.50 119.60 0.0000 921.87 6.612 479.71 3795.6 0.4649 1.40081 +FS_17 Duct5.Fl_O 489.73 7.611 500.50 119.60 0.0000 928.84 6.563 479.71 3824.3 0.4649 1.40081 +FS_19 Byp_Nozz.Fl_O 489.73 7.611 500.50 119.60 0.0000 928.84 4.019 416.86 2706.4 1.0000 1.40081 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1482.31 1.462 0.9104 3371.183 1.1262 0.9152 -10856.6 39.33 19.69 +LPC 154.46 2.134 0.8543 3176.754 1.2830 0.8688 -3938.8 25.11 16.56 +HPC 82.18 5.177 0.8659 6251.629 1.6757 0.8923 -12317.3 26.41 26.56 +HPT 27.38 2.726 0.9148 155.424 1.2500 0.9046 12317.5 +LPT 72.34 4.824 0.9207 79.366 1.4497 0.9038 14795.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2842.07 1.322 0.9406 0.855 2.0400 0.5215 1.4369 0.9679 3943.9586 +LPC 165.68 1.348 0.8898 0.867 1.6205 0.9323 3.2631 0.9600 3662.6571 +HPC 195.36 20.308 0.8542 0.983 2.1340 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.063 0.9332 101.510 5.0629 1.4085 0.4249 0.9803 1.5311 +LPT 150.32 6.335 0.9195 97.848 6.3347 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4460.81 13832.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 795.98 190.84 26.253 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 795.98 190.84 26.253 +Duct1 0.0025 0.3961 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 795.98 190.84 26.253 +Duct2 0.0025 0.4192 365.99 +Duct3 0.0050 0.2975 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3611 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.8648 1076.02 259.97 84.314 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.5018 1076.02 259.97 84.314 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 500.50 119.60 7.669 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9831 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6956.0 9300.3 12317.5 +LP_Shaft 3120.6 24900.9 14795.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2003.03 0.9940 0.0550 1.06365 0.01428 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.201 0.9973 1.0000 0.9975 2706.36 1.000 998.8 16722.2 +Core_Nozz 1.726 0.9999 1.0000 0.9999 862.88 0.925 1363.0 3512.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:54 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 334 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 35000.0 0.00 525.23 4268.2 0.6309 2692.85 6.6896 778.64 12.648 1804.4 1762.0 1385.2 + core size:20.95 Q: 223.27 Maximum Thrust: 10670.3 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 525.23 5.272 444.43 106.17 0.0000 1355.29 3.458 393.85 4099.1 0.8000 1.40134 +FS_2 Inlet.Fl_O 525.23 5.246 444.43 106.17 0.0000 1362.11 4.616 428.46 5943.4 0.4311 1.40134 +FS_21 Fan.Fl_O 525.23 7.064 487.87 116.57 0.0000 1059.75 6.167 469.27 4515.2 0.4445 1.40099 +FS_13 Splitter.Fl_O2 456.92 7.064 487.87 116.57 0.0000 921.93 6.090 467.59 3795.6 0.4650 1.40099 +FS_22 Splitter.Fl_O1 68.30 7.064 487.87 116.57 0.0000 137.82 6.500 476.38 719.5 0.3468 1.40099 +FS_23 Duct1.Fl_O 68.30 7.046 487.87 116.57 0.0000 138.16 6.483 476.38 721.3 0.3468 1.40099 +FS_24 LPC.Fl_O 68.30 13.791 610.21 145.93 0.0000 78.95 12.352 591.33 366.0 0.4000 1.39887 +FS_25 Duct2.Fl_O 68.30 13.757 610.21 145.93 0.0000 79.15 12.321 591.33 366.9 0.4000 1.39887 +FS_3 HPC.Fl_O 68.30 66.682 1004.80 242.18 0.0000 20.95 62.317 986.21 119.9 0.3145 1.38041 +FS_36 Bld3.Fl_O 62.16 66.682 1004.80 242.18 0.0000 19.07 62.317 986.21 109.1 0.3145 1.38041 +FS_4 Burner.Fl_O 62.90 63.015 1804.40 456.85 0.0120 27.36 62.610 1801.54 483.4 0.0986 1.32721 +FS_45 HPT.Fl_O 69.05 22.912 1385.18 342.53 0.0110 72.38 21.588 1363.98 439.1 0.2981 1.34904 +FS_48 Duct3.Fl_O 69.05 22.798 1385.18 342.53 0.0110 72.74 21.480 1363.98 441.4 0.2981 1.34904 +FS_5 LPT.Fl_O 69.05 5.050 965.88 234.39 0.0110 274.23 4.673 945.61 1477.4 0.3376 1.37550 +FS_7 Duct4.Fl_O 69.05 4.999 965.88 234.39 0.0110 277.00 4.804 955.40 2018.9 0.2416 1.37550 +FS_9 Core_Nozz.Fl_O 69.05 4.999 965.88 234.39 0.0110 277.00 3.458 872.98 862.9 0.7492 1.37550 +FS_15 BypBld.Fl_O 456.92 7.064 487.87 116.57 0.0000 921.93 6.090 467.59 3795.6 0.4650 1.40099 +FS_17 Duct5.Fl_O 456.92 7.011 487.87 116.57 0.0000 928.90 6.045 467.59 3824.3 0.4650 1.40099 +FS_19 Byp_Nozz.Fl_O 456.92 7.011 487.87 116.57 0.0000 928.90 3.702 406.34 2706.3 1.0000 1.40099 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1362.11 1.347 0.9101 3052.757 1.0977 0.9138 -7728.0 47.02 21.42 +LPC 138.16 1.957 0.8437 2913.691 1.2508 0.8577 -2837.0 22.75 13.06 +HPC 79.15 4.847 0.8647 6200.158 1.6466 0.8905 -9301.6 31.30 31.54 +HPT 27.36 2.750 0.9154 158.318 1.2590 0.9046 9301.6 +LPT 72.74 4.515 0.9158 75.927 1.4341 0.8983 10565.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2611.67 1.241 0.9402 0.774 2.0757 0.5215 1.4369 0.9679 3943.9586 +LPC 148.19 1.293 0.8788 0.796 1.5419 0.9323 3.2631 0.9600 3662.6571 +HPC 188.16 18.785 0.8531 0.975 2.1669 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.119 0.9338 103.400 5.1194 1.4085 0.4249 0.9803 1.5311 +LPT 151.15 5.903 0.9147 93.609 5.9028 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4099.08 12710.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 749.79 179.62 21.510 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 749.79 179.62 21.510 +Duct1 0.0025 0.3468 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 749.79 179.62 21.510 +Duct2 0.0025 0.4000 365.99 +Duct3 0.0050 0.2981 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3376 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.3906 1004.80 242.18 66.682 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.7567 1004.80 242.18 66.682 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 487.87 116.57 7.064 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6896 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6725.1 7264.3 9301.6 +LP_Shaft 2825.9 19636.4 10565.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1804.40 0.9940 0.0550 0.74801 0.01203 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.028 0.9976 1.0000 0.9975 2706.36 1.000 986.1 14666.2 +Core_Nozz 1.446 0.9999 1.0000 0.9999 862.88 0.749 1077.7 2312.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:54 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 335 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 35000.0 0.00 469.87 2134.1 0.7563 1614.04 7.8875 778.64 9.057 1549.0 1514.7 1180.5 + core size:21.56 Q: 223.27 Maximum Thrust: 10670.3 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 469.87 5.272 444.43 106.17 0.0000 1212.45 3.458 393.85 3667.1 0.8000 1.40134 +FS_2 Inlet.Fl_O 469.87 5.246 444.43 106.17 0.0000 1218.56 4.758 432.19 5943.4 0.3758 1.40134 +FS_21 Fan.Fl_O 469.87 6.351 472.59 112.91 0.0000 1037.91 5.583 455.47 4515.2 0.4327 1.40117 +FS_13 Splitter.Fl_O2 417.00 6.351 472.59 112.91 0.0000 921.13 5.477 452.99 3795.6 0.4644 1.40117 +FS_22 Splitter.Fl_O1 52.87 6.351 472.59 112.91 0.0000 116.78 5.996 464.88 719.5 0.2874 1.40117 +FS_23 Duct1.Fl_O 52.87 6.335 472.59 112.91 0.0000 117.08 5.981 464.88 721.3 0.2874 1.40117 +FS_24 LPC.Fl_O 52.87 10.876 567.71 135.72 0.0000 74.74 9.874 552.26 366.0 0.3742 1.39957 +FS_25 Duct2.Fl_O 52.87 10.849 567.71 135.72 0.0000 74.93 9.849 552.26 366.9 0.3742 1.39957 +FS_3 HPC.Fl_O 52.87 47.747 910.53 218.86 0.0000 21.56 44.422 892.39 119.9 0.3242 1.38621 +FS_36 Bld3.Fl_O 48.11 47.747 910.53 218.86 0.0000 19.62 44.422 892.39 109.1 0.3242 1.38621 +FS_4 Burner.Fl_O 48.56 45.121 1549.04 385.76 0.0093 27.33 44.832 1546.51 483.4 0.0980 1.34113 +FS_45 HPT.Fl_O 53.32 16.218 1180.50 288.42 0.0085 72.89 15.267 1161.62 439.1 0.2988 1.36343 +FS_48 Duct3.Fl_O 53.32 16.137 1180.50 288.42 0.0085 73.26 15.190 1161.62 441.4 0.2988 1.36343 +FS_5 LPT.Fl_O 53.32 4.298 855.01 206.41 0.0085 234.06 4.070 842.18 1477.4 0.2816 1.38384 +FS_7 Duct4.Fl_O 53.32 4.255 855.01 206.41 0.0085 236.42 4.135 848.26 2018.9 0.2036 1.38384 +FS_9 Core_Nozz.Fl_O 53.32 4.255 855.01 206.41 0.0085 236.42 3.458 807.08 862.9 0.5552 1.38384 +FS_15 BypBld.Fl_O 417.00 6.351 472.59 112.91 0.0000 921.13 5.477 452.99 3795.6 0.4644 1.40117 +FS_17 Duct5.Fl_O 417.00 6.303 472.59 112.91 0.0000 928.09 5.436 452.99 3824.3 0.4644 1.40117 +FS_19 Byp_Nozz.Fl_O 417.00 6.303 472.59 112.91 0.0000 928.09 3.458 397.93 2706.3 0.9670 1.40117 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1218.56 1.211 0.8881 2616.336 1.0634 0.8911 -4480.8 57.39 24.02 +LPC 117.08 1.717 0.8305 2537.202 1.2013 0.8430 -1705.9 22.55 9.67 +HPC 74.93 4.401 0.8627 6119.685 1.6039 0.8874 -6219.0 38.79 39.37 +HPT 27.33 2.782 0.9164 162.674 1.2719 0.9052 6219.1 +LPT 73.26 3.754 0.9115 70.488 1.3807 0.8953 6186.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2336.41 1.147 0.9175 0.663 2.2558 0.5215 1.4369 0.9679 3943.9586 +LPC 125.58 1.220 0.8651 0.693 1.4950 0.9323 3.2631 0.9600 3662.6571 +HPC 178.13 16.723 0.8510 0.963 2.2504 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.195 0.9348 106.245 5.1946 1.4085 0.4249 0.9803 1.5311 +LPT 152.22 4.842 0.9103 86.903 4.8422 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3667.07 11371.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 688.62 164.82 16.254 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 688.62 164.82 16.254 +Duct1 0.0025 0.2874 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 688.62 164.82 16.254 +Duct2 0.0025 0.3742 365.99 +Duct3 0.0050 0.2988 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2816 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.8504 910.53 218.86 47.747 +Duct5 0.0075 0.4644 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.9078 910.53 218.86 47.747 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 472.59 112.91 6.351 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8875 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6402.5 5101.7 6219.1 +LP_Shaft 2421.9 13416.6 6186.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1549.04 0.9940 0.0550 0.44834 0.00932 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.823 0.9975 1.0000 0.9975 2706.36 0.967 943.7 12230.6 +Core_Nozz 1.231 0.9999 1.0000 0.9999 862.88 0.555 769.3 1274.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:54 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 336 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 11/ 21/ 1/ 9 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 35000.0 0.00 415.12 533.5 1.5403 821.77 9.7448 778.64 5.976 1265.5 1240.3 957.2 + core size:22.45 Q: 223.27 Maximum Thrust: 10670.3 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 415.12 5.272 444.43 106.17 0.0000 1071.17 3.458 393.85 3239.8 0.8000 1.40134 +FS_2 Inlet.Fl_O 415.12 5.246 444.43 106.17 0.0000 1076.57 4.875 435.20 5943.4 0.3251 1.40134 +FS_21 Fan.Fl_O 415.12 5.726 458.84 109.62 0.0000 1002.05 5.089 443.58 4515.2 0.4139 1.40128 +FS_13 Splitter.Fl_O2 376.49 5.726 458.84 109.62 0.0000 908.79 4.964 440.44 3795.6 0.4562 1.40128 +FS_22 Splitter.Fl_O1 38.63 5.726 458.84 109.62 0.0000 93.26 5.527 454.21 719.5 0.2252 1.40128 +FS_23 Duct1.Fl_O 38.63 5.712 458.84 109.62 0.0000 93.49 5.513 454.21 721.3 0.2252 1.40128 +FS_24 LPC.Fl_O 38.63 8.272 521.58 124.65 0.0000 68.83 7.637 509.80 366.0 0.3396 1.40046 +FS_25 Duct2.Fl_O 38.63 8.251 521.58 124.65 0.0000 69.00 7.618 509.80 366.9 0.3396 1.40046 +FS_3 HPC.Fl_O 38.63 31.505 805.17 193.07 0.0000 22.45 29.108 787.42 119.9 0.3390 1.39170 +FS_36 Bld3.Fl_O 35.16 31.505 805.17 193.07 0.0000 20.43 29.108 787.42 109.1 0.3390 1.39170 +FS_4 Burner.Fl_O 35.39 29.772 1265.47 309.85 0.0065 27.28 29.582 1263.33 483.4 0.0971 1.35943 +FS_45 HPT.Fl_O 38.86 10.578 957.23 231.38 0.0059 73.35 9.949 941.24 439.1 0.2991 1.37936 +FS_48 Duct3.Fl_O 38.86 10.525 957.23 231.38 0.0059 73.72 9.900 941.24 441.4 0.2991 1.37936 +FS_5 LPT.Fl_O 38.86 3.863 747.15 179.61 0.0059 177.45 3.748 740.85 1477.4 0.2086 1.39076 +FS_7 Duct4.Fl_O 38.86 3.824 747.15 179.61 0.0059 179.24 3.763 743.78 2018.9 0.1523 1.39076 +FS_9 Core_Nozz.Fl_O 38.86 3.824 747.15 179.61 0.0059 179.24 3.458 726.29 862.9 0.3832 1.39076 +FS_15 BypBld.Fl_O 376.49 5.726 458.84 109.62 0.0000 908.79 4.964 440.44 3795.6 0.4562 1.40128 +FS_17 Duct5.Fl_O 376.49 5.683 458.84 109.62 0.0000 915.65 4.927 440.44 3824.3 0.4562 1.40128 +FS_19 Byp_Nozz.Fl_O 376.49 5.683 458.84 109.62 0.0000 915.65 3.458 397.97 2706.4 0.8731 1.40128 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1076.57 1.092 0.7845 2081.049 1.0324 0.7872 -2024.9 81.07 25.92 +LPC 93.49 1.448 0.8176 2048.126 1.1367 0.8270 -821.5 26.64 7.86 +HPC 69.00 3.818 0.8528 6011.440 1.5437 0.8773 -3740.2 50.47 51.49 +HPT 27.28 2.815 0.9180 169.460 1.2876 0.9066 3740.2 +LPT 73.72 2.725 0.9020 62.263 1.2812 0.8887 2846.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2064.17 1.064 0.8105 0.528 2.6335 0.5215 1.4369 0.9679 3943.9586 +LPC 100.28 1.137 0.8516 0.559 1.5262 0.9323 3.2631 0.9600 3662.6571 +HPC 164.04 14.028 0.8413 0.946 2.3847 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.271 0.9364 110.677 5.2710 1.4085 0.4249 0.9803 1.5311 +LPT 153.18 3.406 0.9009 76.763 3.4057 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3239.77 10046.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 621.31 148.60 11.658 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 621.31 148.60 11.658 +Duct1 0.0025 0.2252 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 621.31 148.60 11.658 +Duct2 0.0025 0.3396 365.99 +Duct3 0.0050 0.2991 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2086 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.3522 805.17 193.07 31.505 +Duct5 0.0075 0.4562 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.1249 805.17 193.07 31.505 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 458.84 109.62 5.726 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.7448 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6028.3 3258.6 3740.2 +LP_Shaft 1926.4 7760.6 2846.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1265.47 0.9940 0.0550 0.22827 0.00649 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.644 0.9975 1.0000 0.9975 2706.36 0.873 852.0 9970.2 +Core_Nozz 1.106 0.9999 1.0000 0.9999 862.88 0.383 504.6 609.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 337 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 35000.0 0.00 674.69 10979.3 0.6277 6892.13 5.0406 827.30 22.720 2387.5 2326.8 1863.1 + core size:19.94 Q: 252.05 Maximum Thrust: 10979.3 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 674.69 5.547 450.95 107.73 0.0000 1666.72 3.458 393.85 4955.8 0.8500 1.40132 +FS_2 Inlet.Fl_O 674.69 5.519 450.95 107.73 0.0000 1675.11 4.406 422.78 5943.4 0.5763 1.40132 +FS_21 Fan.Fl_O 674.69 9.077 530.49 126.78 0.0000 1104.74 7.803 508.04 4515.2 0.4696 1.40030 +FS_13 Splitter.Fl_O2 563.00 9.077 530.49 126.78 0.0000 921.86 7.826 508.46 3795.6 0.4650 1.40030 +FS_22 Splitter.Fl_O1 111.69 9.077 530.49 126.78 0.0000 182.88 7.678 505.70 719.5 0.4946 1.40030 +FS_23 Duct1.Fl_O 111.69 9.054 530.49 126.78 0.0000 183.34 7.659 505.70 721.3 0.4946 1.40030 +FS_24 LPC.Fl_O 111.69 22.530 711.73 170.40 0.0000 85.34 19.712 685.25 366.0 0.4416 1.39562 +FS_25 Duct2.Fl_O 111.69 22.474 711.73 170.40 0.0000 85.56 19.663 685.25 366.9 0.4416 1.39562 +FS_3 HPC.Fl_O 111.69 126.031 1216.10 295.42 0.0000 19.94 118.609 1196.42 119.9 0.2991 1.36713 +FS_36 Bld3.Fl_O 101.64 126.031 1216.10 295.42 0.0000 18.15 118.609 1196.42 109.1 0.2991 1.36713 +FS_4 Burner.Fl_O 103.55 119.100 2387.54 628.19 0.0188 27.41 118.331 2383.95 483.4 0.0997 1.30352 +FS_45 HPT.Fl_O 113.61 44.617 1863.13 475.83 0.0171 70.92 42.144 1837.46 439.1 0.2946 1.32126 +FS_48 Duct3.Fl_O 113.61 44.393 1863.13 475.83 0.0171 71.28 41.934 1837.46 441.4 0.2946 1.32126 +FS_5 LPT.Fl_O 113.61 9.090 1292.35 319.81 0.0171 289.92 8.321 1262.98 1477.4 0.3636 1.35056 +FS_7 Duct4.Fl_O 113.61 8.999 1292.35 319.81 0.0171 292.85 8.603 1277.32 2018.9 0.2589 1.35056 +FS_9 Core_Nozz.Fl_O 113.61 8.999 1292.35 319.81 0.0171 292.85 4.807 1095.92 862.9 1.0000 1.35056 +FS_15 BypBld.Fl_O 563.00 9.077 530.49 126.78 0.0000 921.86 7.826 508.46 3795.6 0.4650 1.40030 +FS_17 Duct5.Fl_O 563.00 9.009 530.49 126.78 0.0000 928.82 7.767 508.46 3824.3 0.4650 1.40030 +FS_19 Byp_Nozz.Fl_O 563.00 9.009 530.49 126.78 0.0000 928.82 4.757 441.87 2706.3 1.0000 1.40030 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.645 0.8675 3944.235 1.1764 0.8766 -18186.0 24.71 17.45 +LPC 183.34 2.488 0.8683 3636.571 1.3417 0.8840 -6892.6 28.37 23.28 +HPC 85.56 5.608 0.8651 6325.631 1.7087 0.8922 -19756.4 20.10 20.15 +HPT 27.41 2.669 0.9133 151.649 1.2335 0.9035 19756.8 +LPT 71.28 4.884 0.9323 85.204 1.4417 0.9180 25078.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8963 1.000 2.3706 0.5215 1.4369 0.9679 3943.9586 +LPC 196.66 1.456 0.9045 0.993 1.7662 0.9323 3.2631 0.9600 3662.6571 +HPC 203.39 22.301 0.8535 0.995 2.0420 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.929 0.9316 99.045 4.9291 1.4085 0.4249 0.9803 1.5311 +LPT 148.11 6.418 0.9311 105.046 6.4177 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4955.81 17348.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 891.39 214.16 37.645 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 891.39 214.16 37.645 +Duct1 0.0025 0.4946 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 891.39 214.16 37.645 +Duct2 0.0025 0.4416 365.99 +Duct3 0.0050 0.2946 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.9092 1216.10 295.42 126.031 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.1431 1216.10 295.42 126.031 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 530.49 126.78 9.077 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0406 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7409.9 14003.5 19756.8 +LP_Shaft 3677.8 35814.2 25078.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2387.54 0.9940 0.0550 1.91448 0.01884 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.605 0.9953 1.0000 0.9975 2706.36 1.000 1028.4 21510.6 +Core_Nozz 2.603 0.9968 1.0000 0.9999 862.88 1.000 1601.0 6817.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 338 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 35000.0 0.00 657.80 9880.9 0.6173 6099.20 5.3030 827.30 20.828 2301.5 2243.2 1789.4 + core size:20.04 Q: 252.05 Maximum Thrust: 10979.3 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 657.80 5.547 450.95 107.73 0.0000 1625.00 3.458 393.85 4831.8 0.8500 1.40132 +FS_2 Inlet.Fl_O 657.80 5.519 450.95 107.73 0.0000 1633.18 4.480 424.80 5943.4 0.5539 1.40132 +FS_21 Fan.Fl_O 657.80 8.872 524.47 125.34 0.0000 1095.72 7.652 502.74 4515.2 0.4645 1.40041 +FS_13 Splitter.Fl_O2 553.44 8.872 524.47 125.34 0.0000 921.87 7.649 502.70 3795.6 0.4650 1.40041 +FS_22 Splitter.Fl_O1 104.36 8.872 524.47 125.34 0.0000 173.84 7.665 502.99 719.5 0.4618 1.40041 +FS_23 Duct1.Fl_O 104.36 8.850 524.47 125.34 0.0000 174.28 7.646 502.99 721.3 0.4618 1.40041 +FS_24 LPC.Fl_O 104.36 20.623 689.69 165.08 0.0000 85.76 18.013 663.69 366.0 0.4443 1.39637 +FS_25 Duct2.Fl_O 104.36 20.571 689.69 165.08 0.0000 85.98 17.968 663.69 366.9 0.4443 1.39637 +FS_3 HPC.Fl_O 104.36 115.533 1181.46 286.60 0.0000 20.04 108.661 1162.06 119.9 0.3004 1.36931 +FS_36 Bld3.Fl_O 94.97 115.533 1181.46 286.60 0.0000 18.23 108.661 1162.06 109.1 0.3004 1.36931 +FS_4 Burner.Fl_O 96.67 109.179 2301.49 602.22 0.0178 27.41 108.475 2298.00 483.4 0.0995 1.30648 +FS_45 HPT.Fl_O 106.06 40.496 1789.40 454.69 0.0162 71.49 38.214 1764.09 439.1 0.2968 1.32499 +FS_48 Duct3.Fl_O 106.06 40.293 1789.40 454.69 0.0162 71.85 38.023 1764.09 441.4 0.2968 1.32499 +FS_5 LPT.Fl_O 106.06 8.310 1242.20 306.38 0.0162 290.26 7.605 1213.68 1477.4 0.3636 1.35431 +FS_7 Duct4.Fl_O 106.06 8.227 1242.20 306.38 0.0162 293.19 7.864 1227.60 2018.9 0.2589 1.35431 +FS_9 Core_Nozz.Fl_O 106.06 8.227 1242.20 306.38 0.0162 293.19 4.391 1051.79 862.9 1.0000 1.35431 +FS_15 BypBld.Fl_O 553.44 8.872 524.47 125.34 0.0000 921.87 7.649 502.70 3795.6 0.4650 1.40041 +FS_17 Duct5.Fl_O 553.44 8.805 524.47 125.34 0.0000 928.84 7.592 502.70 3824.3 0.4650 1.40041 +FS_19 Byp_Nozz.Fl_O 553.44 8.805 524.47 125.34 0.0000 928.84 4.649 436.85 2706.4 1.0000 1.40041 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1633.18 1.607 0.8925 3742.913 1.1630 0.8995 -16389.2 28.20 17.74 +LPC 174.28 2.330 0.8661 3470.675 1.3150 0.8810 -5867.1 28.90 22.19 +HPC 85.98 5.616 0.8640 6336.239 1.7130 0.8915 -17943.6 20.50 20.53 +HPT 27.41 2.696 0.9138 152.303 1.2384 0.9039 17943.6 +LPT 71.85 4.849 0.9278 82.504 1.4405 0.9125 22256.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3131.22 1.423 0.9220 0.949 2.1756 0.5215 1.4369 0.9679 3943.9586 +LPC 186.93 1.408 0.9021 0.948 1.7524 0.9323 3.2631 0.9600 3662.6571 +HPC 204.39 22.340 0.8524 0.997 2.0714 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.992 0.9322 99.472 4.9918 1.4085 0.4249 0.9803 1.5311 +LPT 149.29 6.369 0.9266 101.717 6.3689 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4831.77 16914.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 864.68 207.61 34.483 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 864.68 207.61 34.483 +Duct1 0.0025 0.4618 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 864.68 207.61 34.483 +Duct2 0.0025 0.4443 365.99 +Duct3 0.0050 0.2968 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.6528 1181.46 286.60 115.533 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.7400 1181.46 286.60 115.533 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 524.47 125.34 8.872 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3030 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7306.6 12898.2 17943.6 +LP_Shaft 3490.0 33493.0 22256.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2301.49 0.9940 0.0550 1.69422 0.01784 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.546 0.9957 1.0000 0.9975 2706.36 1.000 1022.5 20813.5 +Core_Nozz 2.379 0.9985 1.0000 0.9999 862.88 1.000 1570.5 5981.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 339 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 35000.0 0.00 638.67 8783.5 0.6127 5381.24 5.5078 827.30 19.191 2212.7 2157.3 1716.1 + core size:20.19 Q: 252.05 Maximum Thrust: 10979.3 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 638.67 5.547 450.95 107.73 0.0000 1577.73 3.458 393.85 4691.2 0.8500 1.40132 +FS_2 Inlet.Fl_O 638.67 5.519 450.95 107.73 0.0000 1585.68 4.558 426.90 5943.4 0.5299 1.40132 +FS_21 Fan.Fl_O 638.67 8.620 518.97 124.02 0.0000 1089.22 7.451 497.78 4515.2 0.4608 1.40051 +FS_13 Splitter.Fl_O2 540.53 8.620 518.97 124.02 0.0000 921.85 7.432 497.42 3795.6 0.4650 1.40051 +FS_22 Splitter.Fl_O1 98.14 8.620 518.97 124.02 0.0000 167.37 7.548 499.63 719.5 0.4394 1.40051 +FS_23 Duct1.Fl_O 98.14 8.598 518.97 124.02 0.0000 167.79 7.529 499.63 721.3 0.4394 1.40051 +FS_24 LPC.Fl_O 98.14 19.399 676.06 161.79 0.0000 84.88 17.004 651.20 366.0 0.4383 1.39685 +FS_25 Duct2.Fl_O 98.14 19.351 676.06 161.79 0.0000 85.09 16.962 651.20 366.9 0.4383 1.39685 +FS_3 HPC.Fl_O 98.14 106.453 1151.69 279.04 0.0000 20.19 100.018 1132.39 119.9 0.3027 1.37119 +FS_36 Bld3.Fl_O 89.31 106.453 1151.69 279.04 0.0000 18.37 100.018 1132.39 109.1 0.3027 1.37119 +FS_4 Burner.Fl_O 90.80 100.598 2212.72 575.63 0.0167 27.40 99.950 2209.34 483.4 0.0994 1.30961 +FS_45 HPT.Fl_O 99.63 37.131 1716.09 433.84 0.0152 71.73 35.024 1691.42 439.1 0.2974 1.32896 +FS_48 Duct3.Fl_O 99.63 36.946 1716.09 433.84 0.0152 72.09 34.849 1691.42 441.4 0.2974 1.32896 +FS_5 LPT.Fl_O 99.63 7.626 1188.90 292.22 0.0152 290.68 6.978 1161.30 1477.4 0.3636 1.35837 +FS_7 Duct4.Fl_O 99.63 7.550 1188.90 292.22 0.0152 293.61 7.216 1174.77 2018.9 0.2589 1.35837 +FS_9 Core_Nozz.Fl_O 99.63 7.550 1188.90 292.22 0.0152 293.61 4.027 1005.04 862.9 1.0000 1.35837 +FS_15 BypBld.Fl_O 540.53 8.620 518.97 124.02 0.0000 921.85 7.432 497.42 3795.6 0.4650 1.40051 +FS_17 Duct5.Fl_O 540.53 8.555 518.97 124.02 0.0000 928.81 7.376 497.42 3824.3 0.4650 1.40051 +FS_19 Byp_Nozz.Fl_O 540.53 8.555 518.97 124.02 0.0000 928.81 4.517 432.26 2706.4 1.0000 1.40051 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1585.68 1.562 0.9023 3614.129 1.1508 0.9083 -14719.6 31.66 18.33 +LPC 167.79 2.256 0.8631 3368.990 1.3027 0.8778 -5243.4 28.07 20.51 +HPC 85.09 5.501 0.8648 6313.295 1.7035 0.8920 -16281.5 22.12 22.20 +HPT 27.40 2.709 0.9145 153.229 1.2423 0.9043 16281.3 +LPT 72.09 4.844 0.9258 81.349 1.4434 0.9100 19963.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3040.34 1.391 0.9322 0.916 2.0968 0.5215 1.4369 0.9679 3943.9586 +LPC 179.98 1.385 0.8991 0.920 1.7166 0.9323 3.2631 0.9600 3662.6571 +HPC 202.30 21.808 0.8531 0.993 2.0971 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.023 0.9328 100.076 5.0229 1.4085 0.4249 0.9803 1.5311 +LPT 149.79 6.363 0.9246 100.294 6.3628 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4691.22 16422.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 845.13 202.83 32.111 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 845.13 202.83 32.111 +Duct1 0.0025 0.4394 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 845.13 202.83 32.111 +Duct2 0.0025 0.4383 365.99 +Duct3 0.0050 0.2974 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.4349 1151.69 279.04 106.453 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.3977 1151.69 279.04 106.453 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 518.97 124.02 8.620 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5078 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7207.8 11863.7 16281.3 +LP_Shaft 3370.0 31113.1 19963.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2212.72 0.9940 0.0550 1.49479 0.01674 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.474 0.9962 1.0000 0.9975 2706.36 1.000 1017.1 19954.6 +Core_Nozz 2.184 0.9995 1.0000 0.9999 862.88 1.000 1537.2 5251.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 340 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 35000.0 0.00 597.43 6587.5 0.6175 4067.57 5.9838 827.30 15.998 2030.2 1980.9 1568.3 + core size:20.55 Q: 252.05 Maximum Thrust: 10979.3 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 597.43 5.547 450.95 107.73 0.0000 1475.85 3.458 393.85 4388.3 0.8500 1.40132 +FS_2 Inlet.Fl_O 597.43 5.519 450.95 107.73 0.0000 1483.28 4.707 430.85 5943.4 0.4822 1.40132 +FS_21 Fan.Fl_O 597.43 8.076 507.96 121.39 0.0000 1075.91 7.013 487.86 4515.2 0.4534 1.40070 +FS_13 Splitter.Fl_O2 511.88 8.076 507.96 121.39 0.0000 921.85 6.963 486.87 3795.6 0.4649 1.40070 +FS_22 Splitter.Fl_O1 85.55 8.076 507.96 121.39 0.0000 154.06 7.247 492.48 719.5 0.3961 1.40070 +FS_23 Duct1.Fl_O 85.55 8.055 507.96 121.39 0.0000 154.45 7.229 492.48 721.3 0.3961 1.40070 +FS_24 LPC.Fl_O 85.55 17.221 652.04 155.99 0.0000 81.85 15.268 630.07 366.0 0.4185 1.39774 +FS_25 Duct2.Fl_O 85.55 17.178 652.04 155.99 0.0000 82.06 15.230 630.07 366.9 0.4185 1.39774 +FS_3 HPC.Fl_O 85.55 88.739 1091.27 263.80 0.0000 20.55 83.167 1072.11 119.9 0.3083 1.37499 +FS_36 Bld3.Fl_O 77.85 88.739 1091.27 263.80 0.0000 18.70 83.167 1072.11 109.1 0.3083 1.37499 +FS_4 Burner.Fl_O 78.98 83.858 2030.24 521.77 0.0145 27.38 83.319 2027.09 483.4 0.0991 1.31676 +FS_45 HPT.Fl_O 86.68 30.774 1568.27 392.45 0.0132 71.97 29.016 1545.13 439.1 0.2976 1.33748 +FS_48 Duct3.Fl_O 86.68 30.620 1568.27 392.45 0.0132 72.34 28.871 1545.13 441.4 0.2976 1.33748 +FS_5 LPT.Fl_O 86.68 6.322 1081.87 264.19 0.0132 291.00 5.783 1056.29 1477.4 0.3630 1.36658 +FS_7 Duct4.Fl_O 86.68 6.259 1081.87 264.19 0.0132 293.94 5.981 1068.77 2018.9 0.2584 1.36658 +FS_9 Core_Nozz.Fl_O 86.68 6.259 1081.87 264.19 0.0132 293.94 3.458 921.04 862.9 0.9674 1.36658 +FS_15 BypBld.Fl_O 511.88 8.076 507.96 121.39 0.0000 921.85 6.963 486.87 3795.6 0.4649 1.40070 +FS_17 Duct5.Fl_O 511.88 8.015 507.96 121.39 0.0000 928.82 6.911 486.87 3824.3 0.4649 1.40070 +FS_19 Byp_Nozz.Fl_O 511.88 8.015 507.96 121.39 0.0000 928.82 4.232 423.08 2706.4 1.0000 1.40070 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1483.28 1.463 0.9104 3373.778 1.1264 0.9152 -11540.2 39.22 19.66 +LPC 154.45 2.138 0.8540 3178.819 1.2836 0.8686 -4188.7 24.96 16.46 +HPC 82.06 5.166 0.8659 6249.456 1.6736 0.8923 -13048.1 26.53 26.69 +HPT 27.38 2.725 0.9149 155.510 1.2490 0.9047 13048.2 +LPT 72.34 4.844 0.9207 79.438 1.4496 0.9037 15728.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2843.94 1.322 0.9406 0.855 2.0394 0.5215 1.4369 0.9679 3943.9586 +LPC 165.66 1.349 0.8895 0.868 1.6169 0.9323 3.2631 0.9600 3662.6571 +HPC 195.08 20.258 0.8542 0.983 2.1337 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.060 0.9332 101.567 5.0599 1.4085 0.4249 0.9803 1.5311 +LPT 150.30 6.362 0.9195 97.937 6.3617 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4388.29 15361.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 807.84 193.73 27.661 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 807.84 193.73 27.661 +Duct1 0.0025 0.3961 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 807.84 193.73 27.661 +Duct2 0.0025 0.4185 365.99 +Duct3 0.0050 0.2976 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3630 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.9941 1091.27 263.80 88.739 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.7050 1091.27 263.80 88.739 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 507.96 121.39 8.076 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9838 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7007.0 9780.3 13048.2 +LP_Shaft 3145.8 26259.8 15728.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2030.24 0.9940 0.0550 1.12988 0.01451 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.318 0.9969 1.0000 0.9975 2706.36 1.000 1006.3 18104.9 +Core_Nozz 1.810 0.9999 1.0000 0.9999 862.88 0.967 1427.1 3844.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 341 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 35000.0 0.00 550.00 4391.6 0.6510 2859.01 6.6852 827.30 12.678 1827.6 1784.8 1404.2 + core size:20.97 Q: 252.05 Maximum Thrust: 10979.3 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 550.00 5.547 450.95 107.73 0.0000 1358.70 3.458 393.85 4040.0 0.8500 1.40132 +FS_2 Inlet.Fl_O 550.00 5.519 450.95 107.73 0.0000 1365.54 4.853 434.64 5943.4 0.4324 1.40132 +FS_21 Fan.Fl_O 550.00 7.454 495.46 118.39 0.0000 1059.80 6.508 476.57 4515.2 0.4445 1.40089 +FS_13 Splitter.Fl_O2 478.44 7.454 495.46 118.39 0.0000 921.90 6.427 474.87 3795.6 0.4649 1.40089 +FS_22 Splitter.Fl_O1 71.57 7.454 495.46 118.39 0.0000 137.90 6.858 483.78 719.5 0.3470 1.40089 +FS_23 Duct1.Fl_O 71.57 7.436 495.46 118.39 0.0000 138.25 6.841 483.78 721.3 0.3470 1.40089 +FS_24 LPC.Fl_O 71.57 14.625 620.79 148.47 0.0000 78.67 13.111 601.74 366.0 0.3983 1.39865 +FS_25 Duct2.Fl_O 71.57 14.589 620.79 148.47 0.0000 78.87 13.078 601.74 366.9 0.3983 1.39865 +FS_3 HPC.Fl_O 71.57 70.327 1019.96 245.95 0.0000 20.97 65.714 1001.08 119.9 0.3150 1.37947 +FS_36 Bld3.Fl_O 65.13 70.327 1019.96 245.95 0.0000 19.08 65.714 1001.08 109.1 0.3150 1.37947 +FS_4 Burner.Fl_O 65.92 66.459 1827.65 463.40 0.0122 27.36 66.032 1824.75 483.4 0.0986 1.32611 +FS_45 HPT.Fl_O 72.36 24.185 1404.23 347.63 0.0111 72.35 22.788 1382.81 439.1 0.2981 1.34782 +FS_48 Duct3.Fl_O 72.36 24.064 1404.23 347.63 0.0111 72.71 22.674 1382.81 441.4 0.2981 1.34782 +FS_5 LPT.Fl_O 72.36 5.227 975.70 236.88 0.0111 279.03 4.821 954.42 1477.4 0.3445 1.37478 +FS_7 Duct4.Fl_O 72.36 5.175 975.70 236.88 0.0111 281.85 4.965 964.72 2018.9 0.2462 1.37478 +FS_9 Core_Nozz.Fl_O 72.36 5.175 975.70 236.88 0.0111 281.85 3.458 873.60 862.9 0.7854 1.37478 +FS_15 BypBld.Fl_O 478.44 7.454 495.46 118.39 0.0000 921.90 6.427 474.87 3795.6 0.4649 1.40089 +FS_17 Duct5.Fl_O 478.44 7.398 495.46 118.39 0.0000 928.86 6.379 474.87 3824.3 0.4649 1.40089 +FS_19 Byp_Nozz.Fl_O 478.44 7.398 495.46 118.39 0.0000 928.86 3.907 412.66 2706.4 1.0000 1.40089 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1365.54 1.351 0.9103 3063.127 1.0987 0.9141 -8292.6 46.72 21.32 +LPC 138.25 1.967 0.8429 2922.315 1.2529 0.8570 -3045.9 22.30 12.84 +HPC 78.87 4.821 0.8647 6195.341 1.6430 0.8904 -9870.6 31.68 31.92 +HPT 27.36 2.748 0.9154 158.542 1.2581 0.9047 9870.8 +LPT 72.71 4.604 0.9152 76.220 1.4392 0.8974 11338.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2618.23 1.244 0.9405 0.777 2.0717 0.5215 1.4369 0.9679 3943.9586 +LPC 148.29 1.296 0.8780 0.798 1.5321 0.9323 3.2631 0.9600 3662.6571 +HPC 187.51 18.662 0.8530 0.975 2.1688 0.4206 0.2163 1.0137 6357.1603 +HPT 30.10 5.114 0.9338 103.546 5.1141 1.4085 0.4249 0.9803 1.5311 +LPT 151.08 6.027 0.9140 93.969 6.0271 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4039.95 14142.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 762.05 182.59 22.754 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 762.05 182.59 22.754 +Duct1 0.0025 0.3470 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 762.05 182.59 22.754 +Duct2 0.0025 0.3983 365.99 +Duct3 0.0050 0.2981 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3445 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.5048 1019.96 245.95 70.327 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.9361 1019.96 245.95 70.327 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 495.46 118.39 7.454 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6852 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6777.8 7648.9 9870.8 +LP_Shaft 2856.2 20849.9 11338.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1827.65 0.9940 0.0550 0.79417 0.01219 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.140 0.9974 1.0000 0.9975 2706.36 1.000 993.8 15992.4 +Core_Nozz 1.497 0.9999 1.0000 0.9999 862.88 0.785 1130.1 2541.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 342 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 35000.0 0.00 493.24 2195.9 0.7795 1711.82 7.8780 827.30 9.102 1568.0 1533.5 1196.0 + core size:21.60 Q: 252.05 Maximum Thrust: 10979.3 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 493.24 5.547 450.95 107.73 0.0000 1218.47 3.458 393.85 3623.0 0.8500 1.40132 +FS_2 Inlet.Fl_O 493.24 5.519 450.95 107.73 0.0000 1224.60 5.000 438.38 5943.4 0.3780 1.40132 +FS_21 Fan.Fl_O 493.24 6.713 480.17 114.73 0.0000 1038.99 5.899 462.74 4515.2 0.4333 1.40109 +FS_13 Splitter.Fl_O2 437.68 6.713 480.17 114.73 0.0000 921.96 5.787 460.21 3795.6 0.4650 1.40109 +FS_22 Splitter.Fl_O1 55.56 6.713 480.17 114.73 0.0000 117.03 6.336 472.30 719.5 0.2881 1.40109 +FS_23 Duct1.Fl_O 55.56 6.696 480.17 114.73 0.0000 117.32 6.321 472.30 721.3 0.2881 1.40109 +FS_24 LPC.Fl_O 55.56 11.600 578.71 138.36 0.0000 74.35 10.544 563.15 366.0 0.3719 1.39938 +FS_25 Duct2.Fl_O 55.56 11.571 578.71 138.36 0.0000 74.53 10.517 563.15 366.9 0.3719 1.39938 +FS_3 HPC.Fl_O 55.56 50.491 925.37 222.51 0.0000 21.60 46.961 906.88 119.9 0.3250 1.38531 +FS_36 Bld3.Fl_O 50.56 50.491 925.37 222.51 0.0000 19.66 46.961 906.88 109.1 0.3250 1.38531 +FS_4 Burner.Fl_O 51.03 47.714 1568.00 390.90 0.0094 27.33 47.408 1565.44 483.4 0.0980 1.34011 +FS_45 HPT.Fl_O 56.03 17.165 1196.04 292.44 0.0086 72.85 16.160 1176.97 439.1 0.2987 1.36239 +FS_48 Duct3.Fl_O 56.03 17.079 1196.04 292.44 0.0086 73.22 16.079 1176.97 441.4 0.2987 1.36239 +FS_5 LPT.Fl_O 56.03 4.388 859.14 207.44 0.0086 241.50 4.140 845.35 1477.4 0.2915 1.38357 +FS_7 Duct4.Fl_O 56.03 4.345 859.14 207.44 0.0086 243.94 4.214 851.91 2018.9 0.2104 1.38357 +FS_9 Core_Nozz.Fl_O 56.03 4.345 859.14 207.44 0.0086 243.94 3.458 806.33 862.9 0.5832 1.38357 +FS_15 BypBld.Fl_O 437.68 6.713 480.17 114.73 0.0000 921.96 5.787 460.21 3795.6 0.4650 1.40109 +FS_17 Duct5.Fl_O 437.68 6.662 480.17 114.73 0.0000 928.93 5.744 460.21 3824.3 0.4650 1.40109 +FS_19 Byp_Nozz.Fl_O 437.68 6.662 480.17 114.73 0.0000 928.93 3.518 399.92 2706.3 1.0000 1.40109 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1224.60 1.216 0.8898 2636.870 1.0648 0.8929 -4880.9 56.77 23.91 +LPC 117.32 1.732 0.8290 2555.396 1.2052 0.8418 -1857.6 21.62 9.35 +HPC 74.53 4.364 0.8624 6112.345 1.5990 0.8871 -6614.8 39.42 40.02 +HPT 27.33 2.780 0.9164 163.050 1.2710 0.9053 6614.9 +LPT 73.22 3.892 0.9117 71.094 1.3921 0.8951 6738.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2348.00 1.150 0.9193 0.669 2.2449 0.5215 1.4369 0.9679 3943.9586 +LPC 125.84 1.224 0.8636 0.698 1.4764 0.9323 3.2631 0.9600 3662.6571 +HPC 177.19 16.549 0.8508 0.961 2.2574 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.189 0.9348 106.491 5.1887 1.4085 0.4249 0.9803 1.5311 +LPT 152.13 5.034 0.9105 87.651 5.0340 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3622.99 12682.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 701.02 167.81 17.273 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 701.02 167.81 17.273 +Duct1 0.0025 0.2881 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 701.02 167.81 17.273 +Duct2 0.0025 0.3719 365.99 +Duct3 0.0050 0.2987 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2915 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.9445 925.37 222.51 50.491 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.0557 925.37 222.51 50.491 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 480.17 114.73 6.713 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8780 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6456.5 5381.0 6614.9 +LP_Shaft 2458.7 14394.7 6738.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1568.00 0.9940 0.0550 0.47550 0.00941 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.927 0.9975 1.0000 0.9975 2706.36 1.000 978.3 13472.1 +Core_Nozz 1.256 0.9999 1.0000 0.9999 862.88 0.583 807.7 1406.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 343 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 10/ 30/ 2/ 7 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 35000.0 0.00 439.03 548.9 1.5943 875.18 9.7719 827.30 6.036 1283.7 1258.3 971.9 + core size:22.50 Q: 252.05 Maximum Thrust: 10979.3 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 439.03 5.547 450.95 107.73 0.0000 1084.55 3.458 393.85 3224.8 0.8500 1.40132 +FS_2 Inlet.Fl_O 439.03 5.519 450.95 107.73 0.0000 1090.01 5.118 441.32 5943.4 0.3298 1.40132 +FS_21 Fan.Fl_O 439.03 6.049 466.18 111.38 0.0000 1011.21 5.361 450.34 4515.2 0.4187 1.40123 +FS_13 Splitter.Fl_O2 398.27 6.049 466.18 111.38 0.0000 917.34 5.225 447.05 3795.6 0.4619 1.40123 +FS_22 Splitter.Fl_O1 40.76 6.049 466.18 111.38 0.0000 93.88 5.836 461.42 719.5 0.2268 1.40123 +FS_23 Duct1.Fl_O 40.76 6.034 466.18 111.38 0.0000 94.11 5.821 461.42 721.3 0.2268 1.40123 +FS_24 LPC.Fl_O 40.76 8.866 532.73 127.32 0.0000 68.47 8.194 520.85 366.0 0.3375 1.40025 +FS_25 Duct2.Fl_O 40.76 8.844 532.73 127.32 0.0000 68.64 8.173 520.85 366.9 0.3375 1.40025 +FS_3 HPC.Fl_O 40.76 33.480 820.19 196.73 0.0000 22.50 30.922 802.05 119.9 0.3398 1.39098 +FS_36 Bld3.Fl_O 37.09 33.480 820.19 196.73 0.0000 20.47 30.922 802.05 109.1 0.3398 1.39098 +FS_4 Burner.Fl_O 37.33 31.639 1283.68 314.59 0.0066 27.28 31.436 1281.51 483.4 0.0972 1.35825 +FS_45 HPT.Fl_O 41.00 11.247 971.90 235.05 0.0060 73.33 10.580 955.69 439.1 0.2991 1.37840 +FS_48 Duct3.Fl_O 41.00 11.191 971.90 235.05 0.0060 73.70 10.527 955.69 441.4 0.2991 1.37840 +FS_5 LPT.Fl_O 41.00 3.906 749.37 180.16 0.0060 185.40 3.779 742.45 1477.4 0.2185 1.39063 +FS_7 Duct4.Fl_O 41.00 3.867 749.37 180.16 0.0060 187.27 3.800 745.67 2018.9 0.1594 1.39063 +FS_9 Core_Nozz.Fl_O 41.00 3.867 749.37 180.16 0.0060 187.27 3.458 726.17 862.9 0.4042 1.39063 +FS_15 BypBld.Fl_O 398.27 6.049 466.18 111.38 0.0000 917.34 5.225 447.05 3795.6 0.4619 1.40123 +FS_17 Duct5.Fl_O 398.27 6.004 466.18 111.38 0.0000 924.27 5.186 447.05 3824.3 0.4619 1.40123 +FS_19 Byp_Nozz.Fl_O 398.27 6.004 466.18 111.38 0.0000 924.27 3.458 398.04 2706.4 0.9237 1.40123 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1090.01 1.096 0.7872 2117.340 1.0338 0.7901 -2264.6 79.80 26.29 +LPC 94.11 1.469 0.8156 2082.467 1.1427 0.8254 -919.3 24.84 7.48 +HPC 68.64 3.786 0.8519 6004.743 1.5396 0.8764 -4002.7 51.16 52.20 +HPT 27.28 2.813 0.9180 169.852 1.2867 0.9067 4002.7 +LPT 73.70 2.865 0.9028 63.329 1.2970 0.8889 3184.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2089.95 1.067 0.8133 0.537 2.6266 0.5215 1.4369 0.9679 3943.9586 +LPC 100.95 1.144 0.8495 0.569 1.4939 0.9323 3.2631 0.9600 3662.6571 +HPC 163.17 13.877 0.8404 0.945 2.3887 0.4206 0.2163 1.0137 6357.1603 +HPT 30.01 5.267 0.9365 110.934 5.2670 1.4085 0.4249 0.9803 1.5311 +LPT 153.14 3.601 0.9017 78.076 3.6014 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3224.80 11288.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 633.86 151.62 12.453 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 633.86 151.62 12.453 +Duct1 0.0025 0.2268 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 633.86 151.62 12.453 +Duct2 0.0025 0.3375 365.99 +Duct3 0.0050 0.2991 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2185 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.4265 820.19 196.73 33.480 +Duct5 0.0075 0.4619 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.2416 820.19 196.73 33.480 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 466.18 111.38 6.049 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.7719 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6085.6 3454.5 4002.7 +LP_Shaft 1974.3 8470.1 3184.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1283.68 0.9940 0.0550 0.24311 0.00655 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.736 0.9975 1.0000 0.9975 2706.36 0.924 901.5 11159.5 +Core_Nozz 1.118 0.9999 1.0000 0.9999 862.88 0.404 532.3 678.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 344 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.900 35000.0 0.00 706.13 11333.3 0.6480 7343.65 5.0410 875.96 22.715 2421.5 2360.0 1891.0 + core size:19.94 Q: 282.57 Maximum Thrust: 11333.3 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 706.13 5.850 457.87 109.39 0.0000 1666.72 3.458 393.85 4898.6 0.9000 1.40129 +FS_2 Inlet.Fl_O 706.13 5.821 457.87 109.39 0.0000 1675.11 4.646 429.26 5943.4 0.5763 1.40129 +FS_21 Fan.Fl_O 706.13 9.572 538.61 128.73 0.0000 1104.74 8.229 515.83 4515.2 0.4696 1.40014 +FS_13 Splitter.Fl_O2 589.24 9.572 538.61 128.73 0.0000 921.87 8.253 516.25 3795.6 0.4650 1.40014 +FS_22 Splitter.Fl_O1 116.89 9.572 538.61 128.73 0.0000 182.87 8.098 513.45 719.5 0.4946 1.40014 +FS_23 Duct1.Fl_O 116.89 9.548 538.61 128.73 0.0000 183.33 8.077 513.45 721.3 0.4946 1.40014 +FS_24 LPC.Fl_O 116.89 23.764 722.58 173.03 0.0000 85.32 20.793 695.73 366.0 0.4415 1.39527 +FS_25 Duct2.Fl_O 116.89 23.705 722.58 173.03 0.0000 85.53 20.741 695.73 366.9 0.4415 1.39527 +FS_3 HPC.Fl_O 116.89 132.878 1233.49 299.86 0.0000 19.94 125.057 1213.58 119.9 0.2991 1.36604 +FS_36 Bld3.Fl_O 106.37 132.878 1233.49 299.86 0.0000 18.14 125.057 1213.58 109.1 0.2991 1.36604 +FS_4 Burner.Fl_O 108.41 125.569 2421.55 638.48 0.0192 27.41 124.759 2417.91 483.4 0.0997 1.30245 +FS_45 HPT.Fl_O 118.93 47.056 1891.00 483.86 0.0175 70.92 44.449 1865.02 439.1 0.2948 1.31993 +FS_48 Duct3.Fl_O 118.93 46.821 1891.00 483.86 0.0175 71.28 44.227 1865.02 441.4 0.2948 1.31993 +FS_5 LPT.Fl_O 118.93 9.597 1313.43 325.47 0.0175 289.81 8.786 1283.70 1477.4 0.3637 1.34904 +FS_7 Duct4.Fl_O 118.93 9.501 1313.43 325.47 0.0175 292.73 9.083 1298.21 2018.9 0.2590 1.34904 +FS_9 Core_Nozz.Fl_O 118.93 9.501 1313.43 325.47 0.0175 292.73 5.077 1114.49 862.9 1.0000 1.34904 +FS_15 BypBld.Fl_O 589.24 9.572 538.61 128.73 0.0000 921.87 8.253 516.25 3795.6 0.4650 1.40014 +FS_17 Duct5.Fl_O 589.24 9.500 538.61 128.73 0.0000 928.83 8.191 516.25 3824.3 0.4650 1.40014 +FS_19 Byp_Nozz.Fl_O 589.24 9.500 538.61 128.73 0.0000 928.83 5.017 448.65 2706.3 1.0000 1.40014 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.645 0.8675 3944.235 1.1763 0.8766 -19325.9 24.71 17.45 +LPC 183.33 2.489 0.8683 3636.611 1.3416 0.8839 -7325.3 28.35 23.26 +HPC 85.53 5.606 0.8652 6325.033 1.7071 0.8922 -20976.4 20.12 20.18 +HPT 27.41 2.668 0.9134 151.710 1.2327 0.9036 20976.8 +LPT 71.28 4.879 0.9324 85.220 1.4397 0.9182 26651.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8963 1.000 2.3707 0.5215 1.4369 0.9679 3943.9586 +LPC 196.64 1.456 0.9045 0.993 1.7657 0.9323 3.2631 0.9600 3662.6571 +HPC 203.33 22.291 0.8535 0.995 2.0420 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.927 0.9317 99.084 4.9270 1.4085 0.4249 0.9803 1.5311 +LPT 148.10 6.411 0.9312 105.066 6.4107 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4898.56 19224.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 904.67 217.42 39.698 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 904.67 217.42 39.698 +Duct1 0.0025 0.4946 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 904.67 217.42 39.698 +Duct2 0.0025 0.4415 365.99 +Duct3 0.0050 0.2948 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3637 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 4.0911 1233.49 299.86 132.878 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.4289 1233.49 299.86 132.878 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 538.61 128.73 9.572 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0410 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7465.5 14757.5 20976.8 +LP_Shaft 3705.8 37771.4 26651.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2421.55 0.9940 0.0550 2.03990 0.01918 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.748 0.9942 1.0000 0.9975 2706.36 1.000 1036.2 23196.1 +Core_Nozz 2.748 0.9955 1.0000 0.9999 862.88 1.000 1613.7 7362.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 345 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.900 35000.0 0.00 688.48 10199.5 0.6373 6500.36 5.3033 875.96 20.825 2334.6 2275.6 1816.5 + core size:20.03 Q: 282.57 Maximum Thrust: 11333.3 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 688.48 5.850 457.87 109.39 0.0000 1625.07 3.458 393.85 4776.2 0.9000 1.40129 +FS_2 Inlet.Fl_O 688.48 5.821 457.87 109.39 0.0000 1633.25 4.724 431.31 5943.4 0.5539 1.40129 +FS_21 Fan.Fl_O 688.48 9.356 532.52 127.27 0.0000 1095.72 8.070 510.46 4515.2 0.4645 1.40026 +FS_13 Splitter.Fl_O2 579.26 9.356 532.52 127.27 0.0000 921.88 8.067 510.41 3795.6 0.4650 1.40026 +FS_22 Splitter.Fl_O1 109.23 9.356 532.52 127.27 0.0000 173.83 8.084 510.71 719.5 0.4617 1.40026 +FS_23 Duct1.Fl_O 109.23 9.333 532.52 127.27 0.0000 174.27 8.063 510.71 721.3 0.4617 1.40026 +FS_24 LPC.Fl_O 109.23 21.756 700.26 167.63 0.0000 85.73 19.005 673.90 366.0 0.4441 1.39600 +FS_25 Duct2.Fl_O 109.23 21.701 700.26 167.63 0.0000 85.94 18.958 673.90 366.9 0.4441 1.39600 +FS_3 HPC.Fl_O 109.23 121.825 1198.47 290.93 0.0000 20.03 114.584 1178.85 119.9 0.3004 1.36824 +FS_36 Bld3.Fl_O 99.40 121.825 1198.47 290.93 0.0000 18.23 114.584 1178.85 109.1 0.3004 1.36824 +FS_4 Burner.Fl_O 101.20 115.124 2334.65 612.16 0.0182 27.41 114.382 2331.12 483.4 0.0996 1.30536 +FS_45 HPT.Fl_O 111.03 42.716 1816.53 462.43 0.0165 71.49 40.309 1790.92 439.1 0.2970 1.32362 +FS_48 Duct3.Fl_O 111.03 42.503 1816.53 462.43 0.0165 71.85 40.108 1790.92 441.4 0.2970 1.32362 +FS_5 LPT.Fl_O 111.03 8.776 1262.73 311.84 0.0165 290.12 8.032 1233.85 1477.4 0.3636 1.35282 +FS_7 Duct4.Fl_O 111.03 8.688 1262.73 311.84 0.0165 293.05 8.305 1247.94 2018.9 0.2589 1.35282 +FS_9 Core_Nozz.Fl_O 111.03 8.688 1262.73 311.84 0.0165 293.05 4.638 1069.82 862.9 1.0000 1.35282 +FS_15 BypBld.Fl_O 579.26 9.356 532.52 127.27 0.0000 921.88 8.067 510.41 3795.6 0.4650 1.40026 +FS_17 Duct5.Fl_O 579.26 9.286 532.52 127.27 0.0000 928.85 8.007 510.41 3824.3 0.4650 1.40026 +FS_19 Byp_Nozz.Fl_O 579.26 9.286 532.52 127.27 0.0000 928.85 4.903 443.56 2706.4 1.0000 1.40026 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1633.25 1.608 0.8924 3743.170 1.1630 0.8995 -17419.7 28.20 17.74 +LPC 174.27 2.331 0.8660 3470.913 1.3150 0.8809 -6237.0 28.87 22.16 +HPC 85.94 5.614 0.8641 6335.405 1.7115 0.8915 -19053.7 20.52 20.55 +HPT 27.41 2.695 0.9139 152.352 1.2375 0.9040 19053.7 +LPT 71.85 4.843 0.9279 82.517 1.4386 0.9127 23656.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3131.37 1.423 0.9220 0.949 2.1758 0.5215 1.4369 0.9679 3943.9586 +LPC 186.92 1.408 0.9021 0.948 1.7517 0.9323 3.2631 0.9600 3662.6571 +HPC 204.32 22.328 0.8524 0.997 2.0710 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.990 0.9322 99.504 4.9896 1.4085 0.4249 0.9803 1.5311 +LPT 149.28 6.361 0.9267 101.733 6.3612 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4776.16 18744.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 877.64 210.78 36.369 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 877.64 210.78 36.369 +Duct1 0.0025 0.4617 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 877.64 210.78 36.369 +Duct2 0.0025 0.4441 365.99 +Duct3 0.0050 0.2970 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.8229 1198.47 290.93 121.825 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 6.0074 1198.47 290.93 121.825 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 532.52 127.27 9.356 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3033 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7361.4 13594.2 19053.7 +LP_Shaft 3516.9 35328.3 23656.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2334.65 0.9940 0.0550 1.80565 0.01817 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.686 0.9947 1.0000 0.9975 2706.36 1.000 1030.3 22462.6 +Core_Nozz 2.513 0.9976 1.0000 0.9999 862.88 1.000 1583.1 6481.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 346 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.900 35000.0 0.00 668.44 9066.7 0.6325 5734.27 5.5081 875.96 19.188 2244.6 2188.4 1742.1 + core size:20.18 Q: 282.57 Maximum Thrust: 11333.3 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 668.44 5.850 457.87 109.39 0.0000 1577.77 3.458 393.85 4637.1 0.9000 1.40129 +FS_2 Inlet.Fl_O 668.44 5.821 457.87 109.39 0.0000 1585.71 4.806 433.44 5943.4 0.5299 1.40129 +FS_21 Fan.Fl_O 668.44 9.090 526.92 125.93 0.0000 1089.22 7.858 505.42 4515.2 0.4608 1.40037 +FS_13 Splitter.Fl_O2 565.73 9.090 526.92 125.93 0.0000 921.85 7.838 505.04 3795.6 0.4650 1.40037 +FS_22 Splitter.Fl_O1 102.71 9.090 526.92 125.93 0.0000 167.36 7.960 507.30 719.5 0.4394 1.40037 +FS_23 Duct1.Fl_O 102.71 9.067 526.92 125.93 0.0000 167.78 7.941 507.30 721.3 0.4394 1.40037 +FS_24 LPC.Fl_O 102.71 20.461 686.38 164.28 0.0000 84.86 17.936 661.17 366.0 0.4383 1.39648 +FS_25 Duct2.Fl_O 102.71 20.410 686.38 164.28 0.0000 85.07 17.891 661.17 366.9 0.4383 1.39648 +FS_3 HPC.Fl_O 102.71 112.245 1168.34 283.26 0.0000 20.18 105.463 1148.81 119.9 0.3027 1.37014 +FS_36 Bld3.Fl_O 93.47 112.245 1168.34 283.26 0.0000 18.37 105.463 1148.81 109.1 0.3027 1.37014 +FS_4 Burner.Fl_O 95.06 106.072 2244.58 585.08 0.0170 27.40 105.388 2241.16 483.4 0.0994 1.30855 +FS_45 HPT.Fl_O 104.30 39.165 1742.05 441.16 0.0155 71.73 36.943 1717.09 439.1 0.2976 1.32758 +FS_48 Duct3.Fl_O 104.30 38.969 1742.05 441.16 0.0155 72.09 36.758 1717.09 441.4 0.2976 1.32758 +FS_5 LPT.Fl_O 104.30 8.054 1208.52 297.39 0.0155 290.53 7.369 1180.58 1477.4 0.3636 1.35693 +FS_7 Duct4.Fl_O 104.30 7.973 1208.52 297.39 0.0155 293.46 7.620 1194.22 2018.9 0.2589 1.35693 +FS_9 Core_Nozz.Fl_O 104.30 7.973 1208.52 297.39 0.0155 293.46 4.253 1022.21 862.9 1.0000 1.35693 +FS_15 BypBld.Fl_O 565.73 9.090 526.92 125.93 0.0000 921.85 7.838 505.04 3795.6 0.4650 1.40037 +FS_17 Duct5.Fl_O 565.73 9.022 526.92 125.93 0.0000 928.82 7.779 505.04 3824.3 0.4650 1.40037 +FS_19 Byp_Nozz.Fl_O 565.73 9.022 526.92 125.93 0.0000 928.82 4.764 438.89 2706.4 1.0000 1.40037 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1585.71 1.562 0.9023 3614.214 1.1508 0.9083 -15643.6 31.66 18.33 +LPC 167.78 2.257 0.8631 3369.085 1.3026 0.8778 -5572.6 28.05 20.49 +HPC 85.07 5.499 0.8648 6312.869 1.7022 0.8920 -17291.1 22.14 22.22 +HPT 27.40 2.708 0.9145 153.284 1.2414 0.9045 17291.0 +LPT 72.09 4.839 0.9259 81.360 1.4415 0.9101 21216.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3040.41 1.391 0.9322 0.916 2.0969 0.5215 1.4369 0.9679 3943.9586 +LPC 179.97 1.385 0.8991 0.920 1.7162 0.9323 3.2631 0.9600 3662.6571 +HPC 202.25 21.800 0.8532 0.993 2.0972 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.021 0.9328 100.113 5.0207 1.4085 0.4249 0.9803 1.5311 +LPT 149.79 6.355 0.9247 100.306 6.3549 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4637.14 18198.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 857.80 205.92 33.864 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 857.80 205.92 33.864 +Duct1 0.0025 0.4394 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 857.80 205.92 33.864 +Duct2 0.0025 0.4383 365.99 +Duct3 0.0050 0.2976 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.5948 1168.34 283.26 112.245 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.6490 1168.34 283.26 112.245 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 526.92 125.93 9.090 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5081 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7262.1 12505.1 17291.0 +LP_Shaft 3395.8 32814.7 21216.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2244.58 0.9940 0.0550 1.59285 0.01704 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.609 0.9953 1.0000 0.9975 2706.36 1.000 1024.9 21555.9 +Core_Nozz 2.306 0.9989 1.0000 0.9999 862.88 1.000 1549.6 5709.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 347 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.900 35000.0 0.00 625.26 6799.9 0.6368 4330.44 5.9862 875.96 15.987 2059.1 2009.1 1591.8 + core size:20.55 Q: 282.57 Maximum Thrust: 11333.3 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 625.26 5.850 457.87 109.39 0.0000 1475.85 3.458 393.85 4337.6 0.9000 1.40129 +FS_2 Inlet.Fl_O 625.26 5.821 457.87 109.39 0.0000 1483.28 4.964 437.45 5943.4 0.4822 1.40129 +FS_21 Fan.Fl_O 625.26 8.517 515.76 123.25 0.0000 1075.84 7.396 495.35 4515.2 0.4534 1.40057 +FS_13 Splitter.Fl_O2 535.76 8.517 515.76 123.25 0.0000 921.85 7.343 494.34 3795.6 0.4650 1.40057 +FS_22 Splitter.Fl_O1 89.50 8.517 515.76 123.25 0.0000 154.00 7.644 500.05 719.5 0.3959 1.40057 +FS_23 Duct1.Fl_O 89.50 8.496 515.76 123.25 0.0000 154.38 7.625 500.05 721.3 0.3959 1.40057 +FS_24 LPC.Fl_O 89.50 18.170 662.11 158.42 0.0000 81.79 16.113 639.86 366.0 0.4181 1.39737 +FS_25 Duct2.Fl_O 89.50 18.125 662.11 158.42 0.0000 81.99 16.073 639.86 366.9 0.4181 1.39737 +FS_3 HPC.Fl_O 89.50 93.524 1107.05 267.77 0.0000 20.55 87.653 1087.66 119.9 0.3084 1.37400 +FS_36 Bld3.Fl_O 81.44 93.524 1107.05 267.77 0.0000 18.70 87.653 1087.66 109.1 0.3084 1.37400 +FS_4 Burner.Fl_O 82.65 88.380 2059.09 530.15 0.0148 27.38 87.811 2055.91 483.4 0.0991 1.31561 +FS_45 HPT.Fl_O 90.70 32.446 1591.82 398.95 0.0134 71.97 30.592 1568.40 439.1 0.2977 1.33613 +FS_48 Duct3.Fl_O 90.70 32.283 1591.82 398.95 0.0134 72.33 30.439 1568.40 441.4 0.2977 1.33613 +FS_5 LPT.Fl_O 90.70 6.663 1099.18 268.67 0.0134 291.21 6.095 1073.21 1477.4 0.3634 1.36531 +FS_7 Duct4.Fl_O 90.70 6.597 1099.18 268.67 0.0134 294.15 6.304 1085.88 2018.9 0.2587 1.36531 +FS_9 Core_Nozz.Fl_O 90.70 6.597 1099.18 268.67 0.0134 294.15 3.512 926.65 862.9 1.0000 1.36531 +FS_15 BypBld.Fl_O 535.76 8.517 515.76 123.25 0.0000 921.85 7.343 494.34 3795.6 0.4650 1.40057 +FS_17 Duct5.Fl_O 535.76 8.453 515.76 123.25 0.0000 928.81 7.288 494.34 3824.3 0.4650 1.40057 +FS_19 Byp_Nozz.Fl_O 535.76 8.453 515.76 123.25 0.0000 928.81 4.463 429.58 2706.4 1.0000 1.40057 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1483.28 1.463 0.9105 3373.896 1.1264 0.9152 -12265.8 39.21 19.65 +LPC 154.38 2.139 0.8538 3178.917 1.2838 0.8685 -4453.1 24.88 16.41 +HPC 81.99 5.160 0.8659 6248.231 1.6720 0.8923 -13846.9 26.59 26.75 +HPT 27.38 2.724 0.9149 155.574 1.2481 0.9046 13847.0 +LPT 72.33 4.845 0.9207 79.453 1.4482 0.9038 16718.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2843.95 1.322 0.9406 0.855 2.0391 0.5215 1.4369 0.9679 3943.9586 +LPC 165.59 1.349 0.8894 0.868 1.6149 0.9323 3.2631 0.9600 3662.6571 +HPC 194.92 20.231 0.8543 0.983 2.1334 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.057 0.9332 101.608 5.0575 1.4085 0.4249 0.9803 1.5311 +LPT 150.30 6.363 0.9195 97.956 6.3634 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4337.60 17023.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 820.02 196.69 29.171 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 820.02 196.69 29.171 +Duct1 0.0025 0.3959 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 820.02 196.69 29.171 +Duct2 0.0025 0.4181 365.99 +Duct3 0.0050 0.2977 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3634 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.1325 1107.05 267.77 93.524 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.9225 1107.05 267.77 93.524 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 515.76 123.25 8.517 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9862 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7059.5 10301.9 13847.0 +LP_Shaft 3170.0 27700.2 16718.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2059.09 0.9940 0.0550 1.20290 0.01477 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.445 0.9963 1.0000 0.9975 2706.36 1.000 1014.0 19606.1 +Core_Nozz 1.908 0.9999 1.0000 0.9999 862.88 1.000 1479.4 4217.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 348 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 8/ 18/ 1/ 6 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.900 35000.0 0.00 576.77 4533.3 0.6707 3040.29 6.6837 875.96 12.696 1851.9 1808.6 1424.0 + core size:20.99 Q: 282.57 Maximum Thrust: 11333.3 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 576.77 5.850 457.87 109.39 0.0000 1361.38 3.458 393.85 4001.2 0.9000 1.40129 +FS_2 Inlet.Fl_O 576.77 5.821 457.87 109.39 0.0000 1368.23 5.115 441.23 5943.4 0.4335 1.40129 +FS_21 Fan.Fl_O 576.77 7.879 503.41 120.29 0.0000 1059.79 6.879 484.22 4515.2 0.4445 1.40077 +FS_13 Splitter.Fl_O2 501.70 7.879 503.41 120.29 0.0000 921.87 6.794 482.49 3795.6 0.4649 1.40077 +FS_22 Splitter.Fl_O1 75.06 7.879 503.41 120.29 0.0000 137.93 7.249 491.53 719.5 0.3471 1.40077 +FS_23 Duct1.Fl_O 75.06 7.860 503.41 120.29 0.0000 138.27 7.231 491.53 721.3 0.3471 1.40077 +FS_24 LPC.Fl_O 75.06 15.523 631.66 151.09 0.0000 78.43 13.927 612.43 366.0 0.3968 1.39838 +FS_25 Duct2.Fl_O 75.06 15.484 631.66 151.09 0.0000 78.62 13.893 612.43 366.9 0.3968 1.39838 +FS_3 HPC.Fl_O 75.06 74.272 1035.64 249.86 0.0000 20.99 69.391 1016.47 119.9 0.3153 1.37849 +FS_36 Bld3.Fl_O 68.31 74.272 1035.64 249.86 0.0000 19.10 69.391 1016.47 109.1 0.3153 1.37849 +FS_4 Burner.Fl_O 69.15 70.187 1851.85 470.24 0.0124 27.36 69.736 1848.93 483.4 0.0987 1.32499 +FS_45 HPT.Fl_O 75.91 25.560 1424.04 352.95 0.0113 72.32 24.086 1402.39 439.1 0.2981 1.34657 +FS_48 Duct3.Fl_O 75.91 25.433 1424.04 352.95 0.0113 72.68 23.965 1402.39 441.4 0.2981 1.34657 +FS_5 LPT.Fl_O 75.91 5.431 986.56 239.64 0.0113 283.27 4.996 964.33 1477.4 0.3507 1.37398 +FS_7 Duct4.Fl_O 75.91 5.377 986.56 239.64 0.0113 286.13 5.152 975.12 2018.9 0.2503 1.37398 +FS_9 Core_Nozz.Fl_O 75.91 5.377 986.56 239.64 0.0113 286.13 3.458 874.17 862.9 0.8242 1.37398 +FS_15 BypBld.Fl_O 501.70 7.879 503.41 120.29 0.0000 921.87 6.794 482.49 3795.6 0.4649 1.40077 +FS_17 Duct5.Fl_O 501.70 7.820 503.41 120.29 0.0000 928.83 6.743 482.49 3824.3 0.4649 1.40077 +FS_19 Byp_Nozz.Fl_O 501.70 7.820 503.41 120.29 0.0000 928.83 4.129 419.28 2706.4 1.0000 1.40077 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1368.23 1.354 0.9105 3071.331 1.0995 0.9143 -8898.8 46.48 21.24 +LPC 138.27 1.975 0.8422 2929.127 1.2548 0.8564 -3270.3 21.90 12.64 +HPC 78.62 4.797 0.8647 6190.443 1.6396 0.8904 -10490.5 32.00 32.27 +HPT 27.36 2.746 0.9155 158.750 1.2571 0.9048 10490.5 +LPT 72.68 4.683 0.9147 76.470 1.4434 0.8966 12169.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2623.40 1.246 0.9407 0.779 2.0685 0.5215 1.4369 0.9679 3943.9586 +LPC 148.32 1.299 0.8772 0.800 1.5233 0.9323 3.2631 0.9600 3662.6571 +HPC 186.91 18.552 0.8531 0.974 2.1712 0.4206 0.2163 1.0137 6357.1603 +HPT 30.10 5.109 0.9338 103.682 5.1092 1.4085 0.4249 0.9803 1.5311 +LPT 151.02 6.137 0.9135 94.278 6.1371 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4001.15 15702.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 774.68 185.66 24.096 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 774.68 185.66 24.096 +Duct1 0.0025 0.3471 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 774.68 185.66 24.096 +Duct2 0.0025 0.3968 365.99 +Duct3 0.0050 0.2981 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3507 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.6272 1035.64 249.86 74.272 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.1285 1035.64 249.86 74.272 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 503.41 120.29 7.879 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6837 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6831.5 8065.1 10490.5 +LP_Shaft 2885.7 22148.4 12169.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1851.85 0.9940 0.0550 0.84452 0.01236 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.262 0.9971 1.0000 0.9975 2706.36 1.000 1001.7 17437.5 +Core_Nozz 1.555 0.9999 1.0000 0.9999 862.88 0.824 1186.3 2798.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 349 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.900 35000.0 0.00 518.13 2266.7 0.8016 1816.88 7.8696 875.96 9.133 1587.4 1552.6 1211.9 + core size:21.64 Q: 282.57 Maximum Thrust: 11333.3 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 518.13 5.850 457.87 109.39 0.0000 1222.97 3.458 393.85 3594.4 0.9000 1.40129 +FS_2 Inlet.Fl_O 518.13 5.821 457.87 109.39 0.0000 1229.13 5.269 445.00 5943.4 0.3797 1.40129 +FS_21 Fan.Fl_O 518.13 7.109 488.12 116.63 0.0000 1039.09 6.247 470.40 4515.2 0.4334 1.40099 +FS_13 Splitter.Fl_O2 459.71 7.109 488.12 116.63 0.0000 921.94 6.129 467.83 3795.6 0.4650 1.40099 +FS_22 Splitter.Fl_O1 58.42 7.109 488.12 116.63 0.0000 117.15 6.710 480.11 719.5 0.2884 1.40099 +FS_23 Duct1.Fl_O 58.42 7.091 488.12 116.63 0.0000 117.45 6.693 480.11 721.3 0.2884 1.40099 +FS_24 LPC.Fl_O 58.42 12.378 589.96 141.06 0.0000 73.97 11.264 574.29 366.0 0.3696 1.39920 +FS_25 Duct2.Fl_O 58.42 12.347 589.96 141.06 0.0000 74.15 11.236 574.29 366.9 0.3696 1.39920 +FS_3 HPC.Fl_O 58.42 53.427 940.54 226.25 0.0000 21.64 49.677 921.70 119.9 0.3257 1.38438 +FS_36 Bld3.Fl_O 53.16 53.427 940.54 226.25 0.0000 19.69 49.677 921.70 109.1 0.3257 1.38438 +FS_4 Burner.Fl_O 53.66 50.489 1587.41 396.19 0.0095 27.33 50.165 1584.82 483.4 0.0980 1.33907 +FS_45 HPT.Fl_O 58.92 18.179 1211.94 296.56 0.0086 72.81 17.115 1192.68 439.1 0.2987 1.36133 +FS_48 Duct3.Fl_O 58.92 18.088 1211.94 296.56 0.0086 73.18 17.030 1192.68 441.4 0.2987 1.36133 +FS_5 LPT.Fl_O 58.92 4.491 863.97 208.64 0.0086 248.82 4.220 849.17 1477.4 0.3014 1.38326 +FS_7 Duct4.Fl_O 58.92 4.446 863.97 208.64 0.0086 251.34 4.304 856.23 2018.9 0.2172 1.38326 +FS_9 Core_Nozz.Fl_O 58.92 4.446 863.97 208.64 0.0086 251.34 3.458 805.67 862.9 0.6130 1.38326 +FS_15 BypBld.Fl_O 459.71 7.109 488.12 116.63 0.0000 921.94 6.129 467.83 3795.6 0.4650 1.40099 +FS_17 Duct5.Fl_O 459.71 7.056 488.12 116.63 0.0000 928.90 6.083 467.83 3824.3 0.4650 1.40099 +FS_19 Byp_Nozz.Fl_O 459.71 7.056 488.12 116.63 0.0000 928.90 3.726 406.55 2706.4 1.0000 1.40099 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1229.13 1.221 0.8916 2653.883 1.0661 0.8947 -5310.1 56.14 23.75 +LPC 117.45 1.746 0.8275 2570.326 1.2086 0.8405 -2019.0 20.77 9.05 +HPC 74.15 4.327 0.8622 6105.306 1.5943 0.8868 -7041.2 40.04 40.67 +HPT 27.33 2.777 0.9165 163.428 1.2701 0.9054 7041.2 +LPT 73.18 4.027 0.9115 71.625 1.4028 0.8944 7329.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2356.68 1.154 0.9211 0.673 2.2332 0.5215 1.4369 0.9679 3943.9586 +LPC 125.98 1.228 0.8620 0.702 1.4593 0.9323 3.2631 0.9600 3662.6571 +HPC 176.29 16.381 0.8506 0.960 2.2646 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.183 0.9349 106.738 5.1832 1.4085 0.4249 0.9803 1.5311 +LPT 152.06 5.223 0.9103 88.305 5.2229 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3594.36 14106.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 713.70 170.88 18.365 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 713.70 170.88 18.365 +Duct1 0.0025 0.2884 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 713.70 170.88 18.365 +Duct2 0.0025 0.3696 365.99 +Duct3 0.0050 0.2987 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3014 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.0446 940.54 226.25 53.427 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.2129 940.54 226.25 53.427 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 488.12 116.63 7.109 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8696 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6511.4 5679.5 7041.2 +LP_Shaft 2493.5 15437.5 7329.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1587.41 0.9940 0.0550 0.50469 0.00949 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.040 0.9975 1.0000 0.9975 2706.36 1.000 986.4 14818.9 +Core_Nozz 1.286 0.9999 1.0000 0.9999 862.88 0.613 848.7 1554.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 350 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 10/ 30/ 2/ 7 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.900 35000.0 0.00 463.19 566.7 1.6401 929.41 9.7801 875.96 6.075 1300.8 1275.3 985.7 + core size:22.55 Q: 282.57 Maximum Thrust: 11333.3 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 463.19 5.850 457.87 109.39 0.0000 1093.29 3.458 393.85 3213.2 0.9000 1.40129 +FS_2 Inlet.Fl_O 463.19 5.821 457.87 109.39 0.0000 1098.79 5.390 447.91 5943.4 0.3328 1.40129 +FS_21 Fan.Fl_O 463.19 6.406 473.93 113.23 0.0000 1015.71 5.670 457.65 4515.2 0.4210 1.40116 +FS_13 Splitter.Fl_O2 420.22 6.406 473.93 113.23 0.0000 921.49 5.524 454.25 3795.6 0.4646 1.40116 +FS_22 Splitter.Fl_O1 42.97 6.406 473.93 113.23 0.0000 94.22 6.179 469.05 719.5 0.2277 1.40116 +FS_23 Duct1.Fl_O 42.97 6.390 473.93 113.23 0.0000 94.46 6.163 469.05 721.3 0.2277 1.40116 +FS_24 LPC.Fl_O 42.97 9.501 543.95 130.02 0.0000 68.06 8.790 531.99 366.0 0.3352 1.40003 +FS_25 Duct2.Fl_O 42.97 9.478 543.95 130.02 0.0000 68.23 8.768 531.99 366.9 0.3352 1.40003 +FS_3 HPC.Fl_O 42.97 35.535 835.02 200.35 0.0000 22.55 32.807 816.49 119.9 0.3408 1.39029 +FS_36 Bld3.Fl_O 39.10 35.535 835.02 200.35 0.0000 20.52 32.807 816.49 109.1 0.3408 1.39029 +FS_4 Burner.Fl_O 39.36 33.580 1300.76 319.05 0.0066 27.28 33.366 1298.56 483.4 0.0972 1.35716 +FS_45 HPT.Fl_O 43.22 11.945 985.73 238.51 0.0060 73.31 11.237 969.33 439.1 0.2991 1.37750 +FS_48 Duct3.Fl_O 43.22 11.886 985.73 238.51 0.0060 73.68 11.181 969.33 441.4 0.2991 1.37750 +FS_5 LPT.Fl_O 43.22 3.954 751.26 180.62 0.0060 193.34 3.814 743.68 1477.4 0.2284 1.39052 +FS_7 Duct4.Fl_O 43.22 3.915 751.26 180.62 0.0060 195.29 3.840 747.22 2018.9 0.1664 1.39052 +FS_9 Core_Nozz.Fl_O 43.22 3.915 751.26 180.62 0.0060 195.29 3.458 725.52 862.9 0.4259 1.39052 +FS_15 BypBld.Fl_O 420.22 6.406 473.93 113.23 0.0000 921.49 5.524 454.25 3795.6 0.4646 1.40116 +FS_17 Duct5.Fl_O 420.22 6.358 473.93 113.23 0.0000 928.45 5.483 454.25 3824.3 0.4646 1.40116 +FS_19 Byp_Nozz.Fl_O 420.22 6.358 473.93 113.23 0.0000 928.45 3.458 398.06 2706.4 0.9746 1.40116 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1098.79 1.101 0.7933 2146.079 1.0351 0.7961 -2519.9 78.43 26.39 +LPC 94.46 1.487 0.8134 2109.400 1.1477 0.8236 -1020.2 23.27 7.10 +HPC 68.23 3.749 0.8508 5997.250 1.5351 0.8754 -4276.0 51.94 53.01 +HPT 27.28 2.811 0.9181 170.290 1.2859 0.9068 4276.0 +LPT 73.68 3.006 0.9033 64.223 1.3121 0.8888 3540.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2106.79 1.070 0.8195 0.544 2.6111 0.5215 1.4369 0.9679 3943.9586 +LPC 101.32 1.149 0.8472 0.576 1.4650 0.9323 3.2631 0.9600 3662.6571 +HPC 162.20 13.709 0.8393 0.943 2.3930 0.4206 0.2163 1.0137 6357.1603 +HPT 30.01 5.263 0.9365 111.220 5.2628 1.4085 0.4249 0.9803 1.5311 +LPT 153.10 3.798 0.9022 79.179 3.7980 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3213.23 12610.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 646.39 154.63 13.295 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 646.39 154.63 13.295 +Duct1 0.0025 0.2277 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 646.39 154.63 13.295 +Duct2 0.0025 0.3352 365.99 +Duct3 0.0050 0.2991 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2284 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.5038 835.02 200.35 35.535 +Duct5 0.0075 0.4646 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.3632 835.02 200.35 35.535 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 473.93 113.23 6.406 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.7801 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6141.7 3656.7 4276.0 +LP_Shaft 2016.4 9221.0 3540.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1300.76 0.9940 0.0550 0.25817 0.00660 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.839 0.9975 1.0000 0.9975 2706.36 0.975 951.2 12424.0 +Core_Nozz 1.132 0.9999 1.0000 0.9999 862.88 0.426 560.7 753.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 351 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 9/ 19/ 1/ 7 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 39000.0 0.00 459.84 8166.6 0.5262 4297.34 5.0383 581.09 22.747 2224.7 2167.8 1729.8 + core size:19.97 Q: 103.65 Maximum Thrust: 8166.6 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 459.84 3.640 418.14 99.88 0.0000 1666.72 2.854 389.97 5768.9 0.6000 1.40128 +FS_2 Inlet.Fl_O 459.84 3.622 418.14 99.88 0.0000 1675.11 2.892 392.01 5943.4 0.5763 1.40128 +FS_21 Fan.Fl_O 459.84 5.956 491.91 117.54 0.0000 1104.91 5.120 471.07 4515.2 0.4696 1.40094 +FS_13 Splitter.Fl_O2 383.69 5.956 491.91 117.54 0.0000 921.93 5.135 471.47 3795.6 0.4650 1.40094 +FS_22 Splitter.Fl_O1 76.15 5.956 491.91 117.54 0.0000 182.98 5.037 468.88 719.5 0.4949 1.40094 +FS_23 Duct1.Fl_O 76.15 5.941 491.91 117.54 0.0000 183.44 5.025 468.88 721.3 0.4949 1.40094 +FS_24 LPC.Fl_O 76.15 14.766 660.04 157.92 0.0000 85.50 12.911 635.30 366.0 0.4423 1.39745 +FS_25 Duct2.Fl_O 76.15 14.729 660.04 157.92 0.0000 85.71 12.879 635.30 366.9 0.4423 1.39745 +FS_3 HPC.Fl_O 76.15 82.809 1132.82 274.27 0.0000 19.97 77.918 1114.24 119.9 0.2990 1.37238 +FS_36 Bld3.Fl_O 69.30 82.809 1132.82 274.27 0.0000 18.18 77.918 1114.24 109.1 0.2990 1.37238 +FS_4 Burner.Fl_O 70.49 78.255 2224.69 579.43 0.0172 27.42 77.750 2221.30 483.4 0.0995 1.30896 +FS_45 HPT.Fl_O 77.35 29.265 1729.78 437.83 0.0157 70.93 27.644 1705.57 439.1 0.2939 1.32803 +FS_48 Duct3.Fl_O 77.35 29.119 1729.78 437.83 0.0157 71.29 27.506 1705.57 441.4 0.2939 1.32803 +FS_5 LPT.Fl_O 77.35 5.929 1191.80 293.08 0.0157 290.62 5.425 1164.16 1477.4 0.3636 1.35789 +FS_7 Duct4.Fl_O 77.35 5.869 1191.80 293.08 0.0157 293.56 5.610 1177.65 2018.9 0.2589 1.35789 +FS_9 Core_Nozz.Fl_O 77.35 5.869 1191.80 293.08 0.0157 293.56 3.131 1007.68 862.8 1.0000 1.35789 +FS_15 BypBld.Fl_O 383.69 5.956 491.91 117.54 0.0000 921.93 5.135 471.47 3795.6 0.4650 1.40094 +FS_17 Duct5.Fl_O 383.69 5.912 491.91 117.54 0.0000 928.90 5.097 471.47 3824.3 0.4650 1.40094 +FS_19 Byp_Nozz.Fl_O 383.69 5.912 491.91 117.54 0.0000 928.90 3.122 409.71 2706.4 1.0000 1.40094 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.644 0.8675 3944.235 1.1764 0.8764 -11490.6 24.72 17.46 +LPC 183.44 2.485 0.8685 3636.464 1.3418 0.8841 -4351.0 28.53 23.43 +HPC 85.71 5.622 0.8649 6329.799 1.7163 0.8925 -12536.0 19.98 20.02 +HPT 27.42 2.674 0.9131 151.389 1.2378 0.9031 12536.4 +LPT 71.29 4.911 0.9319 85.149 1.4514 0.9171 15840.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.448 0.8962 1.000 2.3715 0.5215 1.4369 0.9679 3943.9586 +LPC 196.78 1.455 0.9046 0.993 1.7705 0.9323 3.2631 0.9600 3662.6571 +HPC 203.77 22.367 0.8532 0.996 2.0431 0.4206 0.2163 1.0137 6357.1603 +HPT 30.17 4.940 0.9314 98.875 4.9399 1.4085 0.4249 0.9803 1.5311 +LPT 148.13 6.456 0.9307 104.978 6.4563 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5768.90 8305.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 828.01 198.64 24.703 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 828.01 198.64 24.703 +Duct1 0.0025 0.4949 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 828.01 198.64 24.703 +Duct2 0.0025 0.4423 365.99 +Duct3 0.0050 0.2939 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.6654 1132.82 274.27 82.809 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.1884 1132.82 274.27 82.809 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 491.91 117.54 5.956 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0383 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7140.5 9221.0 12536.4 +LP_Shaft 3541.4 23493.0 15840.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2224.69 0.9940 0.0550 1.19371 0.01723 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.071 0.9975 1.0000 0.9975 2706.36 1.000 990.2 12533.2 +Core_Nozz 2.057 0.9998 1.0000 0.9999 862.88 1.000 1539.0 3938.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 352 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 39000.0 0.00 447.98 7349.6 0.5159 3791.28 5.3080 581.09 20.800 2142.0 2087.6 1659.4 + core size:20.07 Q: 103.65 Maximum Thrust: 8166.6 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 447.98 3.640 418.14 99.88 0.0000 1623.74 2.854 389.97 5620.2 0.6000 1.40128 +FS_2 Inlet.Fl_O 447.98 3.622 418.14 99.88 0.0000 1631.92 2.942 393.94 5943.4 0.5533 1.40128 +FS_21 Fan.Fl_O 447.98 5.818 486.19 116.17 0.0000 1095.66 5.018 466.03 4515.2 0.4644 1.40101 +FS_13 Splitter.Fl_O2 376.96 5.818 486.19 116.17 0.0000 921.96 5.016 465.98 3795.6 0.4650 1.40101 +FS_22 Splitter.Fl_O1 71.02 5.818 486.19 116.17 0.0000 173.69 5.028 466.29 719.5 0.4612 1.40101 +FS_23 Duct1.Fl_O 71.02 5.803 486.19 116.17 0.0000 174.13 5.015 466.29 721.3 0.4612 1.40101 +FS_24 LPC.Fl_O 71.02 13.498 639.27 152.92 0.0000 85.84 11.786 615.04 366.0 0.4445 1.39816 +FS_25 Duct2.Fl_O 71.02 13.464 639.27 152.92 0.0000 86.06 11.757 615.04 366.9 0.4445 1.39816 +FS_3 HPC.Fl_O 71.02 75.720 1099.25 265.81 0.0000 20.07 71.203 1080.96 119.9 0.3003 1.37449 +FS_36 Bld3.Fl_O 64.63 75.720 1099.25 265.81 0.0000 18.26 71.203 1080.96 109.1 0.3003 1.37449 +FS_4 Burner.Fl_O 65.68 71.556 2142.02 554.90 0.0163 27.41 71.094 2138.73 483.4 0.0994 1.31193 +FS_45 HPT.Fl_O 72.07 26.492 1659.39 418.02 0.0148 71.51 24.998 1635.54 439.1 0.2961 1.33189 +FS_48 Duct3.Fl_O 72.07 26.359 1659.39 418.02 0.0148 71.87 24.873 1635.54 441.4 0.2961 1.33189 +FS_5 LPT.Fl_O 72.07 5.406 1144.23 280.56 0.0148 290.98 4.946 1117.44 1477.4 0.3636 1.36150 +FS_7 Duct4.Fl_O 72.07 5.352 1144.23 280.56 0.0148 293.92 5.115 1130.51 2018.9 0.2589 1.36150 +FS_9 Core_Nozz.Fl_O 72.07 5.352 1144.23 280.56 0.0148 293.92 2.854 966.19 862.9 0.9996 1.36150 +FS_15 BypBld.Fl_O 376.96 5.818 486.19 116.17 0.0000 921.96 5.016 465.98 3795.6 0.4650 1.40101 +FS_17 Duct5.Fl_O 376.96 5.774 486.19 116.17 0.0000 928.93 4.978 465.98 3824.3 0.4650 1.40101 +FS_19 Byp_Nozz.Fl_O 376.96 5.774 486.19 116.17 0.0000 928.93 3.049 404.94 2706.4 1.0000 1.40101 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1631.92 1.606 0.8928 3738.578 1.1627 0.8998 -10325.4 28.31 17.76 +LPC 174.13 2.326 0.8661 3467.085 1.3149 0.8809 -3692.6 28.98 22.22 +HPC 86.06 5.624 0.8639 6338.422 1.7196 0.8918 -11343.2 20.43 20.45 +HPT 27.41 2.701 0.9136 152.043 1.2428 0.9033 11343.4 +LPT 71.87 4.876 0.9273 82.404 1.4502 0.9117 14016.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3128.67 1.422 0.9224 0.948 2.1727 0.5215 1.4369 0.9679 3943.9586 +LPC 186.77 1.406 0.9021 0.947 1.7539 0.9323 3.2631 0.9600 3662.6571 +HPC 204.58 22.375 0.8522 0.997 2.0717 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 5.004 0.9320 99.302 5.0036 1.4085 0.4249 0.9803 1.5311 +LPT 149.33 6.406 0.9261 101.593 6.4063 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5620.16 8091.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 802.53 192.43 22.585 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 802.53 192.43 22.585 +Duct1 0.0025 0.4612 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 802.53 192.43 22.585 +Duct2 0.0025 0.4445 365.99 +Duct3 0.0050 0.2961 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.4857 1099.25 265.81 75.720 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.9060 1099.25 265.81 75.720 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 486.19 116.17 5.818 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3080 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7036.8 8466.5 11343.4 +LP_Shaft 3356.8 21931.1 14016.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2142.02 0.9940 0.0550 1.05313 0.01630 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.023 0.9976 1.0000 0.9975 2706.36 1.000 984.4 12062.1 +Core_Nozz 1.875 0.9999 1.0000 0.9999 862.88 1.000 1508.2 3378.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 353 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 39000.0 0.00 434.39 6533.3 0.5114 3340.83 5.5159 581.09 19.131 2058.8 2007.0 1590.7 + core size:20.21 Q: 103.65 Maximum Thrust: 8166.6 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 434.39 3.640 418.14 99.88 0.0000 1574.46 2.854 389.97 5449.6 0.6000 1.40128 +FS_2 Inlet.Fl_O 434.39 3.622 418.14 99.88 0.0000 1582.38 2.995 395.96 5943.4 0.5283 1.40128 +FS_21 Fan.Fl_O 434.39 5.644 480.85 114.89 0.0000 1089.12 4.879 461.21 4515.2 0.4607 1.40108 +FS_13 Splitter.Fl_O2 367.72 5.644 480.85 114.89 0.0000 921.97 4.866 460.86 3795.6 0.4650 1.40108 +FS_22 Splitter.Fl_O1 66.67 5.644 480.85 114.89 0.0000 167.15 4.944 462.98 719.5 0.4386 1.40108 +FS_23 Duct1.Fl_O 66.67 5.630 480.85 114.89 0.0000 167.57 4.932 462.98 721.3 0.4386 1.40108 +FS_24 LPC.Fl_O 66.67 12.659 625.98 149.72 0.0000 85.03 11.089 602.80 366.0 0.4391 1.39853 +FS_25 Duct2.Fl_O 66.67 12.627 625.98 149.72 0.0000 85.24 11.062 602.80 366.9 0.4391 1.39853 +FS_3 HPC.Fl_O 66.67 69.646 1070.68 258.63 0.0000 20.21 65.427 1052.52 119.9 0.3025 1.37629 +FS_36 Bld3.Fl_O 60.67 69.646 1070.68 258.63 0.0000 18.39 65.427 1052.52 109.1 0.3025 1.37629 +FS_4 Burner.Fl_O 61.59 65.815 2058.79 530.38 0.0153 27.40 65.391 2055.60 483.4 0.0992 1.31526 +FS_45 HPT.Fl_O 67.59 24.241 1590.74 398.84 0.0139 71.76 22.864 1567.50 439.1 0.2968 1.33586 +FS_48 Duct3.Fl_O 67.59 24.120 1590.74 398.84 0.0139 72.12 22.750 1567.50 441.4 0.2968 1.33586 +FS_5 LPT.Fl_O 67.59 4.983 1096.23 268.01 0.0139 289.83 4.562 1070.61 1477.4 0.3614 1.36519 +FS_7 Duct4.Fl_O 67.59 4.933 1096.23 268.01 0.0139 292.76 4.716 1083.10 2018.9 0.2574 1.36519 +FS_9 Core_Nozz.Fl_O 67.59 4.933 1096.23 268.01 0.0139 292.76 2.854 945.43 862.9 0.9268 1.36519 +FS_15 BypBld.Fl_O 367.72 5.644 480.85 114.89 0.0000 921.97 4.866 460.86 3795.6 0.4650 1.40108 +FS_17 Duct5.Fl_O 367.72 5.601 480.85 114.89 0.0000 928.94 4.829 460.86 3824.3 0.4650 1.40108 +FS_19 Byp_Nozz.Fl_O 367.72 5.601 480.85 114.89 0.0000 928.94 2.958 400.49 2706.4 1.0000 1.40108 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1582.38 1.558 0.9027 3606.099 1.1500 0.9086 -9226.8 31.95 18.40 +LPC 167.57 2.249 0.8632 3362.727 1.3018 0.8778 -3285.2 28.24 20.58 +HPC 85.24 5.516 0.8646 6316.869 1.7104 0.8922 -10272.6 21.97 22.08 +HPT 27.40 2.715 0.9143 152.943 1.2468 0.9041 10272.6 +LPT 72.12 4.841 0.9255 81.181 1.4511 0.9096 12512.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3034.01 1.388 0.9326 0.914 2.0943 0.5215 1.4369 0.9679 3943.9586 +LPC 179.74 1.383 0.8992 0.918 1.7201 0.9323 3.2631 0.9600 3662.6571 +HPC 202.64 21.875 0.8530 0.994 2.0970 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 5.037 0.9327 99.890 5.0365 1.4085 0.4249 0.9803 1.5311 +LPT 149.87 6.358 0.9243 100.086 6.3577 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5449.56 7845.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 783.66 187.84 20.980 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 783.66 187.84 20.980 +Duct1 0.0025 0.4386 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 783.66 187.84 20.980 +Duct2 0.0025 0.4391 365.99 +Duct3 0.0050 0.2968 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3614 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.3333 1070.68 258.63 69.646 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.6666 1070.68 258.63 69.646 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 480.85 114.89 5.644 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5159 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6939.6 7774.6 10272.6 +LP_Shaft 3237.8 20295.9 12512.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2058.79 0.9940 0.0550 0.92801 0.01530 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.963 0.9975 1.0000 0.9975 2706.36 1.000 979.0 11470.8 +Core_Nozz 1.728 0.9999 1.0000 0.9999 862.88 0.927 1384.1 2907.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 354 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 39000.0 0.00 403.21 4900.0 0.5147 2522.05 6.0006 581.09 15.820 1891.4 1845.0 1454.6 + core size:20.52 Q: 103.65 Maximum Thrust: 8166.6 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 403.21 3.640 418.14 99.88 0.0000 1461.45 2.854 389.97 5058.4 0.6000 1.40128 +FS_2 Inlet.Fl_O 403.21 3.622 418.14 99.88 0.0000 1468.81 3.102 399.97 5943.4 0.4759 1.40128 +FS_21 Fan.Fl_O 403.21 5.246 469.51 112.18 0.0000 1074.70 4.557 450.97 4515.2 0.4527 1.40120 +FS_13 Splitter.Fl_O2 345.61 5.246 469.51 112.18 0.0000 921.19 4.524 450.03 3795.6 0.4644 1.40120 +FS_22 Splitter.Fl_O1 57.60 5.246 469.51 112.18 0.0000 153.52 4.712 455.30 719.5 0.3943 1.40120 +FS_23 Duct1.Fl_O 57.60 5.233 469.51 112.18 0.0000 153.90 4.700 455.30 721.3 0.3943 1.40120 +FS_24 LPC.Fl_O 57.60 10.992 599.21 143.28 0.0000 82.77 9.713 578.43 366.0 0.4242 1.39906 +FS_25 Duct2.Fl_O 57.60 10.965 599.21 143.28 0.0000 82.97 9.689 578.43 366.9 0.4242 1.39906 +FS_3 HPC.Fl_O 57.60 57.594 1011.09 243.74 0.0000 20.52 53.990 993.24 119.9 0.3073 1.38002 +FS_36 Bld3.Fl_O 52.41 57.594 1011.09 243.74 0.0000 18.67 53.990 993.24 109.1 0.3073 1.38002 +FS_4 Burner.Fl_O 53.11 54.426 1891.41 481.84 0.0134 27.39 54.076 1888.43 483.4 0.0989 1.32269 +FS_45 HPT.Fl_O 58.30 19.907 1454.61 361.42 0.0122 72.07 18.767 1432.77 439.1 0.2972 1.34422 +FS_48 Duct3.Fl_O 58.30 19.807 1454.61 361.42 0.0122 72.43 18.673 1432.77 441.4 0.2972 1.34422 +FS_5 LPT.Fl_O 58.30 4.293 1009.66 245.63 0.0122 278.42 3.962 987.87 1477.4 0.3440 1.37191 +FS_7 Duct4.Fl_O 58.30 4.250 1009.66 245.63 0.0122 281.23 4.078 998.42 2018.9 0.2459 1.37191 +FS_9 Core_Nozz.Fl_O 58.30 4.250 1009.66 245.63 0.0122 281.23 2.854 905.67 862.9 0.7813 1.37191 +FS_15 BypBld.Fl_O 345.61 5.246 469.51 112.18 0.0000 921.19 4.524 450.03 3795.6 0.4644 1.40120 +FS_17 Duct5.Fl_O 345.61 5.206 469.51 112.18 0.0000 928.15 4.490 450.03 3824.3 0.4644 1.40120 +FS_19 Byp_Nozz.Fl_O 345.61 5.206 469.51 112.18 0.0000 928.15 2.854 395.24 2706.4 0.9677 1.40120 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1468.81 1.448 0.9107 3337.326 1.1229 0.9153 -7015.0 40.40 19.92 +LPC 153.90 2.101 0.8558 3149.464 1.2762 0.8700 -2535.1 26.23 17.17 +HPC 82.97 5.253 0.8656 6266.872 1.6874 0.8923 -8186.5 25.54 25.68 +HPT 27.39 2.734 0.9148 154.882 1.2542 0.9042 8186.5 +LPT 72.43 4.614 0.9215 78.567 1.4407 0.9050 9550.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2816.25 1.312 0.9408 0.846 2.0418 0.5215 1.4369 0.9679 3943.9586 +LPC 165.08 1.337 0.8914 0.860 1.6452 0.9323 3.2631 0.9600 3662.6571 +HPC 197.26 20.659 0.8539 0.986 2.1341 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.081 0.9331 101.156 5.0812 1.4085 0.4249 0.9803 1.5311 +LPT 150.51 6.041 0.9203 96.863 6.0409 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5058.43 7282.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 744.95 178.45 17.796 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 744.95 178.45 17.796 +Duct1 0.0025 0.3943 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 744.95 178.45 17.796 +Duct2 0.0025 0.4242 365.99 +Duct3 0.0050 0.2972 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3440 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.0159 1011.09 243.74 57.594 +Duct5 0.0075 0.4644 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.1678 1011.09 243.74 57.594 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 469.51 112.18 5.246 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.0006 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6735.9 6383.2 8186.5 +LP_Shaft 2996.5 16739.0 9550.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1891.41 0.9940 0.0550 0.70057 0.01337 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.824 0.9975 1.0000 0.9975 2706.36 0.968 941.2 10110.1 +Core_Nozz 1.489 0.9999 1.0000 0.9999 862.88 0.781 1143.6 2072.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 355 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 39000.0 0.00 365.31 3266.7 0.5395 1762.50 6.6869 581.09 12.367 1702.3 1661.7 1301.4 + core size:20.88 Q: 103.65 Maximum Thrust: 8166.6 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 365.31 3.640 418.14 99.88 0.0000 1324.10 2.854 389.97 4583.0 0.6000 1.40128 +FS_2 Inlet.Fl_O 365.31 3.622 418.14 99.88 0.0000 1330.76 3.211 403.94 5943.4 0.4186 1.40128 +FS_21 Fan.Fl_O 365.31 4.806 456.88 109.15 0.0000 1048.34 4.212 439.92 4515.2 0.4383 1.40129 +FS_13 Splitter.Fl_O2 317.79 4.806 456.88 109.15 0.0000 911.96 4.161 438.40 3795.6 0.4583 1.40129 +FS_22 Splitter.Fl_O1 47.52 4.806 456.88 109.15 0.0000 136.38 4.431 446.37 719.5 0.3426 1.40129 +FS_23 Duct1.Fl_O 47.52 4.794 456.88 109.15 0.0000 136.72 4.420 446.37 721.3 0.3426 1.40129 +FS_24 LPC.Fl_O 47.52 9.084 565.10 135.09 0.0000 80.25 8.100 546.90 366.0 0.4080 1.39962 +FS_25 Duct2.Fl_O 47.52 9.061 565.10 135.09 0.0000 80.45 8.080 546.90 366.9 0.4080 1.39962 +FS_3 HPC.Fl_O 47.52 45.021 939.67 226.04 0.0000 20.88 42.096 922.28 119.9 0.3128 1.38443 +FS_36 Bld3.Fl_O 43.25 45.021 939.67 226.04 0.0000 19.00 42.096 922.28 109.1 0.3128 1.38443 +FS_4 Burner.Fl_O 43.74 42.545 1702.33 428.30 0.0113 27.37 42.271 1699.59 483.4 0.0984 1.33227 +FS_45 HPT.Fl_O 48.01 15.400 1301.38 320.26 0.0103 72.58 14.505 1281.11 439.1 0.2984 1.35457 +FS_48 Duct3.Fl_O 48.01 15.323 1301.38 320.26 0.0103 72.94 14.432 1281.11 441.4 0.2984 1.35457 +FS_5 LPT.Fl_O 48.01 3.746 924.94 224.03 0.0103 251.55 3.514 908.84 1477.4 0.3057 1.37851 +FS_7 Duct4.Fl_O 48.01 3.708 924.94 224.03 0.0103 254.09 3.587 916.53 2018.9 0.2201 1.37851 +FS_9 Core_Nozz.Fl_O 48.01 3.708 924.94 224.03 0.0103 254.09 2.854 860.60 862.9 0.6264 1.37851 +FS_15 BypBld.Fl_O 317.79 4.806 456.88 109.15 0.0000 911.96 4.161 438.40 3795.6 0.4583 1.40129 +FS_17 Duct5.Fl_O 317.79 4.770 456.88 109.15 0.0000 918.85 4.130 438.40 3824.3 0.4583 1.40129 +FS_19 Byp_Nozz.Fl_O 317.79 4.770 456.88 109.15 0.0000 918.85 2.854 394.36 2706.4 0.8888 1.40129 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1330.76 1.327 0.9107 2979.896 1.0926 0.9142 -4792.9 47.65 21.22 +LPC 136.72 1.895 0.8468 2850.761 1.2369 0.8600 -1744.2 25.15 14.06 +HPC 80.45 4.968 0.8649 6221.120 1.6628 0.8909 -6115.2 29.75 29.95 +HPT 27.37 2.763 0.9153 157.386 1.2636 0.9045 6115.2 +LPT 72.94 4.091 0.9186 74.168 1.4070 0.9026 6537.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2551.56 1.228 0.9409 0.756 2.0684 0.5215 1.4369 0.9679 3943.9586 +LPC 146.65 1.274 0.8821 0.778 1.5921 0.9323 3.2631 0.9600 3662.6571 +HPC 191.26 19.345 0.8532 0.979 2.1682 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.149 0.9337 102.791 5.1487 1.4085 0.4249 0.9803 1.5311 +LPT 151.57 5.311 0.9174 91.439 5.3113 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4583.01 6597.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 697.33 166.92 14.329 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 697.33 166.92 14.329 +Duct1 0.0025 0.3426 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 697.33 166.92 14.329 +Duct2 0.0025 0.4080 365.99 +Duct3 0.0050 0.2984 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3057 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.6633 939.67 226.04 45.021 +Duct5 0.0075 0.4583 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.6138 939.67 226.04 45.021 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 456.88 109.15 4.806 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6869 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6493.6 4946.1 6115.2 +LP_Shaft 2675.6 12832.2 6537.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1702.33 0.9940 0.0550 0.48958 0.01132 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.671 0.9975 1.0000 0.9975 2706.36 0.889 863.5 8528.9 +Core_Nozz 1.299 0.9999 1.0000 0.9999 862.88 0.626 895.0 1335.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 356 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 39000.0 0.00 316.84 1633.3 0.6403 1045.81 7.7628 581.09 8.694 1457.6 1424.6 1105.7 + core size:21.43 Q: 103.65 Maximum Thrust: 8166.6 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 316.84 3.640 418.14 99.88 0.0000 1148.41 2.854 389.97 3974.9 0.6000 1.40128 +FS_2 Inlet.Fl_O 316.84 3.622 418.14 99.88 0.0000 1154.19 3.324 407.97 5943.4 0.3524 1.40128 +FS_21 Fan.Fl_O 316.84 4.317 442.21 105.64 0.0000 995.96 3.843 427.72 4515.2 0.4108 1.40134 +FS_13 Splitter.Fl_O2 280.68 4.317 442.21 105.64 0.0000 882.31 3.781 425.74 3795.6 0.4390 1.40134 +FS_22 Splitter.Fl_O1 36.16 4.317 442.21 105.64 0.0000 113.66 4.090 435.41 719.5 0.2789 1.40134 +FS_23 Duct1.Fl_O 36.16 4.306 442.21 105.64 0.0000 113.94 4.079 435.41 721.3 0.2789 1.40134 +FS_24 LPC.Fl_O 36.16 6.967 520.34 124.35 0.0000 76.39 6.293 505.41 366.0 0.3840 1.40049 +FS_25 Duct2.Fl_O 36.16 6.950 520.34 124.35 0.0000 76.58 6.277 505.41 366.9 0.3840 1.40049 +FS_3 HPC.Fl_O 36.16 31.650 844.75 202.73 0.0000 21.43 29.476 828.05 119.9 0.3215 1.38983 +FS_36 Bld3.Fl_O 32.90 31.650 844.75 202.73 0.0000 19.50 29.476 828.05 109.1 0.3215 1.38983 +FS_4 Burner.Fl_O 33.19 29.909 1457.59 361.07 0.0088 27.34 29.717 1455.18 483.4 0.0978 1.34634 +FS_45 HPT.Fl_O 36.45 10.693 1105.71 269.18 0.0080 73.14 10.061 1087.71 439.1 0.2993 1.36851 +FS_48 Duct3.Fl_O 36.45 10.639 1105.71 269.18 0.0080 73.51 10.011 1087.71 441.4 0.2993 1.36851 +FS_5 LPT.Fl_O 36.45 3.323 831.45 200.53 0.0080 204.08 3.191 822.13 1477.4 0.2425 1.38531 +FS_7 Duct4.Fl_O 36.45 3.290 831.45 200.53 0.0080 206.14 3.220 826.50 2018.9 0.1763 1.38531 +FS_9 Core_Nozz.Fl_O 36.45 3.290 831.45 200.53 0.0080 206.14 2.854 799.15 862.9 0.4575 1.38531 +FS_15 BypBld.Fl_O 280.68 4.317 442.21 105.64 0.0000 882.31 3.781 425.74 3795.6 0.4390 1.40134 +FS_17 Duct5.Fl_O 280.68 4.284 442.21 105.64 0.0000 888.97 3.753 425.74 3824.3 0.4390 1.40134 +FS_19 Byp_Nozz.Fl_O 280.68 4.284 442.21 105.64 0.0000 888.97 2.854 393.62 2706.4 0.7843 1.40134 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1154.19 1.192 0.8951 2475.451 1.0576 0.8977 -2582.8 57.02 22.16 +LPC 113.94 1.618 0.8358 2407.136 1.1767 0.8466 -957.3 27.79 11.08 +HPC 76.58 4.554 0.8631 6150.790 1.6235 0.8885 -4009.7 36.47 36.92 +HPT 27.34 2.797 0.9162 161.366 1.2767 0.9050 4009.7 +LPT 73.51 3.202 0.9083 66.842 1.3299 0.8938 3540.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2213.01 1.133 0.9248 0.628 2.2152 0.5215 1.4369 0.9679 3943.9586 +LPC 122.22 1.189 0.8706 0.657 1.5929 0.9323 3.2631 0.9600 3662.6571 +HPC 182.06 17.429 0.8515 0.968 2.2282 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.230 0.9346 105.391 5.2298 1.4085 0.4249 0.9803 1.5311 +LPT 152.74 4.071 0.9071 82.408 4.0711 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3974.92 5722.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 634.56 151.79 10.568 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 634.56 151.79 10.568 +Duct1 0.0025 0.2789 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 634.56 151.79 10.568 +Duct2 0.0025 0.3840 365.99 +Duct3 0.0050 0.2993 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2425 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.2655 844.75 202.73 31.650 +Duct5 0.0075 0.4390 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 1.9887 844.75 202.73 31.650 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 442.21 105.64 4.317 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.7628 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6160.7 3418.4 4009.7 +LP_Shaft 2222.6 8365.3 3540.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1457.59 0.9940 0.0550 0.29050 0.00883 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.501 0.9975 1.0000 0.9975 2706.36 0.784 761.2 6641.0 +Core_Nozz 1.153 0.9999 1.0000 0.9999 862.88 0.457 630.9 714.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 357 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 11/ 21/ 1/ 9 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.600 39000.0 0.00 267.39 408.3 1.2413 506.86 9.3680 581.09 5.546 1167.8 1144.2 879.5 + core size:22.38 Q: 103.65 Maximum Thrust: 8166.6 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 267.39 3.640 418.14 99.88 0.0000 969.19 2.854 389.97 3354.6 0.6000 1.40128 +FS_2 Inlet.Fl_O 267.39 3.622 418.14 99.88 0.0000 974.07 3.416 411.17 5943.4 0.2905 1.40128 +FS_21 Fan.Fl_O 267.39 3.902 429.15 102.52 0.0000 916.17 3.547 417.61 4515.2 0.3711 1.40133 +FS_13 Splitter.Fl_O2 241.60 3.902 429.15 102.52 0.0000 827.80 3.484 415.47 3795.6 0.4051 1.40133 +FS_22 Splitter.Fl_O1 25.79 3.902 429.15 102.52 0.0000 88.36 3.780 425.29 719.5 0.2127 1.40133 +FS_23 Duct1.Fl_O 25.79 3.892 429.15 102.52 0.0000 88.59 3.771 425.29 721.3 0.2127 1.40133 +FS_24 LPC.Fl_O 25.79 5.197 474.23 113.31 0.0000 69.73 4.787 463.19 366.0 0.3446 1.40116 +FS_25 Duct2.Fl_O 25.79 5.184 474.23 113.31 0.0000 69.90 4.775 463.19 366.9 0.3446 1.40116 +FS_3 HPC.Fl_O 25.79 20.189 737.01 176.52 0.0000 22.38 18.664 720.81 119.9 0.3373 1.39476 +FS_36 Bld3.Fl_O 23.47 20.189 737.01 176.52 0.0000 20.36 18.664 720.81 109.1 0.3373 1.39476 +FS_4 Burner.Fl_O 23.61 19.078 1167.82 284.57 0.0060 27.29 18.956 1165.81 483.4 0.0969 1.36594 +FS_45 HPT.Fl_O 25.93 6.750 879.48 212.03 0.0055 73.51 6.348 864.58 439.1 0.2993 1.38443 +FS_48 Duct3.Fl_O 25.93 6.717 879.48 212.03 0.0055 73.88 6.316 864.58 441.4 0.2993 1.38443 +FS_5 LPT.Fl_O 25.93 3.076 724.73 174.10 0.0055 146.46 3.014 720.62 1477.4 0.1706 1.39191 +FS_7 Duct4.Fl_O 25.93 3.045 724.73 174.10 0.0055 147.94 3.012 722.52 2018.9 0.1251 1.39191 +FS_9 Core_Nozz.Fl_O 25.93 3.045 724.73 174.10 0.0055 147.94 2.854 711.62 862.9 0.3065 1.39191 +FS_15 BypBld.Fl_O 241.60 3.902 429.15 102.52 0.0000 827.80 3.484 415.47 3795.6 0.4051 1.40133 +FS_17 Duct5.Fl_O 241.60 3.872 429.15 102.52 0.0000 834.06 3.458 415.47 3824.3 0.4051 1.40133 +FS_19 Byp_Nozz.Fl_O 241.60 3.872 429.15 102.52 0.0000 834.06 2.854 393.23 2706.4 0.6748 1.40133 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 974.07 1.077 0.8163 1867.166 1.0263 0.8183 -997.6 84.06 21.58 +LPC 88.59 1.335 0.8222 1843.045 1.1050 0.8293 -393.7 36.58 9.39 +HPC 69.90 3.894 0.8545 6028.012 1.5541 0.8792 -2306.7 49.03 50.00 +HPT 27.29 2.826 0.9179 168.669 1.2926 0.9061 2306.7 +LPT 73.88 2.184 0.8966 56.531 1.2135 0.8859 1391.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1867.64 1.054 0.8433 0.473 2.5540 0.5215 1.4369 0.9679 3943.9586 +LPC 95.02 1.103 0.8564 0.503 1.6955 0.9323 3.2631 0.9600 3662.6571 +HPC 166.19 14.379 0.8430 0.948 2.3775 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.298 0.9363 110.161 5.2984 1.4085 0.4249 0.9803 1.5311 +LPT 153.52 2.651 0.8954 69.695 2.6513 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3354.58 4829.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 566.52 135.43 7.383 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 566.52 135.43 7.383 +Duct1 0.0025 0.2127 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 566.52 135.43 7.383 +Duct2 0.0025 0.3446 365.99 +Duct3 0.0050 0.2993 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1706 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 0.9027 737.01 176.52 20.189 +Duct5 0.0075 0.4051 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 1.4185 737.01 176.52 20.189 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 429.15 102.52 3.902 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.3680 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 5764.0 2101.8 2306.7 +LP_Shaft 1676.5 4359.2 1391.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1167.82 0.9940 0.0550 0.14080 0.00600 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.357 0.9975 1.0000 0.9975 2706.36 0.675 654.6 4915.6 +Core_Nozz 1.067 0.9999 1.0000 0.9999 862.88 0.307 399.7 322.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 358 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 4/ 14/ 1/ 2 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 39000.0 0.00 494.12 8405.2 0.5651 4750.12 5.0387 677.94 22.740 2275.3 2217.3 1771.2 + core size:19.96 Q: 141.08 Maximum Thrust: 8405.2 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 494.12 3.959 428.31 102.31 0.0000 1666.72 2.854 389.97 5313.4 0.7000 1.40132 +FS_2 Inlet.Fl_O 494.12 3.939 428.31 102.31 0.0000 1675.11 3.145 401.55 5943.4 0.5763 1.40132 +FS_21 Fan.Fl_O 494.12 6.478 503.87 120.41 0.0000 1104.82 5.569 482.54 4515.2 0.4696 1.40076 +FS_13 Splitter.Fl_O2 412.29 6.478 503.87 120.41 0.0000 921.87 5.585 482.94 3795.6 0.4649 1.40076 +FS_22 Splitter.Fl_O1 81.83 6.478 503.87 120.41 0.0000 182.96 5.479 480.29 719.5 0.4948 1.40076 +FS_23 Duct1.Fl_O 81.83 6.462 503.87 120.41 0.0000 183.42 5.465 480.29 721.3 0.4948 1.40076 +FS_24 LPC.Fl_O 81.83 16.066 676.07 161.79 0.0000 85.45 14.051 650.79 366.0 0.4421 1.39685 +FS_25 Duct2.Fl_O 81.83 16.026 676.07 161.79 0.0000 85.67 14.016 650.79 366.9 0.4421 1.39685 +FS_3 HPC.Fl_O 81.83 90.033 1158.80 280.85 0.0000 19.96 84.719 1139.87 119.9 0.2990 1.37074 +FS_36 Bld3.Fl_O 74.46 90.033 1158.80 280.85 0.0000 18.17 84.719 1139.87 109.1 0.2990 1.37074 +FS_4 Burner.Fl_O 75.78 85.081 2275.34 594.51 0.0177 27.42 84.532 2271.88 483.4 0.0995 1.30726 +FS_45 HPT.Fl_O 83.14 31.835 1771.19 449.56 0.0161 70.93 30.071 1746.52 439.1 0.2941 1.32586 +FS_48 Duct3.Fl_O 83.14 31.676 1771.19 449.56 0.0161 71.28 29.921 1746.52 441.4 0.2941 1.32586 +FS_5 LPT.Fl_O 83.14 6.461 1222.96 301.31 0.0161 290.39 5.913 1194.78 1477.4 0.3636 1.35561 +FS_7 Duct4.Fl_O 83.14 6.396 1222.96 301.31 0.0161 293.33 6.114 1208.53 2018.9 0.2589 1.35561 +FS_9 Core_Nozz.Fl_O 83.14 6.396 1222.96 301.31 0.0161 293.33 3.413 1034.97 862.9 1.0000 1.35561 +FS_15 BypBld.Fl_O 412.29 6.478 503.87 120.41 0.0000 921.87 5.585 482.94 3795.6 0.4649 1.40076 +FS_17 Duct5.Fl_O 412.29 6.430 503.87 120.41 0.0000 928.83 5.544 482.94 3824.3 0.4649 1.40076 +FS_19 Byp_Nozz.Fl_O 412.29 6.430 503.87 120.41 0.0000 928.83 3.395 419.67 2706.4 1.0000 1.40076 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.644 0.8675 3944.235 1.1764 0.8765 -12648.1 24.71 17.46 +LPC 183.42 2.486 0.8684 3636.485 1.3418 0.8841 -4791.0 28.48 23.38 +HPC 85.67 5.618 0.8650 6328.616 1.7140 0.8924 -13783.4 20.02 20.06 +HPT 27.42 2.673 0.9132 151.474 1.2365 0.9032 13783.3 +LPT 71.28 4.903 0.9320 85.166 1.4483 0.9173 17439.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8962 1.000 2.3710 0.5215 1.4369 0.9679 3943.9586 +LPC 196.74 1.455 0.9046 0.993 1.7692 0.9323 3.2631 0.9600 3662.6571 +HPC 203.66 22.348 0.8533 0.996 2.0430 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.937 0.9315 98.930 4.9365 1.4085 0.4249 0.9803 1.5311 +LPT 148.12 6.444 0.9308 104.999 6.4440 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5313.37 10411.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 847.73 203.46 26.868 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 847.73 203.46 26.868 +Duct1 0.0025 0.4948 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 847.73 203.46 26.868 +Duct2 0.0025 0.4421 365.99 +Duct3 0.0050 0.2941 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.8639 1158.80 280.85 90.033 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.5004 1158.80 280.85 90.033 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 503.87 120.41 6.478 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0387 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7225.4 10019.1 13783.3 +LP_Shaft 3584.2 25554.2 17439.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2275.34 0.9940 0.0550 1.31948 0.01772 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.253 0.9972 1.0000 0.9975 2706.36 1.000 1002.2 14306.8 +Core_Nozz 2.241 0.9992 1.0000 0.9999 862.88 1.000 1558.5 4510.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 359 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 39000.0 0.00 481.60 7564.4 0.5550 4198.12 5.3042 677.94 20.822 2192.1 2136.4 1700.1 + core size:20.06 Q: 141.08 Maximum Thrust: 8405.2 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 481.60 3.959 428.31 102.31 0.0000 1624.48 2.854 389.97 5178.7 0.7000 1.40132 +FS_2 Inlet.Fl_O 481.60 3.939 428.31 102.31 0.0000 1632.66 3.198 403.49 5943.4 0.5536 1.40132 +FS_21 Fan.Fl_O 481.60 6.330 498.10 119.02 0.0000 1095.70 5.459 477.45 4515.2 0.4644 1.40085 +FS_13 Splitter.Fl_O2 405.20 6.330 498.10 119.02 0.0000 921.90 5.458 477.40 3795.6 0.4649 1.40085 +FS_22 Splitter.Fl_O1 76.39 6.330 498.10 119.02 0.0000 173.80 5.469 477.69 719.5 0.4616 1.40085 +FS_23 Duct1.Fl_O 76.39 6.314 498.10 119.02 0.0000 174.24 5.456 477.69 721.3 0.4616 1.40085 +FS_24 LPC.Fl_O 76.39 14.699 655.01 156.71 0.0000 85.83 12.835 630.21 366.0 0.4445 1.39764 +FS_25 Duct2.Fl_O 76.39 14.662 655.01 156.71 0.0000 86.05 12.803 630.21 366.9 0.4445 1.39764 +FS_3 HPC.Fl_O 76.39 82.439 1125.11 272.32 0.0000 20.06 77.525 1106.46 119.9 0.3003 1.37286 +FS_36 Bld3.Fl_O 69.52 82.439 1125.11 272.32 0.0000 18.25 77.525 1106.46 109.1 0.3003 1.37286 +FS_4 Burner.Fl_O 70.68 77.905 2192.07 569.67 0.0168 27.41 77.402 2188.71 483.4 0.0994 1.31015 +FS_45 HPT.Fl_O 77.56 28.861 1700.11 429.43 0.0153 71.50 27.234 1675.80 439.1 0.2963 1.32967 +FS_48 Duct3.Fl_O 77.56 28.716 1700.11 429.43 0.0153 71.86 27.098 1675.80 441.4 0.2963 1.32967 +FS_5 LPT.Fl_O 77.56 5.899 1174.80 288.57 0.0153 290.78 5.397 1147.46 1477.4 0.3637 1.35925 +FS_7 Duct4.Fl_O 77.56 5.840 1174.80 288.57 0.0153 293.72 5.582 1160.80 2018.9 0.2589 1.35925 +FS_9 Core_Nozz.Fl_O 77.56 5.840 1174.80 288.57 0.0153 293.72 3.114 992.78 862.9 1.0000 1.35925 +FS_15 BypBld.Fl_O 405.20 6.330 498.10 119.02 0.0000 921.90 5.458 477.40 3795.6 0.4649 1.40085 +FS_17 Duct5.Fl_O 405.20 6.282 498.10 119.02 0.0000 928.87 5.417 477.40 3824.3 0.4649 1.40085 +FS_19 Byp_Nozz.Fl_O 405.20 6.282 498.10 119.02 0.0000 928.87 3.317 414.86 2706.4 1.0000 1.40085 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1632.66 1.607 0.8926 3741.096 1.1629 0.8996 -11384.9 28.25 17.75 +LPC 174.24 2.328 0.8661 3469.134 1.3150 0.8809 -4073.4 28.97 22.23 +HPC 86.05 5.623 0.8639 6338.143 1.7177 0.8917 -12496.0 20.44 20.46 +HPT 27.41 2.699 0.9137 152.129 1.2414 0.9035 12496.1 +LPT 71.86 4.868 0.9275 82.451 1.4471 0.9119 15457.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3130.15 1.422 0.9222 0.949 2.1743 0.5215 1.4369 0.9679 3943.9586 +LPC 186.89 1.407 0.9022 0.947 1.7539 0.9323 3.2631 0.9600 3662.6571 +HPC 204.56 22.370 0.8523 0.997 2.0719 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 5.000 0.9320 99.358 4.9996 1.4085 0.4249 0.9803 1.5311 +LPT 149.31 6.395 0.9263 101.651 6.3954 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5178.73 10147.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 821.99 197.17 24.591 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 821.99 197.17 24.591 +Duct1 0.0025 0.4616 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 821.99 197.17 24.591 +Duct2 0.0025 0.4445 365.99 +Duct3 0.0050 0.2963 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3637 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.6737 1125.11 272.32 82.439 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.2016 1125.11 272.32 82.439 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 498.10 119.02 6.330 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3042 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7122.6 9214.5 12496.1 +LP_Shaft 3399.6 23880.1 15457.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2192.07 0.9940 0.0550 1.16614 0.01677 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.201 0.9973 1.0000 0.9975 2706.36 1.000 996.4 13803.4 +Core_Nozz 2.046 0.9998 1.0000 0.9999 862.88 1.000 1528.2 3908.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:55 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 360 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 39000.0 0.00 467.51 6724.2 0.5507 3703.29 5.5105 677.94 19.179 2107.2 2054.3 1630.3 + core size:20.21 Q: 141.08 Maximum Thrust: 8405.2 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 467.51 3.959 428.31 102.31 0.0000 1576.96 2.854 389.97 5027.2 0.7000 1.40132 +FS_2 Inlet.Fl_O 467.51 3.939 428.31 102.31 0.0000 1584.90 3.254 405.49 5943.4 0.5296 1.40132 +FS_21 Fan.Fl_O 467.51 6.149 492.84 117.76 0.0000 1089.21 5.315 472.71 4515.2 0.4608 1.40092 +FS_13 Splitter.Fl_O2 395.70 6.149 492.84 117.76 0.0000 921.91 5.301 472.36 3795.6 0.4649 1.40092 +FS_22 Splitter.Fl_O1 71.81 6.149 492.84 117.76 0.0000 167.30 5.385 474.49 719.5 0.4391 1.40092 +FS_23 Duct1.Fl_O 71.81 6.133 492.84 117.76 0.0000 167.72 5.372 474.49 721.3 0.4391 1.40092 +FS_24 LPC.Fl_O 71.81 13.829 642.08 153.60 0.0000 84.91 12.120 618.41 366.0 0.4383 1.39807 +FS_25 Duct2.Fl_O 71.81 13.794 642.08 153.60 0.0000 85.12 12.090 618.41 366.9 0.4383 1.39807 +FS_3 HPC.Fl_O 71.81 75.932 1096.40 265.09 0.0000 20.21 71.334 1077.87 119.9 0.3026 1.37467 +FS_36 Bld3.Fl_O 65.35 75.932 1096.40 265.09 0.0000 18.39 71.334 1077.87 109.1 0.3026 1.37467 +FS_4 Burner.Fl_O 66.37 71.756 2107.20 544.53 0.0157 27.40 71.293 2103.95 483.4 0.0993 1.31338 +FS_45 HPT.Fl_O 72.84 26.453 1630.28 409.81 0.0143 71.74 24.952 1606.60 439.1 0.2969 1.33364 +FS_48 Duct3.Fl_O 72.84 26.321 1630.28 409.81 0.0143 72.10 24.827 1606.60 441.4 0.2969 1.33364 +FS_5 LPT.Fl_O 72.84 5.414 1124.36 275.33 0.0143 291.08 4.953 1097.94 1477.4 0.3636 1.36311 +FS_7 Duct4.Fl_O 72.84 5.360 1124.36 275.33 0.0143 294.02 5.122 1110.83 2018.9 0.2588 1.36311 +FS_9 Core_Nozz.Fl_O 72.84 5.360 1124.36 275.33 0.0143 294.02 2.856 948.70 862.9 1.0000 1.36311 +FS_15 BypBld.Fl_O 395.70 6.149 492.84 117.76 0.0000 921.91 5.301 472.36 3795.6 0.4649 1.40092 +FS_17 Duct5.Fl_O 395.70 6.103 492.84 117.76 0.0000 928.88 5.262 472.36 3824.3 0.4649 1.40092 +FS_19 Byp_Nozz.Fl_O 395.70 6.103 492.84 117.76 0.0000 928.88 3.222 410.48 2706.4 1.0000 1.40092 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1584.90 1.561 0.9024 3612.235 1.1507 0.9084 -10218.8 31.73 18.34 +LPC 167.72 2.255 0.8631 3367.459 1.3028 0.8778 -3640.6 28.09 20.51 +HPC 85.12 5.505 0.8648 6313.956 1.7076 0.8922 -11327.6 22.07 22.14 +HPT 27.40 2.713 0.9144 153.038 1.2452 0.9041 11327.5 +LPT 72.10 4.861 0.9255 81.298 1.4500 0.9095 13859.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3038.85 1.390 0.9323 0.916 2.0962 0.5215 1.4369 0.9679 3943.9586 +LPC 179.90 1.385 0.8991 0.919 1.7169 0.9323 3.2631 0.9600 3662.6571 +HPC 202.36 21.824 0.8531 0.993 2.0964 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 5.031 0.9328 99.952 5.0307 1.4085 0.4249 0.9803 1.5311 +LPT 149.82 6.386 0.9243 100.230 6.3865 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5027.24 9850.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 803.30 192.62 22.897 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 803.30 192.62 22.897 +Duct1 0.0025 0.4391 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 803.30 192.62 22.897 +Duct2 0.0025 0.4383 365.99 +Duct3 0.0050 0.2969 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.5133 1096.40 265.09 75.932 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.9494 1096.40 265.09 75.932 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 492.84 117.76 6.149 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5105 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7025.1 8468.7 11327.5 +LP_Shaft 3282.5 22175.5 13859.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2107.20 0.9940 0.0550 1.02869 0.01574 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.138 0.9975 1.0000 0.9975 2706.36 1.000 991.1 13187.3 +Core_Nozz 1.878 0.9999 1.0000 0.9999 862.88 1.000 1495.8 3387.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 361 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 39000.0 0.00 435.86 5043.1 0.5555 2801.41 5.9880 677.94 15.941 1935.1 1887.8 1490.5 + core size:20.54 Q: 141.08 Maximum Thrust: 8405.2 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 435.86 3.959 428.31 102.31 0.0000 1470.20 2.854 389.97 4686.9 0.7000 1.40132 +FS_2 Inlet.Fl_O 435.86 3.939 428.31 102.31 0.0000 1477.60 3.365 409.40 5943.4 0.4797 1.40132 +FS_21 Fan.Fl_O 435.86 5.738 481.80 115.12 0.0000 1075.94 4.983 462.72 4515.2 0.4534 1.40107 +FS_13 Splitter.Fl_O2 373.49 5.738 481.80 115.12 0.0000 921.97 4.947 461.77 3795.6 0.4650 1.40107 +FS_22 Splitter.Fl_O1 62.37 5.738 481.80 115.12 0.0000 153.97 5.150 467.12 719.5 0.3957 1.40107 +FS_23 Duct1.Fl_O 62.37 5.723 481.80 115.12 0.0000 154.36 5.137 467.12 721.3 0.3957 1.40107 +FS_24 LPC.Fl_O 62.37 12.140 616.88 147.53 0.0000 82.34 10.744 595.77 366.0 0.4215 1.39874 +FS_25 Duct2.Fl_O 62.37 12.110 616.88 147.53 0.0000 82.55 10.718 595.77 366.9 0.4215 1.39874 +FS_3 HPC.Fl_O 62.37 63.112 1037.35 250.29 0.0000 20.54 59.153 1019.05 119.9 0.3078 1.37838 +FS_36 Bld3.Fl_O 56.76 63.112 1037.35 250.29 0.0000 18.69 59.153 1019.05 109.1 0.3078 1.37838 +FS_4 Burner.Fl_O 57.54 59.641 1935.13 494.34 0.0137 27.39 59.257 1932.10 483.4 0.0989 1.32076 +FS_45 HPT.Fl_O 63.15 21.846 1490.48 371.15 0.0125 72.02 20.596 1468.24 439.1 0.2972 1.34204 +FS_48 Duct3.Fl_O 63.15 21.736 1490.48 371.15 0.0125 72.38 20.493 1468.24 441.4 0.2972 1.34204 +FS_5 LPT.Fl_O 63.15 4.584 1029.70 250.77 0.0125 285.23 4.211 1006.28 1477.4 0.3540 1.37042 +FS_7 Duct4.Fl_O 63.15 4.539 1029.70 250.77 0.0125 288.11 4.346 1017.67 2018.9 0.2525 1.37042 +FS_9 Core_Nozz.Fl_O 63.15 4.539 1029.70 250.77 0.0125 288.11 2.854 907.42 862.9 0.8473 1.37042 +FS_15 BypBld.Fl_O 373.49 5.738 481.80 115.12 0.0000 921.97 4.947 461.77 3795.6 0.4650 1.40107 +FS_17 Duct5.Fl_O 373.49 5.695 481.80 115.12 0.0000 928.93 4.910 461.77 3824.3 0.4650 1.40107 +FS_19 Byp_Nozz.Fl_O 373.49 5.695 481.80 115.12 0.0000 928.93 3.007 401.28 2706.4 1.0000 1.40107 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1477.60 1.457 0.9104 3358.933 1.1249 0.9151 -7895.7 39.79 19.81 +LPC 154.36 2.121 0.8550 3167.011 1.2804 0.8694 -2860.6 25.62 16.86 +HPC 82.55 5.212 0.8657 6258.620 1.6816 0.8923 -9068.3 26.02 26.16 +HPT 27.39 2.730 0.9148 155.159 1.2525 0.9044 9068.4 +LPT 72.38 4.741 0.9210 79.063 1.4475 0.9042 10756.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2833.08 1.318 0.9406 0.852 2.0423 0.5215 1.4369 0.9679 3943.9586 +LPC 165.57 1.344 0.8906 0.865 1.6319 0.9323 3.2631 0.9600 3662.6571 +HPC 196.24 20.469 0.8541 0.984 2.1344 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.072 0.9332 101.337 5.0720 1.4085 0.4249 0.9803 1.5311 +LPT 150.39 6.219 0.9198 97.475 6.2190 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4686.90 9184.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 765.79 183.50 19.582 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 765.79 183.50 19.582 +Duct1 0.0025 0.3957 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 765.79 183.50 19.582 +Duct2 0.0025 0.4215 365.99 +Duct3 0.0050 0.2972 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3540 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.1831 1037.35 250.29 63.112 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.4305 1037.35 250.29 63.112 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 481.80 115.12 5.738 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9880 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6825.5 6978.0 9068.4 +LP_Shaft 3052.4 18508.2 10756.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1935.13 0.9940 0.0550 0.77817 0.01371 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.995 0.9976 1.0000 0.9975 2706.36 1.000 980.0 11790.9 +Core_Nozz 1.590 0.9999 1.0000 0.9999 862.88 0.847 1241.2 2436.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 362 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 39000.0 0.00 398.86 3362.2 0.5853 1967.86 6.7042 677.94 12.543 1743.8 1702.5 1335.7 + core size:20.92 Q: 141.08 Maximum Thrust: 8405.2 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 398.86 3.959 428.31 102.31 0.0000 1345.40 2.854 389.97 4289.0 0.7000 1.40132 +FS_2 Inlet.Fl_O 398.86 3.939 428.31 102.31 0.0000 1352.18 3.475 413.19 5943.4 0.4271 1.40132 +FS_21 Fan.Fl_O 398.86 5.265 469.10 112.08 0.0000 1058.77 4.598 451.25 4515.2 0.4439 1.40121 +FS_13 Splitter.Fl_O2 347.09 5.265 469.10 112.08 0.0000 921.34 4.541 449.63 3795.6 0.4645 1.40121 +FS_22 Splitter.Fl_O1 51.77 5.265 469.10 112.08 0.0000 137.43 4.847 458.12 719.5 0.3456 1.40121 +FS_23 Duct1.Fl_O 51.77 5.252 469.10 112.08 0.0000 137.77 4.835 458.12 721.3 0.3456 1.40121 +FS_24 LPC.Fl_O 51.77 10.145 584.07 139.65 0.0000 79.58 9.068 565.64 366.0 0.4039 1.39929 +FS_25 Duct2.Fl_O 51.77 10.120 584.07 139.65 0.0000 79.78 9.045 565.64 366.9 0.4039 1.39929 +FS_3 HPC.Fl_O 51.77 49.659 966.61 232.70 0.0000 20.92 46.421 948.71 119.9 0.3136 1.38278 +FS_36 Bld3.Fl_O 47.11 49.659 966.61 232.70 0.0000 19.03 46.421 948.71 109.1 0.3136 1.38278 +FS_4 Burner.Fl_O 47.66 46.928 1743.84 439.87 0.0116 27.37 46.626 1741.05 483.4 0.0985 1.33017 +FS_45 HPT.Fl_O 52.32 17.027 1335.65 329.34 0.0106 72.46 16.041 1315.02 439.1 0.2981 1.35229 +FS_48 Duct3.Fl_O 52.32 16.942 1335.65 329.34 0.0106 72.83 15.961 1315.02 441.4 0.2981 1.35229 +FS_5 LPT.Fl_O 52.32 3.929 939.10 227.61 0.0106 263.34 3.660 921.04 1477.4 0.3220 1.37745 +FS_7 Duct4.Fl_O 52.32 3.889 939.10 227.61 0.0106 266.00 3.750 929.71 2018.9 0.2312 1.37745 +FS_9 Core_Nozz.Fl_O 52.32 3.889 939.10 227.61 0.0106 266.00 2.854 862.46 862.8 0.6834 1.37745 +FS_15 BypBld.Fl_O 347.09 5.265 469.10 112.08 0.0000 921.34 4.541 449.63 3795.6 0.4645 1.40121 +FS_17 Duct5.Fl_O 347.09 5.226 469.10 112.08 0.0000 928.30 4.507 449.63 3824.3 0.4645 1.40121 +FS_19 Byp_Nozz.Fl_O 347.09 5.226 469.10 112.08 0.0000 928.30 2.854 394.48 2706.3 0.9709 1.40121 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1352.18 1.337 0.9095 3024.231 1.0952 0.9131 -5510.1 47.74 21.62 +LPC 137.77 1.932 0.8453 2889.756 1.2451 0.8590 -2019.4 23.83 13.56 +HPC 79.78 4.907 0.8648 6210.168 1.6550 0.8908 -6816.1 30.51 30.73 +HPT 27.37 2.756 0.9153 157.811 1.2615 0.9046 6816.1 +LPT 72.83 4.312 0.9173 75.197 1.4223 0.9004 7529.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2592.62 1.234 0.9396 0.767 2.0842 0.5215 1.4369 0.9679 3943.9586 +LPC 147.78 1.286 0.8805 0.789 1.5652 0.9323 3.2631 0.9600 3662.6571 +HPC 189.67 19.061 0.8532 0.977 2.1668 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.133 0.9337 103.069 5.1330 1.4085 0.4249 0.9803 1.5311 +LPT 151.32 5.621 0.9161 92.709 5.6207 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4289.04 8404.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 719.22 172.21 15.913 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 719.22 172.21 15.913 +Duct1 0.0025 0.3456 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 719.22 172.21 15.913 +Duct2 0.0025 0.4039 365.99 +Duct3 0.0050 0.2981 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3220 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.8120 966.61 232.70 49.659 +Duct5 0.0075 0.4645 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.8475 966.61 232.70 49.659 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 469.10 112.08 5.265 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.7042 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6590.1 5432.3 6816.1 +LP_Shaft 2748.2 14390.1 7529.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1743.84 0.9940 0.0550 0.54663 0.01160 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.831 0.9975 1.0000 0.9975 2706.36 0.971 943.4 10177.2 +Core_Nozz 1.363 0.9999 1.0000 0.9999 862.88 0.683 977.4 1589.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 363 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 39000.0 0.00 352.31 1681.0 0.6998 1176.44 7.8609 677.94 8.910 1496.3 1462.7 1137.5 + core size:21.49 Q: 141.08 Maximum Thrust: 8405.2 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 352.31 3.959 428.31 102.31 0.0000 1188.38 2.854 389.97 3788.5 0.7000 1.40132 +FS_2 Inlet.Fl_O 352.31 3.939 428.31 102.31 0.0000 1194.36 3.589 417.05 5943.4 0.3669 1.40132 +FS_21 Fan.Fl_O 352.31 4.729 454.18 108.51 0.0000 1024.55 4.174 438.25 4515.2 0.4257 1.40131 +FS_13 Splitter.Fl_O2 312.55 4.729 454.18 108.51 0.0000 908.93 4.099 435.97 3795.6 0.4563 1.40131 +FS_22 Splitter.Fl_O1 39.76 4.729 454.18 108.51 0.0000 115.63 4.471 446.94 719.5 0.2842 1.40131 +FS_23 Duct1.Fl_O 39.76 4.717 454.18 108.51 0.0000 115.92 4.459 446.94 721.3 0.2842 1.40131 +FS_24 LPC.Fl_O 39.76 7.896 540.73 129.24 0.0000 75.56 7.150 525.62 366.0 0.3791 1.40009 +FS_25 Duct2.Fl_O 39.76 7.876 540.73 129.24 0.0000 75.75 7.132 525.62 366.9 0.3791 1.40009 +FS_3 HPC.Fl_O 39.76 35.274 872.75 209.59 0.0000 21.49 32.836 855.43 119.9 0.3227 1.38841 +FS_36 Bld3.Fl_O 36.18 35.274 872.75 209.59 0.0000 19.55 32.836 855.43 109.1 0.3227 1.38841 +FS_4 Burner.Fl_O 36.51 33.334 1496.25 371.47 0.0090 27.34 33.120 1493.79 483.4 0.0979 1.34410 +FS_45 HPT.Fl_O 40.09 11.952 1137.50 277.33 0.0082 73.00 11.249 1119.14 439.1 0.2989 1.36635 +FS_48 Duct3.Fl_O 40.09 11.892 1137.50 277.33 0.0082 73.36 11.192 1119.14 441.4 0.2989 1.36635 +FS_5 LPT.Fl_O 40.09 3.422 838.67 202.34 0.0082 218.94 3.264 827.75 1477.4 0.2616 1.38484 +FS_7 Duct4.Fl_O 40.09 3.387 838.67 202.34 0.0082 221.15 3.304 832.89 2018.9 0.1897 1.38484 +FS_9 Core_Nozz.Fl_O 40.09 3.387 838.67 202.34 0.0082 221.15 2.854 799.58 862.9 0.5033 1.38484 +FS_15 BypBld.Fl_O 312.55 4.729 454.18 108.51 0.0000 908.93 4.099 435.97 3795.6 0.4563 1.40131 +FS_17 Duct5.Fl_O 312.55 4.693 454.18 108.51 0.0000 915.79 4.068 435.97 3824.3 0.4563 1.40131 +FS_19 Byp_Nozz.Fl_O 312.55 4.693 454.18 108.51 0.0000 915.79 2.854 393.86 2706.4 0.8736 1.40131 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1194.36 1.200 0.8890 2556.813 1.0604 0.8919 -3087.1 57.83 23.56 +LPC 115.92 1.674 0.8334 2482.918 1.1906 0.8451 -1166.5 24.86 10.35 +HPC 75.75 4.479 0.8630 6135.134 1.6140 0.8881 -4519.6 37.56 38.08 +HPT 27.34 2.789 0.9163 161.945 1.2744 0.9051 4519.6 +LPT 73.36 3.475 0.9101 68.890 1.3563 0.8948 4253.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2290.03 1.139 0.9185 0.648 2.2529 0.5215 1.4369 0.9679 3943.9586 +LPC 124.33 1.207 0.8681 0.678 1.5394 0.9323 3.2631 0.9600 3662.6571 +HPC 180.09 17.082 0.8514 0.965 2.2377 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.211 0.9346 105.769 5.2109 1.4085 0.4249 0.9803 1.5311 +LPT 152.44 4.453 0.9090 84.933 4.4532 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3788.47 7423.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 657.72 157.36 11.890 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 657.72 157.36 11.890 +Duct1 0.0025 0.2842 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 657.72 157.36 11.890 +Duct2 0.0025 0.3791 365.99 +Duct3 0.0050 0.2989 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2616 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.3916 872.75 209.59 35.274 +Duct5 0.0075 0.4563 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.1868 872.75 209.59 35.274 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 454.18 108.51 4.729 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8609 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6264.3 3789.4 4519.6 +LP_Shaft 2323.4 9615.1 4253.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1496.25 0.9940 0.0550 0.32679 0.00903 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.645 0.9975 1.0000 0.9975 2706.36 0.874 848.2 8239.6 +Core_Nozz 1.187 0.9999 1.0000 0.9999 862.88 0.503 694.2 865.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 364 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 11/ 21/ 1/ 9 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 39000.0 0.00 305.33 420.3 1.4017 589.10 9.6188 677.94 5.798 1213.7 1189.3 916.0 + core size:22.39 Q: 141.08 Maximum Thrust: 8405.2 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 305.33 3.959 428.31 102.31 0.0000 1029.90 2.854 389.97 3283.3 0.7000 1.40132 +FS_2 Inlet.Fl_O 305.33 3.939 428.31 102.31 0.0000 1035.09 3.684 420.16 5943.4 0.3110 1.40132 +FS_21 Fan.Fl_O 305.33 4.269 440.96 105.34 0.0000 969.06 3.829 427.42 4515.2 0.3972 1.40134 +FS_13 Splitter.Fl_O2 276.57 4.269 440.96 105.34 0.0000 877.80 3.746 424.74 3795.6 0.4361 1.40134 +FS_22 Splitter.Fl_O1 28.75 4.269 440.96 105.34 0.0000 91.26 4.128 436.71 719.5 0.2201 1.40134 +FS_23 Duct1.Fl_O 28.75 4.259 440.96 105.34 0.0000 91.49 4.117 436.71 721.3 0.2201 1.40134 +FS_24 LPC.Fl_O 28.75 5.946 494.82 118.24 0.0000 69.41 5.481 483.43 366.0 0.3428 1.40090 +FS_25 Duct2.Fl_O 28.75 5.931 494.82 118.24 0.0000 69.59 5.467 483.43 366.9 0.3428 1.40090 +FS_3 HPC.Fl_O 28.75 22.954 767.27 183.86 0.0000 22.39 21.219 750.42 119.9 0.3376 1.39352 +FS_36 Bld3.Fl_O 26.17 22.954 767.27 183.86 0.0000 20.38 21.219 750.42 109.1 0.3376 1.39352 +FS_4 Burner.Fl_O 26.33 21.691 1213.75 296.42 0.0063 27.29 21.553 1211.68 483.4 0.0970 1.36286 +FS_45 HPT.Fl_O 28.92 7.695 916.03 221.10 0.0057 73.39 7.238 900.62 439.1 0.2990 1.38207 +FS_48 Duct3.Fl_O 28.92 7.657 916.03 221.10 0.0057 73.76 7.202 900.62 441.4 0.2990 1.38207 +FS_5 LPT.Fl_O 28.92 3.126 733.74 176.32 0.0057 161.68 3.050 728.63 1477.4 0.1891 1.39143 +FS_7 Duct4.Fl_O 28.92 3.095 733.74 176.32 0.0057 163.32 3.054 730.99 2018.9 0.1384 1.39143 +FS_9 Core_Nozz.Fl_O 28.92 3.095 733.74 176.32 0.0057 163.32 2.854 717.19 862.8 0.3432 1.39143 +FS_15 BypBld.Fl_O 276.57 4.269 440.96 105.34 0.0000 877.80 3.746 424.74 3795.6 0.4361 1.40134 +FS_17 Duct5.Fl_O 276.57 4.237 440.96 105.34 0.0000 884.43 3.718 424.74 3824.3 0.4361 1.40134 +FS_19 Byp_Nozz.Fl_O 276.57 4.237 440.96 105.34 0.0000 884.43 2.854 393.75 2706.4 0.7730 1.40134 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1035.09 1.084 0.7896 1986.772 1.0295 0.7920 -1307.5 83.26 24.31 +LPC 91.49 1.396 0.8207 1958.080 1.1222 0.8290 -524.7 31.03 8.64 +HPC 69.59 3.870 0.8541 6022.192 1.5506 0.8786 -2669.6 49.40 50.39 +HPT 27.29 2.819 0.9179 168.838 1.2900 0.9062 2669.6 +LPT 73.76 2.449 0.8999 59.652 1.2484 0.8879 1832.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1984.64 1.058 0.8157 0.504 2.6195 0.5215 1.4369 0.9679 3943.9586 +LPC 98.13 1.121 0.8549 0.535 1.6024 0.9323 3.2631 0.9600 3662.6571 +HPC 165.43 14.268 0.8426 0.947 2.3784 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.281 0.9363 110.271 5.2808 1.4085 0.4249 0.9803 1.5311 +LPT 153.26 3.022 0.8987 73.544 3.0217 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3283.26 6433.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 590.56 141.21 8.425 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 590.56 141.21 8.425 +Duct1 0.0025 0.2201 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 590.56 141.21 8.425 +Duct2 0.0025 0.3428 365.99 +Duct3 0.0050 0.2990 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1891 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.0064 767.27 183.86 22.954 +Duct5 0.0075 0.4361 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 1.5814 767.27 183.86 22.954 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 440.96 105.34 4.269 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.6188 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 5882.1 2383.7 2669.6 +LP_Shaft 1805.4 5329.8 1832.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1213.75 0.9940 0.0550 0.16364 0.00625 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.485 0.9975 1.0000 0.9975 2706.36 0.773 750.3 6450.1 +Core_Nozz 1.084 0.9999 1.0000 0.9999 862.88 0.343 449.3 403.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 365 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 39000.0 0.00 513.96 8584.0 0.5846 5018.18 5.0391 726.36 22.736 2303.6 2244.8 1794.3 + core size:19.96 Q: 161.96 Maximum Thrust: 8584.0 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 513.96 4.145 433.98 103.67 0.0000 1666.72 2.854 389.97 5158.3 0.7500 1.40134 +FS_2 Inlet.Fl_O 513.96 4.125 433.98 103.67 0.0000 1675.11 3.293 406.87 5943.4 0.5763 1.40134 +FS_21 Fan.Fl_O 513.96 6.783 510.54 122.00 0.0000 1104.79 5.831 488.93 4515.2 0.4696 1.40066 +FS_13 Splitter.Fl_O2 428.85 6.783 510.54 122.00 0.0000 921.85 5.848 489.34 3795.6 0.4649 1.40066 +FS_22 Splitter.Fl_O1 85.11 6.783 510.54 122.00 0.0000 182.94 5.737 486.66 719.5 0.4948 1.40066 +FS_23 Duct1.Fl_O 85.11 6.766 510.54 122.00 0.0000 183.40 5.723 486.66 721.3 0.4948 1.40066 +FS_24 LPC.Fl_O 85.11 16.826 685.02 163.95 0.0000 85.42 14.717 659.44 366.0 0.4420 1.39653 +FS_25 Duct2.Fl_O 85.11 16.784 685.02 163.95 0.0000 85.64 14.680 659.44 366.9 0.4420 1.39653 +FS_3 HPC.Fl_O 85.11 94.246 1173.22 284.50 0.0000 19.96 88.686 1154.10 119.9 0.2990 1.36983 +FS_36 Bld3.Fl_O 77.45 94.246 1173.22 284.50 0.0000 18.16 88.686 1154.10 109.1 0.2990 1.36983 +FS_4 Burner.Fl_O 78.84 89.062 2303.56 602.94 0.0180 27.42 88.488 2300.06 483.4 0.0996 1.30631 +FS_45 HPT.Fl_O 86.50 33.335 1794.29 456.13 0.0164 70.93 31.488 1769.37 439.1 0.2943 1.32468 +FS_48 Duct3.Fl_O 86.50 33.168 1794.29 456.13 0.0164 71.28 31.330 1769.37 441.4 0.2943 1.32468 +FS_5 LPT.Fl_O 86.50 6.773 1240.38 305.94 0.0164 290.26 6.198 1211.90 1477.4 0.3636 1.35433 +FS_7 Duct4.Fl_O 86.50 6.705 1240.38 305.94 0.0164 293.20 6.409 1225.80 2018.9 0.2589 1.35433 +FS_9 Core_Nozz.Fl_O 86.50 6.705 1240.38 305.94 0.0164 293.20 3.578 1050.25 862.9 1.0000 1.35433 +FS_15 BypBld.Fl_O 428.85 6.783 510.54 122.00 0.0000 921.85 5.848 489.34 3795.6 0.4649 1.40066 +FS_17 Duct5.Fl_O 428.85 6.732 510.54 122.00 0.0000 928.81 5.804 489.34 3824.3 0.4649 1.40066 +FS_19 Byp_Nozz.Fl_O 428.85 6.732 510.54 122.00 0.0000 928.81 3.555 425.23 2706.4 1.0000 1.40066 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.645 0.8675 3944.235 1.1764 0.8765 -13330.8 24.71 17.45 +LPC 183.40 2.487 0.8684 3636.500 1.3417 0.8841 -5050.5 28.45 23.35 +HPC 85.64 5.615 0.8650 6327.797 1.7127 0.8924 -14516.3 20.04 20.09 +HPT 27.42 2.672 0.9132 151.516 1.2357 0.9033 14516.4 +LPT 71.28 4.897 0.9321 85.174 1.4466 0.9175 18381.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8963 1.000 2.3708 0.5215 1.4369 0.9679 3943.9586 +LPC 196.72 1.456 0.9046 0.993 1.7683 0.9323 3.2631 0.9600 3662.6571 +HPC 203.59 22.335 0.8534 0.995 2.0426 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.935 0.9315 98.958 4.9346 1.4085 0.4249 0.9803 1.5311 +LPT 148.12 6.437 0.9309 105.009 6.4368 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5158.28 11603.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 858.69 206.14 28.132 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 858.69 206.14 28.132 +Duct1 0.0025 0.4948 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 858.69 206.14 28.132 +Duct2 0.0025 0.4420 365.99 +Duct3 0.0050 0.2943 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.9787 1173.22 284.50 94.246 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.6808 1173.22 284.50 94.246 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 510.54 122.00 6.783 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0391 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7272.1 10484.2 14516.4 +LP_Shaft 3607.9 26758.1 18381.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2303.56 0.9940 0.0550 1.39394 0.01800 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.359 0.9968 1.0000 0.9975 2706.36 1.000 1008.8 15343.1 +Core_Nozz 2.349 0.9987 1.0000 0.9999 862.88 1.000 1569.3 4844.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 366 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 39000.0 0.00 501.01 7725.3 0.5744 4437.56 5.3030 726.36 20.829 2219.7 2163.4 1722.6 + core size:20.05 Q: 161.96 Maximum Thrust: 8584.0 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 501.01 4.145 433.98 103.67 0.0000 1624.73 2.854 389.97 5028.3 0.7500 1.40134 +FS_2 Inlet.Fl_O 501.01 4.125 433.98 103.67 0.0000 1632.91 3.348 408.83 5943.4 0.5538 1.40134 +FS_21 Fan.Fl_O 501.01 6.629 504.72 120.61 0.0000 1095.72 5.717 483.80 4515.2 0.4644 1.40075 +FS_13 Splitter.Fl_O2 421.52 6.629 504.72 120.61 0.0000 921.88 5.715 483.75 3795.6 0.4650 1.40075 +FS_22 Splitter.Fl_O1 79.49 6.629 504.72 120.61 0.0000 173.84 5.727 484.03 719.5 0.4617 1.40075 +FS_23 Duct1.Fl_O 79.49 6.612 504.72 120.61 0.0000 174.28 5.712 484.03 721.3 0.4617 1.40075 +FS_24 LPC.Fl_O 79.49 15.397 663.73 158.81 0.0000 85.82 13.446 638.62 366.0 0.4445 1.39731 +FS_25 Duct2.Fl_O 79.49 15.358 663.73 158.81 0.0000 86.04 13.412 638.62 366.9 0.4445 1.39731 +FS_3 HPC.Fl_O 79.49 86.342 1139.37 275.93 0.0000 20.05 81.199 1120.54 119.9 0.3003 1.37196 +FS_36 Bld3.Fl_O 72.33 86.342 1139.37 275.93 0.0000 18.25 81.199 1120.54 109.1 0.3003 1.37196 +FS_4 Burner.Fl_O 73.57 81.594 2219.70 577.85 0.0170 27.41 81.067 2216.31 483.4 0.0995 1.30922 +FS_45 HPT.Fl_O 80.72 30.237 1722.60 435.77 0.0155 71.50 28.533 1698.04 439.1 0.2964 1.32847 +FS_48 Duct3.Fl_O 80.72 30.086 1722.60 435.77 0.0155 71.86 28.390 1698.04 441.4 0.2964 1.32847 +FS_5 LPT.Fl_O 80.72 6.187 1191.75 293.03 0.0155 290.65 5.660 1164.10 1477.4 0.3637 1.35800 +FS_7 Duct4.Fl_O 80.72 6.125 1191.75 293.03 0.0155 293.59 5.854 1177.60 2018.9 0.2589 1.35800 +FS_9 Core_Nozz.Fl_O 80.72 6.125 1191.75 293.03 0.0155 293.59 3.267 1007.59 862.9 1.0000 1.35800 +FS_15 BypBld.Fl_O 421.52 6.629 504.72 120.61 0.0000 921.88 5.715 483.75 3795.6 0.4650 1.40075 +FS_17 Duct5.Fl_O 421.52 6.579 504.72 120.61 0.0000 928.85 5.672 483.75 3824.3 0.4650 1.40075 +FS_19 Byp_Nozz.Fl_O 421.52 6.579 504.72 120.61 0.0000 928.85 3.474 420.38 2706.4 1.0000 1.40075 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1632.91 1.607 0.8925 3741.940 1.1630 0.8995 -12006.0 28.23 17.74 +LPC 174.28 2.329 0.8661 3469.831 1.3150 0.8810 -4296.3 28.96 22.23 +HPC 86.04 5.622 0.8639 6337.938 1.7166 0.8917 -13171.3 20.45 20.48 +HPT 27.41 2.698 0.9137 152.177 1.2407 0.9036 13171.3 +LPT 71.86 4.863 0.9276 82.470 1.4454 0.9121 16301.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3130.65 1.423 0.9221 0.949 2.1749 0.5215 1.4369 0.9679 3943.9586 +LPC 186.93 1.407 0.9022 0.947 1.7539 0.9323 3.2631 0.9600 3662.6571 +HPC 204.54 22.366 0.8523 0.997 2.0720 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.998 0.9321 99.390 4.9976 1.4085 0.4249 0.9803 1.5311 +LPT 149.30 6.389 0.9264 101.675 6.3888 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5028.33 11310.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 832.75 199.80 25.758 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 832.75 199.80 25.758 +Duct1 0.0025 0.4617 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 832.75 199.80 25.758 +Duct2 0.0025 0.4445 365.99 +Duct3 0.0050 0.2964 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3637 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.7821 1139.37 275.93 86.342 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.3718 1139.37 275.93 86.342 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 504.72 120.61 6.629 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3030 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7169.6 9648.7 13171.3 +LP_Shaft 3422.9 25013.7 16301.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2219.70 0.9940 0.0550 1.23265 0.01704 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.305 0.9970 1.0000 0.9975 2706.36 1.000 1003.0 14818.9 +Core_Nozz 2.146 0.9996 1.0000 0.9999 862.88 1.000 1539.0 4217.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 367 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 39000.0 0.00 486.40 6867.2 0.5702 3915.50 5.5090 726.36 19.189 2134.0 2080.5 1652.1 + core size:20.20 Q: 161.96 Maximum Thrust: 8584.0 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 486.40 4.145 433.98 103.67 0.0000 1577.36 2.854 389.97 4881.7 0.7500 1.40134 +FS_2 Inlet.Fl_O 486.40 4.125 433.98 103.67 0.0000 1585.30 3.406 410.85 5943.4 0.5298 1.40134 +FS_21 Fan.Fl_O 486.40 6.440 499.41 119.34 0.0000 1089.22 5.567 479.02 4515.2 0.4608 1.40083 +FS_13 Splitter.Fl_O2 411.68 6.440 499.41 119.34 0.0000 921.88 5.552 478.66 3795.6 0.4649 1.40083 +FS_22 Splitter.Fl_O1 74.73 6.440 499.41 119.34 0.0000 167.34 5.640 480.81 719.5 0.4393 1.40083 +FS_23 Duct1.Fl_O 74.73 6.424 499.41 119.34 0.0000 167.76 5.626 480.81 721.3 0.4393 1.40083 +FS_24 LPC.Fl_O 74.73 14.488 650.66 155.66 0.0000 84.90 12.698 626.68 366.0 0.4383 1.39779 +FS_25 Duct2.Fl_O 74.73 14.452 650.66 155.66 0.0000 85.11 12.666 626.68 366.9 0.4383 1.39779 +FS_3 HPC.Fl_O 74.73 79.542 1110.42 268.62 0.0000 20.20 74.728 1091.69 119.9 0.3026 1.37379 +FS_36 Bld3.Fl_O 68.00 79.542 1110.42 268.62 0.0000 18.38 74.728 1091.69 109.1 0.3026 1.37379 +FS_4 Burner.Fl_O 69.09 75.167 2134.01 552.40 0.0160 27.40 74.683 2130.73 483.4 0.0993 1.31238 +FS_45 HPT.Fl_O 75.82 27.720 1652.07 415.89 0.0146 71.74 26.147 1628.14 439.1 0.2971 1.33243 +FS_48 Duct3.Fl_O 75.82 27.581 1652.07 415.89 0.0146 72.10 26.016 1628.14 441.4 0.2971 1.33243 +FS_5 LPT.Fl_O 75.82 5.678 1140.69 279.58 0.0146 291.00 5.194 1113.95 1477.4 0.3636 1.36191 +FS_7 Duct4.Fl_O 75.82 5.621 1140.69 279.58 0.0146 293.94 5.372 1127.00 2018.9 0.2589 1.36191 +FS_9 Core_Nozz.Fl_O 75.82 5.621 1140.69 279.58 0.0146 293.94 2.996 962.93 862.9 1.0000 1.36191 +FS_15 BypBld.Fl_O 411.68 6.440 499.41 119.34 0.0000 921.88 5.552 478.66 3795.6 0.4649 1.40083 +FS_17 Duct5.Fl_O 411.68 6.391 499.41 119.34 0.0000 928.85 5.511 478.66 3824.3 0.4649 1.40083 +FS_19 Byp_Nozz.Fl_O 411.68 6.391 499.41 119.34 0.0000 928.85 3.375 415.96 2706.4 1.0000 1.40083 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1585.30 1.561 0.9024 3613.219 1.1508 0.9083 -10780.6 31.70 18.33 +LPC 167.76 2.255 0.8632 3368.232 1.3029 0.8778 -3840.6 28.08 20.51 +HPC 85.11 5.504 0.8648 6313.835 1.7066 0.8922 -11942.8 22.08 22.15 +HPT 27.40 2.712 0.9144 153.083 1.2444 0.9042 11942.7 +LPT 72.10 4.857 0.9256 81.315 1.4483 0.9096 14621.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3039.63 1.391 0.9322 0.916 2.0965 0.5215 1.4369 0.9679 3943.9586 +LPC 179.95 1.385 0.8991 0.920 1.7169 0.9323 3.2631 0.9600 3662.6571 +HPC 202.35 21.821 0.8531 0.993 2.0965 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 5.029 0.9328 99.981 5.0286 1.4085 0.4249 0.9803 1.5311 +LPT 149.81 6.381 0.9244 100.251 6.3811 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4881.74 10981.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 813.88 195.20 23.987 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 813.88 195.20 23.987 +Duct1 0.0025 0.4393 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 813.88 195.20 23.987 +Duct2 0.0025 0.4383 365.99 +Duct3 0.0050 0.2971 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.6155 1110.42 268.62 79.542 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.1100 1110.42 268.62 79.542 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 499.41 119.34 6.440 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5090 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7071.7 8869.8 11942.7 +LP_Shaft 3305.1 23234.6 14621.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2134.01 0.9940 0.0550 1.08764 0.01599 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.240 0.9972 1.0000 0.9975 2706.36 1.000 997.7 14176.2 +Core_Nozz 1.970 0.9999 1.0000 0.9999 862.88 1.000 1506.4 3672.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 368 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 39000.0 0.00 454.22 5150.4 0.5752 2962.39 5.9839 726.36 15.977 1959.0 1911.2 1510.0 + core size:20.55 Q: 161.96 Maximum Thrust: 8584.0 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 454.22 4.145 433.98 103.67 0.0000 1472.98 2.854 389.97 4558.7 0.7500 1.40134 +FS_2 Inlet.Fl_O 454.22 4.125 433.98 103.67 0.0000 1480.40 3.520 414.73 5943.4 0.4810 1.40134 +FS_21 Fan.Fl_O 454.22 6.021 488.50 116.72 0.0000 1076.00 5.228 469.16 4515.2 0.4534 1.40098 +FS_13 Splitter.Fl_O2 389.18 6.021 488.50 116.72 0.0000 921.93 5.191 468.20 3795.6 0.4650 1.40098 +FS_22 Splitter.Fl_O1 65.04 6.021 488.50 116.72 0.0000 154.07 5.403 473.60 719.5 0.3961 1.40098 +FS_23 Duct1.Fl_O 65.04 6.006 488.50 116.72 0.0000 154.46 5.390 473.60 721.3 0.3961 1.40098 +FS_24 LPC.Fl_O 65.04 12.782 626.19 149.77 0.0000 82.16 11.320 604.87 366.0 0.4203 1.39852 +FS_25 Duct2.Fl_O 65.04 12.750 626.19 149.77 0.0000 82.37 11.292 604.87 366.9 0.4203 1.39852 +FS_3 HPC.Fl_O 65.04 66.228 1051.35 253.79 0.0000 20.55 62.071 1032.82 119.9 0.3080 1.37750 +FS_36 Bld3.Fl_O 59.18 66.228 1051.35 253.79 0.0000 18.70 62.071 1032.82 109.1 0.3080 1.37750 +FS_4 Burner.Fl_O 60.01 62.585 1959.01 501.19 0.0139 27.38 62.183 1955.94 483.4 0.0990 1.31973 +FS_45 HPT.Fl_O 65.86 22.938 1510.04 376.48 0.0127 72.00 21.627 1487.58 439.1 0.2973 1.34088 +FS_48 Duct3.Fl_O 65.86 22.824 1510.04 376.48 0.0127 72.36 21.519 1487.58 441.4 0.2973 1.34088 +FS_5 LPT.Fl_O 65.86 4.765 1041.67 253.84 0.0127 287.89 4.368 1017.51 1477.4 0.3580 1.36953 +FS_7 Duct4.Fl_O 65.86 4.717 1041.67 253.84 0.0127 290.80 4.512 1029.27 2018.9 0.2551 1.36953 +FS_9 Core_Nozz.Fl_O 65.86 4.717 1041.67 253.84 0.0127 290.80 2.854 908.49 862.9 0.8842 1.36953 +FS_15 BypBld.Fl_O 389.18 6.021 488.50 116.72 0.0000 921.93 5.191 468.20 3795.6 0.4650 1.40098 +FS_17 Duct5.Fl_O 389.18 5.975 488.50 116.72 0.0000 928.90 5.152 468.20 3824.3 0.4650 1.40098 +FS_19 Byp_Nozz.Fl_O 389.18 5.975 488.50 116.72 0.0000 928.90 3.155 406.87 2706.4 1.0000 1.40098 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1480.40 1.460 0.9104 3366.098 1.1256 0.9151 -8387.7 39.52 19.74 +LPC 154.46 2.128 0.8547 3172.713 1.2818 0.8692 -3040.9 25.36 16.72 +HPC 82.37 5.194 0.8658 6255.155 1.6790 0.8923 -9571.9 26.22 26.37 +HPT 27.38 2.728 0.9148 155.284 1.2516 0.9045 9572.0 +LPT 72.36 4.790 0.9208 79.236 1.4496 0.9039 11428.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2838.38 1.320 0.9406 0.853 2.0411 0.5215 1.4369 0.9679 3943.9586 +LPC 165.67 1.346 0.8903 0.866 1.6263 0.9323 3.2631 0.9600 3662.6571 +HPC 195.81 20.389 0.8541 0.984 2.1344 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.068 0.9332 101.418 5.0680 1.4085 0.4249 0.9803 1.5311 +LPT 150.35 6.287 0.9196 97.689 6.2873 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4558.69 10254.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 776.82 186.18 20.585 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 776.82 186.18 20.585 +Duct1 0.0025 0.3961 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 776.82 186.18 20.585 +Duct2 0.0025 0.4203 365.99 +Duct3 0.0050 0.2973 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3580 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.2763 1051.35 253.79 66.228 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.5771 1051.35 253.79 66.228 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 488.50 116.72 6.021 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9839 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6873.0 7314.6 9572.0 +LP_Shaft 3079.1 19494.1 11428.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1959.01 0.9940 0.0550 0.82289 0.01390 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.094 0.9975 1.0000 0.9975 2706.36 1.000 986.8 12752.0 +Core_Nozz 1.653 0.9999 1.0000 0.9999 862.88 0.884 1296.0 2652.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 369 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 39000.0 0.00 416.62 3433.7 0.6068 2083.43 6.6965 726.36 12.606 1765.4 1723.7 1353.4 + core size:20.93 Q: 161.96 Maximum Thrust: 8584.0 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 416.62 4.145 433.98 103.67 0.0000 1351.06 2.854 389.97 4181.4 0.7500 1.40134 +FS_2 Inlet.Fl_O 416.62 4.125 433.98 103.67 0.0000 1357.87 3.633 418.50 5943.4 0.4294 1.40134 +FS_21 Fan.Fl_O 416.62 5.534 475.89 113.70 0.0000 1059.67 4.832 457.75 4515.2 0.4444 1.40114 +FS_13 Splitter.Fl_O2 362.49 5.534 475.89 113.70 0.0000 921.99 4.772 456.10 3795.6 0.4650 1.40114 +FS_22 Splitter.Fl_O1 54.13 5.534 475.89 113.70 0.0000 137.68 5.093 464.70 719.5 0.3464 1.40114 +FS_23 Duct1.Fl_O 54.13 5.521 475.89 113.70 0.0000 138.03 5.081 464.70 721.3 0.3464 1.40114 +FS_24 LPC.Fl_O 54.13 10.740 593.97 142.03 0.0000 79.27 9.609 575.41 366.0 0.4019 1.39913 +FS_25 Duct2.Fl_O 54.13 10.713 593.97 142.03 0.0000 79.47 9.585 575.41 366.9 0.4019 1.39913 +FS_3 HPC.Fl_O 54.13 52.254 980.72 236.20 0.0000 20.93 48.840 962.56 119.9 0.3140 1.38191 +FS_36 Bld3.Fl_O 49.26 52.254 980.72 236.20 0.0000 19.05 48.840 962.56 109.1 0.3140 1.38191 +FS_4 Burner.Fl_O 49.84 49.380 1765.42 445.90 0.0117 27.36 49.063 1762.60 483.4 0.0985 1.32911 +FS_45 HPT.Fl_O 54.71 17.935 1353.40 334.05 0.0107 72.42 16.897 1332.57 439.1 0.2980 1.35112 +FS_48 Duct3.Fl_O 54.71 17.845 1353.40 334.05 0.0107 72.78 16.813 1332.57 441.4 0.2980 1.35112 +FS_5 LPT.Fl_O 54.71 4.040 947.10 229.64 0.0107 268.94 3.751 928.03 1477.4 0.3299 1.37686 +FS_7 Duct4.Fl_O 54.71 3.999 947.10 229.64 0.0107 271.66 3.849 937.22 2018.9 0.2365 1.37686 +FS_9 Core_Nozz.Fl_O 54.71 3.999 947.10 229.64 0.0107 271.66 2.854 863.22 862.9 0.7150 1.37686 +FS_15 BypBld.Fl_O 362.49 5.534 475.89 113.70 0.0000 921.99 4.772 456.10 3795.6 0.4650 1.40114 +FS_17 Duct5.Fl_O 362.49 5.493 475.89 113.70 0.0000 928.96 4.736 456.10 3824.3 0.4650 1.40114 +FS_19 Byp_Nozz.Fl_O 362.49 5.493 475.89 113.70 0.0000 928.96 2.901 396.36 2706.3 1.0000 1.40114 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1357.87 1.342 0.9097 3039.887 1.0966 0.9134 -5912.8 47.39 21.54 +LPC 138.03 1.945 0.8445 2902.968 1.2481 0.8584 -2169.2 23.28 13.31 +HPC 79.47 4.878 0.8648 6205.168 1.6511 0.8907 -7212.5 30.89 31.12 +HPT 27.36 2.753 0.9154 158.040 1.2605 0.9046 7212.5 +LPT 72.78 4.417 0.9165 75.585 1.4290 0.8993 8082.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2603.52 1.238 0.9398 0.771 2.0807 0.5215 1.4369 0.9679 3943.9586 +LPC 148.05 1.290 0.8797 0.793 1.5534 0.9323 3.2631 0.9600 3662.6571 +HPC 188.92 18.926 0.8531 0.976 2.1667 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.127 0.9337 103.219 5.1266 1.4085 0.4249 0.9803 1.5311 +LPT 151.23 5.767 0.9153 93.187 5.7670 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4181.37 9405.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 730.67 174.99 16.799 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 730.67 174.99 16.799 +Duct1 0.0025 0.3464 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 730.67 174.99 16.799 +Duct2 0.0025 0.4019 365.99 +Duct3 0.0050 0.2980 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3299 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.8946 980.72 236.20 52.254 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.9772 980.72 236.20 52.254 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 475.89 113.70 5.534 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6965 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6640.3 5704.6 7212.5 +LP_Shaft 2780.7 15265.5 8082.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1765.42 0.9940 0.0550 0.57873 0.01175 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.925 0.9975 1.0000 0.9975 2706.36 1.000 973.9 11099.9 +Core_Nozz 1.401 0.9999 1.0000 0.9999 862.88 0.715 1023.0 1739.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 370 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 39000.0 0.00 370.79 1716.9 0.7270 1248.17 7.8825 726.36 8.993 1515.5 1481.7 1153.3 + core size:21.52 Q: 161.96 Maximum Thrust: 8584.0 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 370.79 4.145 433.98 103.67 0.0000 1202.44 2.854 389.97 3721.4 0.7500 1.40134 +FS_2 Inlet.Fl_O 370.79 4.125 433.98 103.67 0.0000 1208.49 3.748 422.25 5943.4 0.3721 1.40134 +FS_21 Fan.Fl_O 370.79 4.971 460.84 110.10 0.0000 1033.18 4.377 444.33 4515.2 0.4302 1.40127 +FS_13 Splitter.Fl_O2 329.05 4.971 460.84 110.10 0.0000 916.86 4.295 441.95 3795.6 0.4615 1.40127 +FS_22 Splitter.Fl_O1 41.74 4.971 460.84 110.10 0.0000 116.32 4.696 453.39 719.5 0.2861 1.40127 +FS_23 Duct1.Fl_O 41.74 4.959 460.84 110.10 0.0000 116.61 4.685 453.39 721.3 0.2861 1.40127 +FS_24 LPC.Fl_O 41.74 8.416 551.33 131.79 0.0000 75.15 7.631 536.12 366.0 0.3766 1.39988 +FS_25 Duct2.Fl_O 41.74 8.395 551.33 131.79 0.0000 75.34 7.612 536.12 366.9 0.3766 1.39988 +FS_3 HPC.Fl_O 41.74 37.279 887.19 213.13 0.0000 21.52 34.693 869.54 119.9 0.3234 1.38760 +FS_36 Bld3.Fl_O 37.99 37.279 887.19 213.13 0.0000 19.59 34.693 869.54 109.1 0.3234 1.38760 +FS_4 Burner.Fl_O 38.33 35.229 1515.53 376.67 0.0091 27.33 35.003 1513.04 483.4 0.0979 1.34301 +FS_45 HPT.Fl_O 42.09 12.646 1153.32 281.40 0.0083 72.94 11.904 1134.78 439.1 0.2988 1.36528 +FS_48 Duct3.Fl_O 42.09 12.583 1153.32 281.40 0.0083 73.31 11.844 1134.78 441.4 0.2988 1.36528 +FS_5 LPT.Fl_O 42.09 3.481 842.42 203.27 0.0083 226.48 3.309 830.63 1477.4 0.2715 1.38460 +FS_7 Duct4.Fl_O 42.09 3.446 842.42 203.27 0.0083 228.77 3.355 836.20 2018.9 0.1966 1.38460 +FS_9 Core_Nozz.Fl_O 42.09 3.446 842.42 203.27 0.0083 228.77 2.854 799.34 862.8 0.5285 1.38460 +FS_15 BypBld.Fl_O 329.05 4.971 460.84 110.10 0.0000 916.86 4.295 441.95 3795.6 0.4615 1.40127 +FS_17 Duct5.Fl_O 329.05 4.934 460.84 110.10 0.0000 923.79 4.263 441.95 3824.3 0.4615 1.40127 +FS_19 Byp_Nozz.Fl_O 329.05 4.934 460.84 110.10 0.0000 923.79 2.854 393.95 2706.3 0.9199 1.40127 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1208.49 1.205 0.8878 2589.495 1.0619 0.8907 -3372.1 57.77 23.91 +LPC 116.61 1.697 0.8320 2512.918 1.1964 0.8441 -1280.8 23.64 10.01 +HPC 75.34 4.441 0.8629 6127.394 1.6092 0.8878 -4804.1 38.15 38.70 +HPT 27.33 2.786 0.9163 162.276 1.2734 0.9051 4804.3 +LPT 73.31 3.615 0.9109 69.748 1.3691 0.8951 4652.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2317.11 1.143 0.9172 0.657 2.2588 0.5215 1.4369 0.9679 3943.9586 +LPC 125.08 1.214 0.8667 0.686 1.5161 0.9323 3.2631 0.9600 3662.6571 +HPC 179.11 16.905 0.8512 0.964 2.2435 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.203 0.9347 105.985 5.2030 1.4085 0.4249 0.9803 1.5311 +LPT 152.32 4.648 0.9097 85.990 4.6478 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3721.39 8371.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 669.72 160.26 12.627 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 669.72 160.26 12.627 +Duct1 0.0025 0.2861 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 669.72 160.26 12.627 +Duct2 0.0025 0.3766 365.99 +Duct3 0.0050 0.2988 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2715 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.4610 887.19 213.13 37.279 +Duct5 0.0075 0.4615 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.2959 887.19 213.13 37.279 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 460.84 110.10 4.971 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8825 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6317.4 3994.1 4804.3 +LP_Shaft 2368.7 10316.7 4652.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1515.53 0.9940 0.0550 0.34672 0.00913 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.729 0.9975 1.0000 0.9975 2706.36 0.920 893.2 9134.4 +Core_Nozz 1.207 0.9999 1.0000 0.9999 862.88 0.528 728.8 953.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 371 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 11/ 21/ 1/ 9 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 39000.0 0.00 324.71 429.2 1.4705 631.13 9.6951 726.36 5.897 1234.1 1209.4 932.3 + core size:22.42 Q: 161.96 Maximum Thrust: 8584.0 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 324.71 4.145 433.98 103.67 0.0000 1053.00 2.854 389.97 3258.9 0.7500 1.40134 +FS_2 Inlet.Fl_O 324.71 4.125 433.98 103.67 0.0000 1058.31 3.844 425.31 5943.4 0.3189 1.40134 +FS_21 Fan.Fl_O 324.71 4.486 447.43 106.89 0.0000 988.05 4.002 433.05 4515.2 0.4068 1.40133 +FS_13 Splitter.Fl_O2 294.35 4.486 447.43 106.89 0.0000 895.67 3.909 430.14 3795.6 0.4476 1.40133 +FS_22 Splitter.Fl_O1 30.36 4.486 447.43 106.89 0.0000 92.38 4.333 443.01 719.5 0.2230 1.40133 +FS_23 Duct1.Fl_O 30.36 4.475 447.43 106.89 0.0000 92.61 4.322 443.01 721.3 0.2230 1.40133 +FS_24 LPC.Fl_O 30.36 6.370 505.53 120.80 0.0000 69.15 5.876 493.99 366.0 0.3414 1.40074 +FS_25 Duct2.Fl_O 30.36 6.354 505.53 120.80 0.0000 69.32 5.861 493.99 366.9 0.3414 1.40074 +FS_3 HPC.Fl_O 30.36 24.444 782.36 187.52 0.0000 22.42 22.591 765.14 119.9 0.3382 1.39280 +FS_36 Bld3.Fl_O 27.63 24.444 782.36 187.52 0.0000 20.40 22.591 765.14 109.1 0.3382 1.39280 +FS_4 Burner.Fl_O 27.80 23.099 1234.13 301.70 0.0063 27.29 22.952 1232.03 483.4 0.0971 1.36151 +FS_45 HPT.Fl_O 30.54 8.200 932.28 225.15 0.0058 73.37 7.713 916.64 439.1 0.2990 1.38101 +FS_48 Duct3.Fl_O 30.54 8.159 932.28 225.15 0.0058 73.74 7.675 916.64 441.4 0.2990 1.38101 +FS_5 LPT.Fl_O 30.54 3.156 736.86 177.09 0.0058 169.50 3.070 731.21 1477.4 0.1987 1.39126 +FS_7 Duct4.Fl_O 30.54 3.124 736.86 177.09 0.0058 171.22 3.079 733.83 2018.9 0.1453 1.39126 +FS_9 Core_Nozz.Fl_O 30.54 3.124 736.86 177.09 0.0058 171.22 2.854 718.35 862.8 0.3628 1.39126 +FS_15 BypBld.Fl_O 294.35 4.486 447.43 106.89 0.0000 895.67 3.909 430.14 3795.6 0.4476 1.40133 +FS_17 Duct5.Fl_O 294.35 4.452 447.43 106.89 0.0000 902.43 3.880 430.14 3824.3 0.4476 1.40133 +FS_19 Byp_Nozz.Fl_O 294.35 4.452 447.43 106.89 0.0000 902.43 2.854 393.92 2706.4 0.8228 1.40133 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1058.31 1.088 0.7852 2037.363 1.0310 0.7878 -1478.7 82.22 25.26 +LPC 92.61 1.424 0.8194 2006.515 1.1298 0.8282 -597.6 28.71 8.25 +HPC 69.32 3.847 0.8535 6017.366 1.5476 0.8781 -2866.0 49.87 50.87 +HPT 27.29 2.817 0.9179 169.104 1.2890 0.9064 2866.0 +LPT 73.74 2.586 0.9011 61.036 1.2652 0.8885 2076.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2029.16 1.061 0.8112 0.517 2.6314 0.5215 1.4369 0.9679 3943.9586 +LPC 99.34 1.130 0.8535 0.548 1.5624 0.9323 3.2631 0.9600 3662.6571 +HPC 164.81 14.161 0.8420 0.947 2.3811 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.276 0.9363 110.445 5.2762 1.4085 0.4249 0.9803 1.5311 +LPT 153.22 3.212 0.9000 75.250 3.2120 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3258.92 7330.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 602.83 144.15 9.004 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 602.83 144.15 9.004 +Duct1 0.0025 0.2230 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 602.83 144.15 9.004 +Duct2 0.0025 0.3414 365.99 +Duct3 0.0050 0.2990 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1987 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.0626 782.36 187.52 24.444 +Duct5 0.0075 0.4476 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 1.6698 782.36 187.52 24.444 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 447.43 106.89 4.486 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.6951 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 5940.6 2533.8 2866.0 +LP_Shaft 1863.6 5851.4 2076.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1234.13 0.9940 0.0550 0.17531 0.00635 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.560 0.9975 1.0000 0.9975 2706.36 0.823 798.9 7308.9 +Core_Nozz 1.095 0.9999 1.0000 0.9999 862.88 0.363 475.2 451.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 372 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 39000.0 0.00 535.75 8801.2 0.6041 5317.22 5.0397 774.79 22.730 2333.7 2274.2 1819.0 + core size:19.95 Q: 184.27 Maximum Thrust: 8801.2 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 535.75 4.351 440.05 105.12 0.0000 1666.72 2.854 389.97 5040.9 0.8000 1.40134 +FS_2 Inlet.Fl_O 535.75 4.329 440.05 105.12 0.0000 1675.11 3.456 412.55 5943.4 0.5763 1.40134 +FS_21 Fan.Fl_O 535.75 7.120 517.67 123.71 0.0000 1104.76 6.121 495.76 4515.2 0.4696 1.40053 +FS_13 Splitter.Fl_O2 447.04 7.120 517.67 123.71 0.0000 921.84 6.139 496.18 3795.6 0.4650 1.40053 +FS_22 Splitter.Fl_O1 88.71 7.120 517.67 123.71 0.0000 182.92 6.023 493.47 719.5 0.4947 1.40053 +FS_23 Duct1.Fl_O 88.71 7.102 517.67 123.71 0.0000 183.38 6.007 493.47 721.3 0.4947 1.40053 +FS_24 LPC.Fl_O 88.71 17.666 694.57 166.26 0.0000 85.39 15.454 668.67 366.0 0.4418 1.39620 +FS_25 Duct2.Fl_O 88.71 17.622 694.57 166.26 0.0000 85.61 15.415 668.67 366.9 0.4418 1.39620 +FS_3 HPC.Fl_O 88.71 98.902 1188.59 288.41 0.0000 19.95 93.071 1169.26 119.9 0.2990 1.36886 +FS_36 Bld3.Fl_O 80.72 98.902 1188.59 288.41 0.0000 18.16 93.071 1169.26 109.1 0.2990 1.36886 +FS_4 Burner.Fl_O 82.20 93.462 2333.66 611.97 0.0183 27.42 92.859 2330.12 483.4 0.0996 1.30529 +FS_45 HPT.Fl_O 90.18 34.993 1818.96 463.17 0.0167 70.93 33.054 1793.76 439.1 0.2944 1.32343 +FS_48 Duct3.Fl_O 90.18 34.818 1818.96 463.17 0.0167 71.28 32.889 1793.76 441.4 0.2944 1.32343 +FS_5 LPT.Fl_O 90.18 7.117 1258.99 310.89 0.0167 290.13 6.514 1230.19 1477.4 0.3636 1.35297 +FS_7 Duct4.Fl_O 90.18 7.046 1258.99 310.89 0.0167 293.06 6.735 1244.24 2018.9 0.2589 1.35297 +FS_9 Core_Nozz.Fl_O 90.18 7.046 1258.99 310.89 0.0167 293.06 3.761 1066.58 862.9 1.0000 1.35297 +FS_15 BypBld.Fl_O 447.04 7.120 517.67 123.71 0.0000 921.84 6.139 496.18 3795.6 0.4650 1.40053 +FS_17 Duct5.Fl_O 447.04 7.066 517.67 123.71 0.0000 928.81 6.093 496.18 3824.3 0.4650 1.40053 +FS_19 Byp_Nozz.Fl_O 447.04 7.066 517.67 123.71 0.0000 928.81 3.731 431.18 2706.3 1.0000 1.40053 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.645 0.8675 3944.235 1.1764 0.8766 -14090.8 24.71 17.45 +LPC 183.38 2.487 0.8684 3636.521 1.3417 0.8840 -5339.3 28.42 23.33 +HPC 85.61 5.612 0.8651 6326.949 1.7112 0.8923 -15330.8 20.06 20.11 +HPT 27.42 2.671 0.9133 151.562 1.2349 0.9034 15331.0 +LPT 71.28 4.892 0.9322 85.184 1.4448 0.9176 19430.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8963 1.000 2.3706 0.5215 1.4369 0.9679 3943.9586 +LPC 196.69 1.456 0.9045 0.993 1.7675 0.9323 3.2631 0.9600 3662.6571 +HPC 203.51 22.322 0.8534 0.995 2.0423 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.933 0.9316 98.988 4.9326 1.4085 0.4249 0.9803 1.5311 +LPT 148.11 6.430 0.9310 105.021 6.4296 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5040.92 12901.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 870.40 209.01 29.530 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 870.40 209.01 29.530 +Duct1 0.0025 0.4947 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 870.40 209.01 29.530 +Duct2 0.0025 0.4418 365.99 +Duct3 0.0050 0.2944 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.1047 1188.59 288.41 98.902 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.8788 1188.59 288.41 98.902 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 517.67 123.71 7.120 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0397 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7321.6 10997.5 15331.0 +LP_Shaft 3633.0 28089.3 19430.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2333.66 0.9940 0.0550 1.47701 0.01830 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.476 0.9962 1.0000 0.9975 2706.36 1.000 1015.9 16489.0 +Core_Nozz 2.469 0.9979 1.0000 0.9999 862.88 1.000 1580.8 5213.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 373 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 39000.0 0.00 522.31 7920.7 0.5939 4704.06 5.3025 774.79 20.832 2249.1 2192.1 1746.6 + core size:20.05 Q: 184.27 Maximum Thrust: 8801.2 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 522.31 4.351 440.05 105.12 0.0000 1624.90 2.854 389.97 4914.4 0.8000 1.40134 +FS_2 Inlet.Fl_O 522.31 4.329 440.05 105.12 0.0000 1633.08 3.514 414.53 5943.4 0.5539 1.40134 +FS_21 Fan.Fl_O 522.31 6.959 511.79 122.30 0.0000 1095.73 6.002 490.58 4515.2 0.4645 1.40063 +FS_13 Splitter.Fl_O2 439.43 6.959 511.79 122.30 0.0000 921.87 6.000 490.53 3795.6 0.4650 1.40063 +FS_22 Splitter.Fl_O1 82.87 6.959 511.79 122.30 0.0000 173.86 6.012 490.81 719.5 0.4618 1.40063 +FS_23 Duct1.Fl_O 82.87 6.941 511.79 122.30 0.0000 174.29 5.997 490.81 721.3 0.4618 1.40063 +FS_24 LPC.Fl_O 82.87 16.168 673.03 161.05 0.0000 85.81 14.120 647.59 366.0 0.4445 1.39696 +FS_25 Duct2.Fl_O 82.87 16.128 673.03 161.05 0.0000 86.02 14.085 647.59 366.9 0.4445 1.39696 +FS_3 HPC.Fl_O 82.87 90.642 1154.51 279.76 0.0000 20.05 85.245 1135.47 119.9 0.3003 1.37101 +FS_36 Bld3.Fl_O 75.41 90.642 1154.51 279.76 0.0000 18.24 85.245 1135.47 109.1 0.3003 1.37101 +FS_4 Burner.Fl_O 76.72 85.657 2249.10 586.59 0.0173 27.41 85.104 2245.67 483.4 0.0995 1.30824 +FS_45 HPT.Fl_O 84.18 31.753 1746.58 442.54 0.0158 71.49 29.964 1721.75 439.1 0.2966 1.32720 +FS_48 Duct3.Fl_O 84.18 31.594 1746.58 442.54 0.0158 71.85 29.814 1721.75 441.4 0.2966 1.32720 +FS_5 LPT.Fl_O 84.18 6.504 1209.85 297.80 0.0158 290.51 5.951 1181.88 1477.4 0.3636 1.35668 +FS_7 Duct4.Fl_O 84.18 6.439 1209.85 297.80 0.0158 293.45 6.154 1195.53 2018.9 0.2589 1.35668 +FS_9 Core_Nozz.Fl_O 84.18 6.439 1209.85 297.80 0.0158 293.45 3.435 1023.43 862.9 1.0000 1.35668 +FS_15 BypBld.Fl_O 439.43 6.959 511.79 122.30 0.0000 921.87 6.000 490.53 3795.6 0.4650 1.40063 +FS_17 Duct5.Fl_O 439.43 6.906 511.79 122.30 0.0000 928.84 5.955 490.53 3824.3 0.4650 1.40063 +FS_19 Byp_Nozz.Fl_O 439.43 6.906 511.79 122.30 0.0000 928.84 3.647 426.27 2706.4 1.0000 1.40063 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1633.08 1.607 0.8925 3742.526 1.1630 0.8995 -12695.3 28.21 17.74 +LPC 174.29 2.329 0.8661 3470.322 1.3150 0.8810 -4543.6 28.95 22.22 +HPC 86.02 5.620 0.8639 6337.461 1.7154 0.8916 -13918.4 20.47 20.49 +HPT 27.41 2.698 0.9138 152.224 1.2399 0.9037 13918.5 +LPT 71.85 4.858 0.9277 82.485 1.4436 0.9122 17238.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3130.99 1.423 0.9220 0.949 2.1753 0.5215 1.4369 0.9679 3943.9586 +LPC 186.95 1.407 0.9021 0.947 1.7535 0.9323 3.2631 0.9600 3662.6571 +HPC 204.50 22.358 0.8523 0.997 2.0718 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.995 0.9321 99.420 4.9955 1.4085 0.4249 0.9803 1.5311 +LPT 149.30 6.382 0.9265 101.694 6.3817 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4914.43 12577.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 844.21 202.60 27.044 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 844.21 202.60 27.044 +Duct1 0.0025 0.4618 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 844.21 202.60 27.044 +Duct2 0.0025 0.4445 365.99 +Duct3 0.0050 0.2966 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.9005 1154.51 279.76 90.642 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.5580 1154.51 279.76 90.642 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 511.79 122.30 6.959 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3025 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7219.1 10126.0 13918.5 +LP_Shaft 3447.2 26264.4 17238.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2249.10 0.9940 0.0550 1.30668 0.01733 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.420 0.9965 1.0000 0.9975 2706.36 1.000 1010.1 15940.9 +Core_Nozz 2.256 0.9992 1.0000 0.9999 862.88 1.000 1550.4 4557.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 374 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 39000.0 0.00 507.11 7041.0 0.5895 4150.91 5.5080 774.79 19.193 2162.4 2108.2 1675.1 + core size:20.20 Q: 184.27 Maximum Thrust: 8801.2 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 507.11 4.351 440.05 105.12 0.0000 1577.61 2.854 389.97 4771.4 0.8000 1.40134 +FS_2 Inlet.Fl_O 507.11 4.329 440.05 105.12 0.0000 1585.56 3.575 416.58 5943.4 0.5299 1.40134 +FS_21 Fan.Fl_O 507.11 6.761 506.42 121.02 0.0000 1089.22 5.844 485.74 4515.2 0.4608 1.40072 +FS_13 Splitter.Fl_O2 429.19 6.761 506.42 121.02 0.0000 921.86 5.829 485.38 3795.6 0.4649 1.40072 +FS_22 Splitter.Fl_O1 77.92 6.761 506.42 121.02 0.0000 167.37 5.920 487.55 719.5 0.4394 1.40072 +FS_23 Duct1.Fl_O 77.92 6.744 506.42 121.02 0.0000 167.79 5.906 487.55 721.3 0.4394 1.40072 +FS_24 LPC.Fl_O 77.92 15.213 659.77 157.86 0.0000 84.90 13.334 635.47 366.0 0.4383 1.39746 +FS_25 Duct2.Fl_O 77.92 15.175 659.77 157.86 0.0000 85.11 13.301 635.47 366.9 0.4383 1.39746 +FS_3 HPC.Fl_O 77.92 83.513 1125.27 272.36 0.0000 20.20 78.460 1106.34 119.9 0.3027 1.37285 +FS_36 Bld3.Fl_O 70.91 83.513 1125.27 272.36 0.0000 18.38 78.460 1106.34 109.1 0.3027 1.37285 +FS_4 Burner.Fl_O 72.06 78.920 2162.37 560.74 0.0163 27.40 78.411 2159.05 483.4 0.0993 1.31135 +FS_45 HPT.Fl_O 79.07 29.113 1675.12 422.33 0.0148 71.73 27.461 1650.92 439.1 0.2972 1.33116 +FS_48 Duct3.Fl_O 79.07 28.968 1675.12 422.33 0.0148 72.09 27.324 1650.92 441.4 0.2972 1.33116 +FS_5 LPT.Fl_O 79.07 5.969 1158.01 284.11 0.0148 290.90 5.461 1130.96 1477.4 0.3636 1.36063 +FS_7 Duct4.Fl_O 79.07 5.909 1158.01 284.11 0.0148 293.83 5.647 1144.16 2018.9 0.2589 1.36063 +FS_9 Core_Nozz.Fl_O 79.07 5.909 1158.01 284.11 0.0148 293.83 3.150 978.04 862.9 1.0000 1.36063 +FS_15 BypBld.Fl_O 429.19 6.761 506.42 121.02 0.0000 921.86 5.829 485.38 3795.6 0.4649 1.40072 +FS_17 Duct5.Fl_O 429.19 6.710 506.42 121.02 0.0000 928.82 5.785 485.38 3824.3 0.4649 1.40072 +FS_19 Byp_Nozz.Fl_O 429.19 6.710 506.42 121.02 0.0000 928.82 3.543 421.79 2706.4 1.0000 1.40072 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1585.56 1.562 0.9023 3613.838 1.1508 0.9083 -11401.9 31.67 18.33 +LPC 167.79 2.256 0.8632 3368.727 1.3028 0.8778 -4061.8 28.08 20.51 +HPC 85.11 5.503 0.8648 6313.705 1.7055 0.8922 -12623.9 22.09 22.16 +HPT 27.40 2.711 0.9145 153.134 1.2436 0.9042 12623.8 +LPT 72.09 4.853 0.9256 81.330 1.4466 0.9098 15463.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3040.11 1.391 0.9322 0.916 2.0967 0.5215 1.4369 0.9679 3943.9586 +LPC 179.97 1.385 0.8991 0.920 1.7168 0.9323 3.2631 0.9600 3662.6571 +HPC 202.34 21.818 0.8531 0.993 2.0967 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 5.026 0.9328 100.014 5.0265 1.4085 0.4249 0.9803 1.5311 +LPT 149.80 6.375 0.9244 100.270 6.3748 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4771.43 12211.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 825.11 197.94 25.186 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 825.11 197.94 25.186 +Duct1 0.0025 0.4394 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 825.11 197.94 25.186 +Duct2 0.0025 0.4383 365.99 +Duct3 0.0050 0.2972 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.7272 1125.27 272.36 83.513 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.2856 1125.27 272.36 83.513 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 506.42 121.02 6.761 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5080 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7120.9 9310.8 12623.8 +LP_Shaft 3328.7 24399.4 15463.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2162.37 0.9940 0.0550 1.15303 0.01626 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.351 0.9968 1.0000 0.9975 2706.36 1.000 1004.7 15267.4 +Core_Nozz 2.071 0.9998 1.0000 0.9999 862.88 1.000 1517.6 3985.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 375 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 39000.0 0.00 474.09 5280.7 0.5946 3139.81 5.9821 774.79 15.997 1984.4 1936.0 1530.8 + core size:20.55 Q: 184.27 Maximum Thrust: 8801.2 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 474.09 4.351 440.05 105.12 0.0000 1474.89 2.854 389.97 4460.7 0.8000 1.40134 +FS_2 Inlet.Fl_O 474.09 4.329 440.05 105.12 0.0000 1482.31 3.693 420.46 5943.4 0.4818 1.40134 +FS_21 Fan.Fl_O 474.09 6.329 495.56 118.41 0.0000 1076.01 5.496 475.94 4515.2 0.4534 1.40089 +FS_13 Splitter.Fl_O2 406.19 6.329 495.56 118.41 0.0000 921.90 5.457 474.97 3795.6 0.4649 1.40089 +FS_22 Splitter.Fl_O1 67.90 6.329 495.56 118.41 0.0000 154.11 5.680 480.44 719.5 0.3962 1.40089 +FS_23 Duct1.Fl_O 67.90 6.313 495.56 118.41 0.0000 154.50 5.665 480.44 721.3 0.3962 1.40089 +FS_24 LPC.Fl_O 67.90 13.472 635.77 152.08 0.0000 82.00 11.938 614.24 366.0 0.4194 1.39826 +FS_25 Duct2.Fl_O 67.90 13.438 635.77 152.08 0.0000 82.21 11.908 614.24 366.9 0.4194 1.39826 +FS_3 HPC.Fl_O 67.90 69.606 1065.93 257.44 0.0000 20.55 65.234 1047.16 119.9 0.3082 1.37659 +FS_36 Bld3.Fl_O 61.79 69.606 1065.93 257.44 0.0000 18.70 65.234 1047.16 109.1 0.3082 1.37659 +FS_4 Burner.Fl_O 62.66 65.777 1984.39 508.50 0.0141 27.38 65.354 1981.29 483.4 0.0990 1.31865 +FS_45 HPT.Fl_O 68.77 24.121 1530.81 382.16 0.0128 71.98 22.743 1508.12 439.1 0.2974 1.33965 +FS_48 Duct3.Fl_O 68.77 24.001 1530.81 382.16 0.0128 72.34 22.629 1508.12 441.4 0.2974 1.33965 +FS_5 LPT.Fl_O 68.77 4.973 1055.18 257.31 0.0128 289.87 4.553 1030.36 1477.4 0.3610 1.36854 +FS_7 Duct4.Fl_O 68.77 4.923 1055.18 257.31 0.0128 292.80 4.707 1042.46 2018.9 0.2571 1.36854 +FS_9 Core_Nozz.Fl_O 68.77 4.923 1055.18 257.31 0.0128 292.80 2.854 909.74 862.9 0.9240 1.36854 +FS_15 BypBld.Fl_O 406.19 6.329 495.56 118.41 0.0000 921.90 5.457 474.97 3795.6 0.4649 1.40089 +FS_17 Duct5.Fl_O 406.19 6.282 495.56 118.41 0.0000 928.86 5.416 474.97 3824.3 0.4649 1.40089 +FS_19 Byp_Nozz.Fl_O 406.19 6.282 495.56 118.41 0.0000 928.86 3.317 412.75 2706.4 1.0000 1.40089 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1482.31 1.462 0.9104 3371.101 1.1261 0.9151 -8914.7 39.34 19.69 +LPC 154.50 2.134 0.8543 3176.691 1.2829 0.8689 -3234.0 25.15 16.59 +HPC 82.21 5.180 0.8658 6252.250 1.6766 0.8923 -10122.2 26.38 26.54 +HPT 27.38 2.727 0.9148 155.392 1.2506 0.9046 10122.3 +LPT 72.34 4.826 0.9207 79.363 1.4508 0.9037 12148.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2842.06 1.321 0.9406 0.855 2.0402 0.5215 1.4369 0.9679 3943.9586 +LPC 165.72 1.348 0.8899 0.867 1.6215 0.9323 3.2631 0.9600 3662.6571 +HPC 195.44 20.321 0.8542 0.983 2.1343 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.065 0.9332 101.489 5.0645 1.4085 0.4249 0.9803 1.5311 +LPT 150.32 6.337 0.9195 97.844 6.3373 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4460.74 11416.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 788.24 188.95 21.667 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 788.24 188.95 21.667 +Duct1 0.0025 0.3962 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 788.24 188.95 21.667 +Duct2 0.0025 0.4194 365.99 +Duct3 0.0050 0.2974 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3610 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.3765 1065.93 257.44 69.606 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.7345 1065.93 257.44 69.606 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 495.56 118.41 6.329 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9821 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6922.1 7680.2 10122.3 +LP_Shaft 3105.1 20548.5 12148.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1984.39 0.9940 0.0550 0.87217 0.01412 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.201 0.9973 1.0000 0.9975 2706.36 1.000 993.9 13800.7 +Core_Nozz 1.725 0.9999 1.0000 0.9999 862.88 0.924 1355.1 2896.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 376 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 39000.0 0.00 435.63 3520.5 0.6273 2208.59 6.6891 774.79 12.651 1787.7 1745.6 1371.7 + core size:20.95 Q: 184.27 Maximum Thrust: 8801.2 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 435.63 4.351 440.05 105.12 0.0000 1355.26 2.854 389.97 4098.9 0.8000 1.40134 +FS_2 Inlet.Fl_O 435.63 4.329 440.05 105.12 0.0000 1362.08 3.810 424.23 5943.4 0.4311 1.40134 +FS_21 Fan.Fl_O 435.63 5.830 483.05 115.42 0.0000 1059.79 5.090 464.63 4515.2 0.4445 1.40105 +FS_13 Splitter.Fl_O2 378.98 5.830 483.05 115.42 0.0000 921.96 5.026 462.97 3795.6 0.4650 1.40105 +FS_22 Splitter.Fl_O1 56.66 5.830 483.05 115.42 0.0000 137.83 5.364 471.67 719.5 0.3468 1.40105 +FS_23 Duct1.Fl_O 56.66 5.815 483.05 115.42 0.0000 138.18 5.351 471.67 721.3 0.3468 1.40105 +FS_24 LPC.Fl_O 56.66 11.380 604.16 144.48 0.0000 78.97 10.192 585.46 366.0 0.4001 1.39898 +FS_25 Duct2.Fl_O 56.66 11.351 604.16 144.48 0.0000 79.16 10.166 585.46 366.9 0.4001 1.39898 +FS_3 HPC.Fl_O 56.66 55.046 995.29 239.81 0.0000 20.95 51.442 976.85 119.9 0.3145 1.38101 +FS_36 Bld3.Fl_O 51.56 55.046 995.29 239.81 0.0000 19.07 51.442 976.85 109.1 0.3145 1.38101 +FS_4 Burner.Fl_O 52.17 52.018 1787.65 452.13 0.0119 27.36 51.684 1784.81 483.4 0.0986 1.32803 +FS_45 HPT.Fl_O 57.27 18.910 1371.65 338.91 0.0108 72.38 17.817 1350.62 439.1 0.2980 1.34993 +FS_48 Duct3.Fl_O 57.27 18.815 1371.65 338.91 0.0108 72.74 17.728 1350.62 441.4 0.2980 1.34993 +FS_5 LPT.Fl_O 57.27 4.167 955.87 231.86 0.0108 274.20 3.856 935.78 1477.4 0.3374 1.37621 +FS_7 Duct4.Fl_O 57.27 4.125 955.87 231.86 0.0108 276.97 3.964 945.48 2018.9 0.2415 1.37621 +FS_9 Core_Nozz.Fl_O 57.27 4.125 955.87 231.86 0.0108 276.97 2.854 863.88 862.9 0.7487 1.37621 +FS_15 BypBld.Fl_O 378.98 5.830 483.05 115.42 0.0000 921.96 5.026 462.97 3795.6 0.4650 1.40105 +FS_17 Duct5.Fl_O 378.98 5.786 483.05 115.42 0.0000 928.93 4.989 462.97 3824.3 0.4650 1.40105 +FS_19 Byp_Nozz.Fl_O 378.98 5.786 483.05 115.42 0.0000 928.93 3.055 402.32 2706.3 1.0000 1.40105 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1362.08 1.347 0.9101 3052.582 1.0977 0.9138 -6345.1 47.03 21.42 +LPC 138.18 1.957 0.8437 2913.545 1.2507 0.8577 -2329.2 22.77 13.08 +HPC 79.16 4.849 0.8647 6200.454 1.6474 0.8905 -7642.3 31.27 31.51 +HPT 27.36 2.751 0.9154 158.276 1.2596 0.9046 7642.3 +LPT 72.74 4.515 0.9158 75.919 1.4350 0.8982 8674.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2611.61 1.241 0.9402 0.774 2.0759 0.5215 1.4369 0.9679 3943.9586 +LPC 148.21 1.293 0.8789 0.795 1.5425 0.9323 3.2631 0.9600 3662.6571 +HPC 188.20 18.794 0.8531 0.975 2.1667 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.121 0.9338 103.373 5.1209 1.4085 0.4249 0.9803 1.5311 +LPT 151.15 5.904 0.9146 93.599 5.9039 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4098.92 10490.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 742.47 177.84 17.753 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 742.47 177.84 17.753 +Duct1 0.0025 0.3468 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 742.47 177.84 17.753 +Duct2 0.0025 0.4001 365.99 +Duct3 0.0050 0.2980 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3374 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.9830 995.29 239.81 55.046 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.1161 995.29 239.81 55.046 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 483.05 115.42 5.830 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6891 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6692.0 5997.9 7642.3 +LP_Shaft 2811.7 16203.4 8674.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1787.65 0.9940 0.0550 0.61350 0.01190 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.027 0.9976 1.0000 0.9975 2706.36 1.000 981.2 12103.6 +Core_Nozz 1.445 0.9999 1.0000 0.9999 862.88 0.749 1071.6 1907.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 377 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 39000.0 0.00 389.72 1760.3 0.7522 1324.04 7.8875 774.79 9.058 1534.6 1500.5 1168.9 + core size:21.56 Q: 184.27 Maximum Thrust: 8801.2 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 389.72 4.351 440.05 105.12 0.0000 1212.43 2.854 389.97 3666.9 0.8000 1.40134 +FS_2 Inlet.Fl_O 389.72 4.329 440.05 105.12 0.0000 1218.53 3.927 427.92 5943.4 0.3758 1.40134 +FS_21 Fan.Fl_O 389.72 5.241 467.92 111.80 0.0000 1037.93 4.608 450.98 4515.2 0.4327 1.40122 +FS_13 Splitter.Fl_O2 345.87 5.241 467.92 111.80 0.0000 921.15 4.520 448.51 3795.6 0.4644 1.40122 +FS_22 Splitter.Fl_O1 43.85 5.241 467.92 111.80 0.0000 116.78 4.949 460.29 719.5 0.2874 1.40122 +FS_23 Duct1.Fl_O 43.85 5.228 467.92 111.80 0.0000 117.08 4.936 460.29 721.3 0.2874 1.40122 +FS_24 LPC.Fl_O 43.85 8.975 562.10 134.37 0.0000 74.75 8.148 546.79 366.0 0.3742 1.39967 +FS_25 Duct2.Fl_O 43.85 8.953 562.10 134.37 0.0000 74.93 8.128 546.79 366.9 0.3742 1.39967 +FS_3 HPC.Fl_O 43.85 39.413 901.80 216.71 0.0000 21.56 36.668 883.81 119.9 0.3241 1.38674 +FS_36 Bld3.Fl_O 39.90 39.413 901.80 216.71 0.0000 19.62 36.668 883.81 109.1 0.3241 1.38674 +FS_4 Burner.Fl_O 40.27 37.245 1534.56 381.82 0.0092 27.33 37.006 1532.04 483.4 0.0979 1.34195 +FS_45 HPT.Fl_O 44.22 13.384 1168.93 285.42 0.0084 72.89 12.599 1150.20 439.1 0.2987 1.36423 +FS_48 Duct3.Fl_O 44.22 13.317 1168.93 285.42 0.0084 73.26 12.536 1150.20 441.4 0.2987 1.36423 +FS_5 LPT.Fl_O 44.22 3.547 846.25 204.23 0.0084 234.02 3.359 833.54 1477.4 0.2815 1.38435 +FS_7 Duct4.Fl_O 44.22 3.511 846.25 204.23 0.0084 236.39 3.413 839.56 2018.9 0.2035 1.38435 +FS_9 Core_Nozz.Fl_O 44.22 3.511 846.25 204.23 0.0084 236.39 2.854 798.80 862.9 0.5549 1.38435 +FS_15 BypBld.Fl_O 345.87 5.241 467.92 111.80 0.0000 921.15 4.520 448.51 3795.6 0.4644 1.40122 +FS_17 Duct5.Fl_O 345.87 5.202 467.92 111.80 0.0000 928.11 4.486 448.51 3824.3 0.4644 1.40122 +FS_19 Byp_Nozz.Fl_O 345.87 5.202 467.92 111.80 0.0000 928.11 2.854 394.00 2706.3 0.9670 1.40122 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1218.53 1.211 0.8881 2616.190 1.0633 0.8911 -3679.0 57.40 24.02 +LPC 117.08 1.717 0.8306 2537.074 1.2013 0.8430 -1400.6 22.56 9.67 +HPC 74.93 4.402 0.8627 6119.812 1.6043 0.8875 -5108.7 38.76 39.34 +HPT 27.33 2.783 0.9164 162.633 1.2724 0.9052 5108.8 +LPT 73.26 3.755 0.9114 70.482 1.3813 0.8953 5079.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2336.36 1.147 0.9175 0.663 2.2560 0.5215 1.4369 0.9679 3943.9586 +LPC 125.58 1.220 0.8651 0.693 1.4952 0.9323 3.2631 0.9600 3662.6571 +HPC 178.14 16.728 0.8511 0.963 2.2500 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.196 0.9347 106.219 5.1961 1.4085 0.4249 0.9803 1.5311 +LPT 152.22 4.843 0.9103 86.896 4.8426 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3666.94 9385.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 681.88 163.19 13.415 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 681.88 163.19 13.415 +Duct1 0.0025 0.2874 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 681.88 163.19 13.415 +Duct2 0.0025 0.3742 365.99 +Duct3 0.0050 0.2987 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2815 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.5348 901.80 216.71 39.413 +Duct5 0.0075 0.4644 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.4118 901.80 216.71 39.413 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 467.92 111.80 5.241 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8875 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6370.9 4211.7 5108.8 +LP_Shaft 2409.8 11071.2 5079.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1534.56 0.9940 0.0550 0.36779 0.00922 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.823 0.9975 1.0000 0.9975 2706.36 0.967 939.0 10093.8 +Core_Nozz 1.230 0.9999 1.0000 0.9999 862.88 0.555 765.1 1051.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 378 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 12/ 32/ 2/ 9 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 39000.0 0.00 344.32 440.1 1.5324 674.38 9.7435 774.79 5.978 1253.5 1228.5 947.8 + core size:22.45 Q: 184.27 Maximum Thrust: 8801.2 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 344.32 4.351 440.05 105.12 0.0000 1071.19 2.854 389.97 3239.8 0.8000 1.40134 +FS_2 Inlet.Fl_O 344.32 4.329 440.05 105.12 0.0000 1076.59 4.023 430.91 5943.4 0.3252 1.40134 +FS_21 Fan.Fl_O 344.32 4.726 454.31 108.54 0.0000 1002.08 4.200 439.21 4515.2 0.4140 1.40131 +FS_13 Splitter.Fl_O2 312.28 4.726 454.31 108.54 0.0000 908.80 4.097 436.10 3795.6 0.4562 1.40131 +FS_22 Splitter.Fl_O1 32.05 4.726 454.31 108.54 0.0000 93.27 4.562 449.73 719.5 0.2252 1.40131 +FS_23 Duct1.Fl_O 32.05 4.714 454.31 108.54 0.0000 93.51 4.550 449.73 721.3 0.2252 1.40131 +FS_24 LPC.Fl_O 32.05 6.827 516.43 123.42 0.0000 68.84 6.303 504.76 366.0 0.3396 1.40056 +FS_25 Duct2.Fl_O 32.05 6.810 516.43 123.42 0.0000 69.01 6.287 504.76 366.9 0.3396 1.40056 +FS_3 HPC.Fl_O 32.05 26.009 797.41 191.18 0.0000 22.45 24.031 779.82 119.9 0.3389 1.39207 +FS_36 Bld3.Fl_O 29.17 26.009 797.41 191.18 0.0000 20.43 24.031 779.82 109.1 0.3389 1.39207 +FS_4 Burner.Fl_O 29.35 24.579 1253.49 306.72 0.0064 27.28 24.422 1251.36 483.4 0.0971 1.36023 +FS_45 HPT.Fl_O 32.24 8.731 947.77 229.01 0.0058 73.35 8.212 931.91 439.1 0.2990 1.37999 +FS_48 Duct3.Fl_O 32.24 8.687 947.77 229.01 0.0058 73.72 8.171 931.91 441.4 0.2990 1.37999 +FS_5 LPT.Fl_O 32.24 3.188 739.58 177.76 0.0058 177.44 3.094 733.34 1477.4 0.2085 1.39111 +FS_7 Duct4.Fl_O 32.24 3.156 739.58 177.76 0.0058 179.23 3.106 736.24 2018.9 0.1523 1.39111 +FS_9 Core_Nozz.Fl_O 32.24 3.156 739.58 177.76 0.0058 179.23 2.854 718.92 862.9 0.3831 1.39111 +FS_15 BypBld.Fl_O 312.28 4.726 454.31 108.54 0.0000 908.80 4.097 436.10 3795.6 0.4562 1.40131 +FS_17 Duct5.Fl_O 312.28 4.691 454.31 108.54 0.0000 915.67 4.066 436.10 3824.3 0.4562 1.40131 +FS_19 Byp_Nozz.Fl_O 312.28 4.691 454.31 108.54 0.0000 915.67 2.854 394.04 2706.4 0.8731 1.40131 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1076.59 1.092 0.7844 2081.051 1.0324 0.7872 -1662.9 81.07 25.92 +LPC 93.51 1.448 0.8176 2048.130 1.1367 0.8270 -674.7 26.66 7.87 +HPC 69.01 3.819 0.8528 6011.676 1.5441 0.8774 -3073.0 50.44 51.46 +HPT 27.28 2.815 0.9180 169.432 1.2881 0.9065 3073.0 +LPT 73.72 2.725 0.9020 62.264 1.2815 0.8887 2337.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2064.21 1.064 0.8104 0.528 2.6336 0.5215 1.4369 0.9679 3943.9586 +LPC 100.30 1.137 0.8517 0.559 1.5266 0.9323 3.2631 0.9600 3662.6571 +HPC 164.07 14.033 0.8413 0.946 2.3845 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.272 0.9364 110.659 5.2723 1.4085 0.4249 0.9803 1.5311 +LPT 153.18 3.406 0.9009 76.764 3.4060 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3239.78 8291.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 615.22 147.13 9.623 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 615.22 147.13 9.623 +Duct1 0.0025 0.2252 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 615.22 147.13 9.623 +Duct2 0.0025 0.3396 365.99 +Duct3 0.0050 0.2990 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2085 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.1217 797.41 191.18 26.009 +Duct5 0.0075 0.4562 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 1.7627 797.41 191.18 26.009 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 454.31 108.54 4.726 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.7435 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 5998.7 2690.6 3073.0 +LP_Shaft 1916.8 6405.2 2337.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1253.49 0.9940 0.0550 0.18733 0.00642 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.644 0.9975 1.0000 0.9975 2706.36 0.873 847.8 8228.8 +Core_Nozz 1.106 0.9999 1.0000 0.9999 862.88 0.383 502.0 503.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 379 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 39000.0 0.00 559.61 9056.2 0.6239 5650.30 5.0403 823.21 22.724 2365.6 2305.4 1845.2 + core size:19.95 Q: 208.03 Maximum Thrust: 9056.2 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 559.61 4.578 446.51 106.67 0.0000 1666.72 2.854 389.97 4955.7 0.8500 1.40133 +FS_2 Inlet.Fl_O 559.61 4.555 446.51 106.67 0.0000 1675.11 3.636 418.61 5943.4 0.5763 1.40133 +FS_21 Fan.Fl_O 559.61 7.491 525.26 125.53 0.0000 1104.75 6.440 503.03 4515.2 0.4696 1.40040 +FS_13 Splitter.Fl_O2 466.97 7.491 525.26 125.53 0.0000 921.85 6.459 503.45 3795.6 0.4650 1.40040 +FS_22 Splitter.Fl_O1 92.65 7.491 525.26 125.53 0.0000 182.90 6.337 500.71 719.5 0.4947 1.40040 +FS_23 Duct1.Fl_O 92.65 7.473 525.26 125.53 0.0000 183.36 6.321 500.71 721.3 0.4947 1.40040 +FS_24 LPC.Fl_O 92.65 18.593 704.73 168.71 0.0000 85.36 16.266 678.49 366.0 0.4417 1.39585 +FS_25 Duct2.Fl_O 92.65 18.546 704.73 168.71 0.0000 85.57 16.225 678.49 366.9 0.4417 1.39585 +FS_3 HPC.Fl_O 92.65 104.036 1204.89 292.56 0.0000 19.95 97.907 1185.35 119.9 0.2990 1.36784 +FS_36 Bld3.Fl_O 84.31 104.036 1204.89 292.56 0.0000 18.15 97.907 1185.35 109.1 0.2990 1.36784 +FS_4 Burner.Fl_O 85.88 98.314 2365.61 621.58 0.0186 27.42 97.680 2362.04 483.4 0.0997 1.30423 +FS_45 HPT.Fl_O 94.22 36.822 1845.16 470.67 0.0169 70.92 34.781 1819.67 439.1 0.2945 1.32214 +FS_48 Duct3.Fl_O 94.22 36.638 1845.16 470.67 0.0169 71.28 34.608 1819.67 441.4 0.2945 1.32214 +FS_5 LPT.Fl_O 94.22 7.497 1278.77 316.17 0.0169 290.00 6.862 1249.63 1477.4 0.3636 1.35154 +FS_7 Duct4.Fl_O 94.22 7.422 1278.77 316.17 0.0169 292.93 7.095 1263.85 2018.9 0.2589 1.35154 +FS_9 Core_Nozz.Fl_O 94.22 7.422 1278.77 316.17 0.0169 292.93 3.963 1083.97 862.9 1.0000 1.35154 +FS_15 BypBld.Fl_O 466.97 7.491 525.26 125.53 0.0000 921.85 6.459 503.45 3795.6 0.4650 1.40040 +FS_17 Duct5.Fl_O 466.97 7.435 525.26 125.53 0.0000 928.82 6.411 503.45 3824.3 0.4650 1.40040 +FS_19 Byp_Nozz.Fl_O 466.97 7.435 525.26 125.53 0.0000 928.82 3.926 437.51 2706.3 1.0000 1.40040 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.645 0.8675 3944.235 1.1764 0.8766 -14935.0 24.71 17.45 +LPC 183.36 2.488 0.8683 3636.548 1.3417 0.8840 -5660.0 28.39 23.30 +HPC 85.57 5.610 0.8651 6326.125 1.7097 0.8923 -16234.6 20.08 20.14 +HPT 27.42 2.670 0.9133 151.612 1.2341 0.9035 16234.9 +LPT 71.28 4.887 0.9322 85.195 1.4429 0.9178 20595.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8963 1.000 2.3706 0.5215 1.4369 0.9679 3943.9586 +LPC 196.67 1.456 0.9045 0.993 1.7667 0.9323 3.2631 0.9600 3662.6571 +HPC 203.43 22.309 0.8535 0.995 2.0421 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.931 0.9316 99.020 4.9305 1.4085 0.4249 0.9803 1.5311 +LPT 148.11 6.422 0.9310 105.035 6.4224 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4955.73 14318.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 882.84 212.06 31.070 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 882.84 212.06 31.070 +Duct1 0.0025 0.4947 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 882.84 212.06 31.070 +Duct2 0.0025 0.4417 365.99 +Duct3 0.0050 0.2945 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.2427 1204.89 292.56 104.036 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.0956 1204.89 292.56 104.036 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 525.26 125.53 7.491 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0403 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7374.0 11563.2 16234.9 +LP_Shaft 3659.6 29557.4 20595.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2365.61 0.9940 0.0550 1.56953 0.01862 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.605 0.9953 1.0000 0.9975 2706.36 1.000 1023.3 17753.0 +Core_Nozz 2.601 0.9969 1.0000 0.9999 862.88 1.000 1592.8 5621.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 380 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 39000.0 0.00 545.61 8150.1 0.6135 5000.29 5.3025 823.21 20.832 2280.2 2222.5 1772.0 + core size:20.04 Q: 208.03 Maximum Thrust: 9056.2 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 545.61 4.578 446.51 106.67 0.0000 1625.01 2.854 389.97 4831.7 0.8500 1.40133 +FS_2 Inlet.Fl_O 545.61 4.555 446.51 106.67 0.0000 1633.19 3.697 420.61 5943.4 0.5539 1.40133 +FS_21 Fan.Fl_O 545.61 7.322 519.31 124.10 0.0000 1095.73 6.315 497.79 4515.2 0.4645 1.40051 +FS_13 Splitter.Fl_O2 459.04 7.322 519.31 124.10 0.0000 921.87 6.313 497.74 3795.6 0.4650 1.40051 +FS_22 Splitter.Fl_O1 86.57 7.322 519.31 124.10 0.0000 173.86 6.326 498.02 719.5 0.4618 1.40051 +FS_23 Duct1.Fl_O 86.57 7.304 519.31 124.10 0.0000 174.29 6.310 498.02 721.3 0.4618 1.40051 +FS_24 LPC.Fl_O 86.57 17.018 682.91 163.44 0.0000 85.78 14.864 657.14 366.0 0.4444 1.39661 +FS_25 Duct2.Fl_O 86.57 16.976 682.91 163.44 0.0000 86.00 14.827 657.14 366.9 0.4444 1.39661 +FS_3 HPC.Fl_O 86.57 95.371 1170.52 283.82 0.0000 20.04 89.697 1151.27 119.9 0.3004 1.37000 +FS_36 Bld3.Fl_O 78.78 95.371 1170.52 283.82 0.0000 18.24 89.697 1151.27 109.1 0.3004 1.37000 +FS_4 Burner.Fl_O 80.17 90.126 2280.24 595.87 0.0176 27.41 89.545 2276.78 483.4 0.0995 1.30719 +FS_45 HPT.Fl_O 87.96 33.421 1772.03 449.75 0.0160 71.49 31.538 1746.91 439.1 0.2967 1.32588 +FS_48 Duct3.Fl_O 87.96 33.254 1772.03 449.75 0.0160 71.85 31.380 1746.91 441.4 0.2967 1.32588 +FS_5 LPT.Fl_O 87.96 6.853 1229.06 302.89 0.0160 290.36 6.271 1200.77 1477.4 0.3636 1.35527 +FS_7 Duct4.Fl_O 87.96 6.785 1229.06 302.89 0.0160 293.30 6.485 1214.58 2018.9 0.2589 1.35527 +FS_9 Core_Nozz.Fl_O 87.96 6.785 1229.06 302.89 0.0160 293.30 3.620 1040.27 862.9 1.0000 1.35527 +FS_15 BypBld.Fl_O 459.04 7.322 519.31 124.10 0.0000 921.87 6.313 497.74 3795.6 0.4650 1.40051 +FS_17 Duct5.Fl_O 459.04 7.267 519.31 124.10 0.0000 928.84 6.266 497.74 3824.3 0.4650 1.40051 +FS_19 Byp_Nozz.Fl_O 459.04 7.267 519.31 124.10 0.0000 928.84 3.837 432.54 2706.4 1.0000 1.40051 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1633.19 1.607 0.8925 3742.937 1.1630 0.8995 -13459.6 28.20 17.74 +LPC 174.29 2.330 0.8661 3470.677 1.3150 0.8810 -4818.0 28.92 22.20 +HPC 86.00 5.618 0.8640 6336.792 1.7140 0.8916 -14744.8 20.48 20.51 +HPT 27.41 2.697 0.9138 152.270 1.2390 0.9038 14744.7 +LPT 71.85 4.852 0.9278 82.498 1.4418 0.9124 18277.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3131.24 1.423 0.9220 0.949 2.1756 0.5215 1.4369 0.9679 3943.9586 +LPC 186.95 1.408 0.9021 0.948 1.7529 0.9323 3.2631 0.9600 3662.6571 +HPC 204.44 22.349 0.8523 0.997 2.0716 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.993 0.9321 99.451 4.9933 1.4085 0.4249 0.9803 1.5311 +LPT 149.29 6.374 0.9266 101.710 6.3741 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4831.73 13960.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 856.37 205.57 28.461 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 856.37 205.57 28.461 +Duct1 0.0025 0.4618 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 856.37 205.57 28.461 +Duct2 0.0025 0.4444 365.99 +Duct3 0.0050 0.2967 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.0300 1170.52 283.82 95.371 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.7614 1170.52 283.82 95.371 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 519.31 124.10 7.322 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3025 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7271.2 10650.4 14744.7 +LP_Shaft 3472.8 27642.1 18277.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2280.24 0.9940 0.0550 1.38897 0.01763 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.546 0.9957 1.0000 0.9975 2706.36 1.000 1017.5 17177.8 +Core_Nozz 2.377 0.9985 1.0000 0.9999 862.88 1.000 1562.3 4932.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 381 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 39000.0 0.00 529.74 7245.0 0.6090 4411.97 5.5076 823.21 19.194 2192.3 2137.4 1699.5 + core size:20.19 Q: 208.03 Maximum Thrust: 9056.2 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 529.74 4.578 446.51 106.67 0.0000 1577.75 2.854 389.97 4691.2 0.8500 1.40133 +FS_2 Inlet.Fl_O 529.74 4.555 446.51 106.67 0.0000 1585.69 3.762 422.68 5943.4 0.5299 1.40133 +FS_21 Fan.Fl_O 529.74 7.114 513.85 122.80 0.0000 1089.23 6.150 492.88 4515.2 0.4608 1.40060 +FS_13 Splitter.Fl_O2 448.34 7.114 513.85 122.80 0.0000 921.85 6.134 492.51 3795.6 0.4650 1.40060 +FS_22 Splitter.Fl_O1 81.40 7.114 513.85 122.80 0.0000 167.38 6.230 494.71 719.5 0.4394 1.40060 +FS_23 Duct1.Fl_O 81.40 7.096 513.85 122.80 0.0000 167.80 6.214 494.71 721.3 0.4394 1.40060 +FS_24 LPC.Fl_O 81.40 16.010 669.43 160.19 0.0000 84.89 14.033 644.80 366.0 0.4383 1.39710 +FS_25 Duct2.Fl_O 81.40 15.970 669.43 160.19 0.0000 85.10 13.998 644.80 366.9 0.4383 1.39710 +FS_3 HPC.Fl_O 81.40 87.874 1140.96 276.33 0.0000 20.19 82.560 1121.81 119.9 0.3027 1.37186 +FS_36 Bld3.Fl_O 74.08 87.874 1140.96 276.33 0.0000 18.37 82.560 1121.81 109.1 0.3027 1.37186 +FS_4 Burner.Fl_O 75.30 83.041 2192.31 569.58 0.0165 27.40 82.506 2188.95 483.4 0.0994 1.31031 +FS_45 HPT.Fl_O 82.63 30.644 1699.47 429.16 0.0151 71.73 28.905 1674.99 439.1 0.2973 1.32985 +FS_48 Duct3.Fl_O 82.63 30.491 1699.47 429.16 0.0151 72.09 28.761 1674.99 441.4 0.2973 1.32985 +FS_5 LPT.Fl_O 82.63 6.289 1176.36 288.92 0.0151 290.77 5.754 1148.98 1477.4 0.3636 1.35929 +FS_7 Duct4.Fl_O 82.63 6.227 1176.36 288.92 0.0151 293.71 5.951 1162.34 2018.9 0.2589 1.35929 +FS_9 Core_Nozz.Fl_O 82.63 6.227 1176.36 288.92 0.0151 293.71 3.320 994.07 862.9 1.0000 1.35929 +FS_15 BypBld.Fl_O 448.34 7.114 513.85 122.80 0.0000 921.85 6.134 492.51 3795.6 0.4650 1.40060 +FS_17 Duct5.Fl_O 448.34 7.061 513.85 122.80 0.0000 928.81 6.088 492.51 3824.3 0.4650 1.40060 +FS_19 Byp_Nozz.Fl_O 448.34 7.061 513.85 122.80 0.0000 928.81 3.728 428.00 2706.4 1.0000 1.40060 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1585.69 1.562 0.9023 3614.167 1.1508 0.9083 -12088.8 31.66 18.33 +LPC 167.80 2.256 0.8632 3369.003 1.3028 0.8778 -4306.3 28.07 20.51 +HPC 85.10 5.502 0.8648 6313.517 1.7044 0.8921 -13376.7 22.11 22.18 +HPT 27.40 2.710 0.9145 153.189 1.2428 0.9043 13376.6 +LPT 72.09 4.848 0.9257 81.343 1.4447 0.9099 16395.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3040.37 1.391 0.9322 0.916 2.0968 0.5215 1.4369 0.9679 3943.9586 +LPC 179.99 1.385 0.8991 0.920 1.7167 0.9323 3.2631 0.9600 3662.6571 +HPC 202.32 21.813 0.8531 0.993 2.0970 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.024 0.9328 100.051 5.0243 1.4085 0.4249 0.9803 1.5311 +LPT 149.80 6.368 0.9245 100.286 6.3678 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4691.19 13554.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 837.00 200.84 26.504 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 837.00 200.84 26.504 +Duct1 0.0025 0.4394 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 837.00 200.84 26.504 +Duct2 0.0025 0.4383 365.99 +Duct3 0.0050 0.2973 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.8491 1140.96 276.33 87.874 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.4772 1140.96 276.33 87.874 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 513.85 122.80 7.114 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5076 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7172.6 9794.9 13376.6 +LP_Shaft 3353.3 25678.9 16395.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2192.31 0.9940 0.0550 1.22555 0.01654 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.474 0.9962 1.0000 0.9975 2706.36 1.000 1012.1 16469.3 +Core_Nozz 2.182 0.9995 1.0000 0.9999 862.88 1.000 1529.3 4329.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 382 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 39000.0 0.00 495.53 5433.7 0.6138 3335.36 5.9826 823.21 16.002 2011.4 1962.4 1552.9 + core size:20.55 Q: 208.03 Maximum Thrust: 9056.2 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 495.53 4.578 446.51 106.67 0.0000 1475.87 2.854 389.97 4388.3 0.8500 1.40133 +FS_2 Inlet.Fl_O 495.53 4.555 446.51 106.67 0.0000 1483.30 3.885 426.60 5943.4 0.4822 1.40133 +FS_21 Fan.Fl_O 495.53 6.665 502.95 120.19 0.0000 1075.96 5.788 483.04 4515.2 0.4534 1.40078 +FS_13 Splitter.Fl_O2 424.57 6.665 502.95 120.19 0.0000 921.87 5.747 482.06 3795.6 0.4649 1.40078 +FS_22 Splitter.Fl_O1 70.97 6.665 502.95 120.19 0.0000 154.09 5.981 487.61 719.5 0.3962 1.40078 +FS_23 Duct1.Fl_O 70.97 6.648 502.95 120.19 0.0000 154.48 5.966 487.61 721.3 0.3962 1.40078 +FS_24 LPC.Fl_O 70.97 14.209 645.58 154.44 0.0000 81.89 12.597 623.80 366.0 0.4186 1.39796 +FS_25 Duct2.Fl_O 70.97 14.174 645.58 154.44 0.0000 82.09 12.565 623.80 366.9 0.4186 1.39796 +FS_3 HPC.Fl_O 70.97 73.261 1081.06 261.24 0.0000 20.55 68.660 1062.06 119.9 0.3083 1.37564 +FS_36 Bld3.Fl_O 64.58 73.261 1081.06 261.24 0.0000 18.70 68.660 1062.06 109.1 0.3083 1.37564 +FS_4 Burner.Fl_O 65.51 69.232 2011.37 516.30 0.0143 27.38 68.786 2008.24 483.4 0.0990 1.31754 +FS_45 HPT.Fl_O 71.89 25.400 1552.88 388.21 0.0131 71.97 23.949 1529.92 439.1 0.2975 1.33837 +FS_48 Duct3.Fl_O 71.89 25.273 1552.88 388.21 0.0131 72.34 23.829 1529.92 441.4 0.2975 1.33837 +FS_5 LPT.Fl_O 71.89 5.216 1070.43 261.24 0.0131 291.02 4.771 1045.07 1477.4 0.3629 1.36742 +FS_7 Duct4.Fl_O 71.89 5.163 1070.43 261.24 0.0131 293.96 4.934 1057.44 2018.9 0.2583 1.36742 +FS_9 Core_Nozz.Fl_O 71.89 5.163 1070.43 261.24 0.0131 293.96 2.854 911.20 862.9 0.9668 1.36742 +FS_15 BypBld.Fl_O 424.57 6.665 502.95 120.19 0.0000 921.87 5.747 482.06 3795.6 0.4649 1.40078 +FS_17 Duct5.Fl_O 424.57 6.615 502.95 120.19 0.0000 928.83 5.703 482.06 3824.3 0.4649 1.40078 +FS_19 Byp_Nozz.Fl_O 424.57 6.615 502.95 120.19 0.0000 928.83 3.493 418.91 2706.4 1.0000 1.40078 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1483.30 1.463 0.9104 3373.753 1.1264 0.9152 -9476.6 39.23 19.66 +LPC 154.48 2.137 0.8541 3178.797 1.2836 0.8687 -3439.4 25.00 16.49 +HPC 82.09 5.169 0.8659 6250.070 1.6745 0.8923 -10723.3 26.50 26.66 +HPT 27.38 2.726 0.9149 155.478 1.2497 0.9047 10723.4 +LPT 72.34 4.846 0.9206 79.435 1.4507 0.9037 12915.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2843.97 1.322 0.9406 0.855 2.0396 0.5215 1.4369 0.9679 3943.9586 +LPC 165.70 1.349 0.8896 0.868 1.6179 0.9323 3.2631 0.9600 3662.6571 +HPC 195.16 20.271 0.8542 0.983 2.1340 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.061 0.9332 101.546 5.0615 1.4085 0.4249 0.9803 1.5311 +LPT 150.30 6.365 0.9194 97.934 6.3647 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4388.26 12678.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 800.01 191.82 22.830 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 800.01 191.82 22.830 +Duct1 0.0025 0.3962 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 800.01 191.82 22.830 +Duct2 0.0025 0.4186 365.99 +Duct3 0.0050 0.2975 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3629 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.4839 1081.06 261.24 73.261 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.9032 1081.06 261.24 73.261 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 502.95 120.19 6.665 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9826 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6972.9 8077.0 10723.4 +LP_Shaft 3130.3 21670.9 12915.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2011.37 0.9940 0.0550 0.92649 0.01435 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.318 0.9969 1.0000 0.9975 2706.36 1.000 1001.3 14942.0 +Core_Nozz 1.809 0.9999 1.0000 0.9999 862.88 0.967 1418.9 3170.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 383 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 39000.0 0.00 456.19 3622.4 0.6473 2344.87 6.6848 823.21 12.681 1810.7 1768.2 1390.5 + core size:20.97 Q: 208.03 Maximum Thrust: 9056.2 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 456.19 4.578 446.51 106.67 0.0000 1358.68 2.854 389.97 4039.8 0.8500 1.40133 +FS_2 Inlet.Fl_O 456.19 4.555 446.51 106.67 0.0000 1365.52 4.005 430.35 5943.4 0.4324 1.40133 +FS_21 Fan.Fl_O 456.19 6.152 490.57 117.22 0.0000 1059.84 5.371 471.86 4515.2 0.4445 1.40096 +FS_13 Splitter.Fl_O2 396.83 6.152 490.57 117.22 0.0000 921.92 5.304 470.18 3795.6 0.4649 1.40096 +FS_22 Splitter.Fl_O1 59.36 6.152 490.57 117.22 0.0000 137.91 5.660 479.00 719.5 0.3471 1.40096 +FS_23 Duct1.Fl_O 59.36 6.136 490.57 117.22 0.0000 138.26 5.645 479.00 721.3 0.3471 1.40096 +FS_24 LPC.Fl_O 59.36 12.068 614.64 146.99 0.0000 78.69 10.819 595.78 366.0 0.3984 1.39878 +FS_25 Duct2.Fl_O 59.36 12.038 614.64 146.99 0.0000 78.89 10.791 595.78 366.9 0.3984 1.39878 +FS_3 HPC.Fl_O 59.36 58.055 1010.32 243.55 0.0000 20.97 54.247 991.59 119.9 0.3149 1.38007 +FS_36 Bld3.Fl_O 54.02 58.055 1010.32 243.55 0.0000 19.09 54.247 991.59 109.1 0.3149 1.38007 +FS_4 Burner.Fl_O 54.67 54.862 1810.71 458.62 0.0121 27.36 54.510 1807.83 483.4 0.0986 1.32692 +FS_45 HPT.Fl_O 60.01 19.960 1390.54 343.96 0.0110 72.35 18.807 1369.29 439.1 0.2980 1.34870 +FS_48 Duct3.Fl_O 60.01 19.860 1390.54 343.96 0.0110 72.71 18.713 1369.29 441.4 0.2980 1.34870 +FS_5 LPT.Fl_O 60.01 4.313 965.57 234.32 0.0110 279.01 3.978 944.50 1477.4 0.3444 1.37550 +FS_7 Duct4.Fl_O 60.01 4.270 965.57 234.32 0.0110 281.82 4.097 954.70 2018.9 0.2461 1.37550 +FS_9 Core_Nozz.Fl_O 60.01 4.270 965.57 234.32 0.0110 281.82 2.854 864.49 862.9 0.7849 1.37550 +FS_15 BypBld.Fl_O 396.83 6.152 490.57 117.22 0.0000 921.92 5.304 470.18 3795.6 0.4649 1.40096 +FS_17 Duct5.Fl_O 396.83 6.106 490.57 117.22 0.0000 928.89 5.264 470.18 3824.3 0.4649 1.40096 +FS_19 Byp_Nozz.Fl_O 396.83 6.106 490.57 117.22 0.0000 928.89 3.224 408.59 2706.4 1.0000 1.40096 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1365.52 1.351 0.9103 3062.987 1.0987 0.9141 -6808.9 46.73 21.33 +LPC 138.26 1.967 0.8430 2922.196 1.2529 0.8571 -2500.9 22.32 12.86 +HPC 78.89 4.823 0.8647 6195.688 1.6437 0.8905 -8109.7 31.65 31.89 +HPT 27.36 2.749 0.9154 158.501 1.2586 0.9047 8109.9 +LPT 72.71 4.605 0.9152 76.212 1.4401 0.8973 9309.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2618.19 1.244 0.9405 0.777 2.0719 0.5215 1.4369 0.9679 3943.9586 +LPC 148.30 1.296 0.8781 0.798 1.5327 0.9323 3.2631 0.9600 3662.6571 +HPC 187.55 18.671 0.8530 0.975 2.1685 0.4206 0.2163 1.0137 6357.1603 +HPT 30.10 5.116 0.9338 103.520 5.1156 1.4085 0.4249 0.9803 1.5311 +LPT 151.08 6.028 0.9140 93.959 6.0284 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4039.83 11672.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 754.62 180.79 18.780 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 754.62 180.79 18.780 +Duct1 0.0025 0.3471 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 754.62 180.79 18.780 +Duct2 0.0025 0.3984 365.99 +Duct3 0.0050 0.2980 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3444 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.0777 1010.32 243.55 58.055 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.2649 1010.32 243.55 58.055 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 490.57 117.22 6.152 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6848 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6744.6 6315.3 8109.9 +LP_Shaft 2841.9 17205.4 9309.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1810.71 0.9940 0.0550 0.65135 0.01206 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.139 0.9975 1.0000 0.9975 2706.36 1.000 988.9 13198.3 +Core_Nozz 1.496 0.9999 1.0000 0.9999 862.88 0.785 1123.8 2096.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 384 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 39000.0 0.00 409.11 1811.3 0.7753 1404.26 7.8781 823.21 9.104 1553.4 1519.1 1184.4 + core size:21.60 Q: 208.03 Maximum Thrust: 9056.2 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 409.11 4.578 446.51 106.67 0.0000 1218.45 2.854 389.97 3622.9 0.8500 1.40133 +FS_2 Inlet.Fl_O 409.11 4.555 446.51 106.67 0.0000 1224.59 4.127 434.06 5943.4 0.3780 1.40133 +FS_21 Fan.Fl_O 409.11 5.540 475.43 113.59 0.0000 1039.01 4.869 458.17 4515.2 0.4333 1.40114 +FS_13 Splitter.Fl_O2 363.03 5.540 475.43 113.59 0.0000 921.98 4.776 455.66 3795.6 0.4650 1.40114 +FS_22 Splitter.Fl_O1 46.08 5.540 475.43 113.59 0.0000 117.03 5.230 467.64 719.5 0.2881 1.40114 +FS_23 Duct1.Fl_O 46.08 5.526 475.43 113.59 0.0000 117.32 5.216 467.64 721.3 0.2881 1.40114 +FS_24 LPC.Fl_O 46.08 9.573 573.00 136.99 0.0000 74.35 8.701 557.59 366.0 0.3719 1.39948 +FS_25 Duct2.Fl_O 46.08 9.549 573.00 136.99 0.0000 74.54 8.679 557.59 366.9 0.3719 1.39948 +FS_3 HPC.Fl_O 46.08 41.677 916.53 220.33 0.0000 21.60 38.764 898.20 119.9 0.3249 1.38584 +FS_36 Bld3.Fl_O 41.93 41.677 916.53 220.33 0.0000 19.66 38.764 898.20 109.1 0.3249 1.38584 +FS_4 Burner.Fl_O 42.32 39.385 1553.38 386.92 0.0093 27.33 39.133 1550.84 483.4 0.0980 1.34092 +FS_45 HPT.Fl_O 46.47 14.166 1184.35 289.41 0.0085 72.85 13.336 1165.44 439.1 0.2986 1.36320 +FS_48 Duct3.Fl_O 46.47 14.095 1184.35 289.41 0.0085 73.22 13.270 1165.44 441.4 0.2986 1.36320 +FS_5 LPT.Fl_O 46.47 3.621 850.34 205.25 0.0085 241.47 3.416 836.67 1477.4 0.2915 1.38409 +FS_7 Duct4.Fl_O 46.47 3.585 850.34 205.25 0.0085 243.91 3.477 843.17 2018.9 0.2103 1.38409 +FS_9 Core_Nozz.Fl_O 46.47 3.585 850.34 205.25 0.0085 243.91 2.854 798.05 863.0 0.5829 1.38409 +FS_15 BypBld.Fl_O 363.03 5.540 475.43 113.59 0.0000 921.98 4.776 455.66 3795.6 0.4650 1.40114 +FS_17 Duct5.Fl_O 363.03 5.498 475.43 113.59 0.0000 928.95 4.741 455.66 3824.3 0.4650 1.40114 +FS_19 Byp_Nozz.Fl_O 363.03 5.498 475.43 113.59 0.0000 928.95 2.904 395.97 2706.3 1.0000 1.40114 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1224.59 1.216 0.8898 2636.754 1.0648 0.8929 -4007.6 56.77 23.91 +LPC 117.32 1.732 0.8291 2555.294 1.2052 0.8418 -1525.3 21.63 9.36 +HPC 74.54 4.365 0.8625 6112.439 1.5995 0.8871 -5433.9 39.39 39.99 +HPT 27.33 2.780 0.9164 163.008 1.2715 0.9053 5434.0 +LPT 73.22 3.892 0.9117 71.088 1.3928 0.8950 5533.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2347.97 1.150 0.9193 0.669 2.2450 0.5215 1.4369 0.9679 3943.9586 +LPC 125.84 1.224 0.8636 0.698 1.4766 0.9323 3.2631 0.9600 3662.6571 +HPC 177.20 16.554 0.8508 0.962 2.2570 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.190 0.9348 106.463 5.1901 1.4085 0.4249 0.9803 1.5311 +LPT 152.13 5.035 0.9105 87.643 5.0347 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3622.88 10467.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 694.17 166.16 14.256 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 694.17 166.16 14.256 +Duct1 0.0025 0.2881 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 694.17 166.16 14.256 +Duct2 0.0025 0.3719 365.99 +Duct3 0.0050 0.2986 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2915 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.6128 916.53 220.33 41.677 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.5344 916.53 220.33 41.677 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 475.43 113.59 5.540 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8781 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6424.6 4442.3 5434.0 +LP_Shaft 2446.5 11878.7 5533.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1553.38 0.9940 0.0550 0.39007 0.00930 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.927 0.9975 1.0000 0.9975 2706.36 1.000 973.5 11118.6 +Core_Nozz 1.256 0.9999 1.0000 0.9999 862.88 0.583 803.2 1160.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 385 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 11/ 31/ 2/ 8 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 39000.0 0.00 364.16 452.8 1.5861 718.17 9.7707 823.21 6.037 1271.5 1246.4 962.3 + core size:22.50 Q: 208.03 Maximum Thrust: 9056.2 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 364.16 4.578 446.51 106.67 0.0000 1084.58 2.854 389.97 3224.8 0.8500 1.40133 +FS_2 Inlet.Fl_O 364.16 4.555 446.51 106.67 0.0000 1090.04 4.224 436.97 5943.4 0.3298 1.40133 +FS_21 Fan.Fl_O 364.16 4.992 461.59 110.28 0.0000 1011.24 4.425 445.90 4515.2 0.4187 1.40126 +FS_13 Splitter.Fl_O2 330.35 4.992 461.59 110.28 0.0000 917.35 4.313 442.64 3795.6 0.4619 1.40126 +FS_22 Splitter.Fl_O1 33.81 4.992 461.59 110.28 0.0000 93.89 4.817 456.87 719.5 0.2268 1.40126 +FS_23 Duct1.Fl_O 33.81 4.980 461.59 110.28 0.0000 94.12 4.804 456.87 721.3 0.2268 1.40126 +FS_24 LPC.Fl_O 33.81 7.317 527.47 126.06 0.0000 68.48 6.762 515.70 366.0 0.3376 1.40036 +FS_25 Duct2.Fl_O 33.81 7.299 527.47 126.06 0.0000 68.65 6.745 515.70 366.9 0.3376 1.40036 +FS_3 HPC.Fl_O 33.81 27.639 812.29 194.81 0.0000 22.50 25.528 794.32 119.9 0.3398 1.39136 +FS_36 Bld3.Fl_O 30.77 27.639 812.29 194.81 0.0000 20.47 25.528 794.32 109.1 0.3398 1.39136 +FS_4 Burner.Fl_O 30.97 26.119 1271.52 311.41 0.0065 27.28 25.952 1269.37 483.4 0.0971 1.35906 +FS_45 HPT.Fl_O 34.01 9.283 962.29 232.64 0.0059 73.33 8.732 946.22 439.1 0.2990 1.37905 +FS_48 Duct3.Fl_O 34.01 9.237 962.29 232.64 0.0059 73.70 8.689 946.22 441.4 0.2990 1.37905 +FS_5 LPT.Fl_O 34.01 3.224 741.76 178.30 0.0059 185.39 3.119 734.91 1477.4 0.2184 1.39099 +FS_7 Duct4.Fl_O 34.01 3.192 741.76 178.30 0.0059 187.26 3.136 738.10 2018.9 0.1593 1.39099 +FS_9 Core_Nozz.Fl_O 34.01 3.192 741.76 178.30 0.0059 187.26 2.854 718.79 862.9 0.4041 1.39099 +FS_15 BypBld.Fl_O 330.35 4.992 461.59 110.28 0.0000 917.35 4.313 442.64 3795.6 0.4619 1.40126 +FS_17 Duct5.Fl_O 330.35 4.955 461.59 110.28 0.0000 924.29 4.280 442.64 3824.3 0.4619 1.40126 +FS_19 Byp_Nozz.Fl_O 330.35 4.955 461.59 110.28 0.0000 924.29 2.854 394.11 2706.4 0.9237 1.40126 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1090.04 1.096 0.7872 2117.362 1.0338 0.7900 -1859.8 79.81 26.30 +LPC 94.12 1.469 0.8156 2082.489 1.1427 0.8254 -755.0 24.86 7.48 +HPC 68.65 3.787 0.8519 6004.954 1.5400 0.8765 -3288.6 51.13 52.18 +HPT 27.28 2.813 0.9180 169.824 1.2873 0.9067 3288.6 +LPT 73.70 2.865 0.9028 63.330 1.2973 0.8889 2614.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2090.00 1.067 0.8133 0.537 2.6267 0.5215 1.4369 0.9679 3943.9586 +LPC 100.96 1.144 0.8496 0.569 1.4943 0.9323 3.2631 0.9600 3662.6571 +HPC 163.20 13.882 0.8404 0.945 2.3885 0.4206 0.2163 1.0137 6357.1603 +HPT 30.01 5.268 0.9365 110.915 5.2682 1.4085 0.4249 0.9803 1.5311 +LPT 153.14 3.602 0.9017 78.078 3.6017 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3224.82 9317.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 627.65 150.12 10.279 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 627.65 150.12 10.279 +Duct1 0.0025 0.2268 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 627.65 150.12 10.279 +Duct2 0.0025 0.3376 365.99 +Duct3 0.0050 0.2990 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2184 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.1833 812.29 194.81 27.639 +Duct5 0.0075 0.4619 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 1.8595 812.29 194.81 27.639 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 461.59 110.28 4.992 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.7707 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6055.7 2852.3 3288.6 +LP_Shaft 1964.5 6990.5 2614.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1271.52 0.9940 0.0550 0.19949 0.00648 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.736 0.9975 1.0000 0.9975 2706.36 0.924 897.1 9210.5 +Core_Nozz 1.118 0.9999 1.0000 0.9999 862.88 0.404 529.5 559.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 386 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.900 39000.0 0.00 585.69 9348.1 0.6440 6020.43 5.0408 871.64 22.718 2399.3 2338.3 1872.8 + core size:19.94 Q: 233.22 Maximum Thrust: 9348.1 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 585.69 4.828 453.35 108.31 0.0000 1666.72 2.854 389.97 4898.5 0.9000 1.40131 +FS_2 Inlet.Fl_O 585.69 4.804 453.35 108.31 0.0000 1675.11 3.835 425.02 5943.4 0.5763 1.40131 +FS_21 Fan.Fl_O 585.69 7.900 533.30 127.46 0.0000 1104.74 6.792 510.74 4515.2 0.4696 1.40024 +FS_13 Splitter.Fl_O2 488.73 7.900 533.30 127.46 0.0000 921.86 6.812 511.17 3795.6 0.4650 1.40024 +FS_22 Splitter.Fl_O1 96.96 7.900 533.30 127.46 0.0000 182.88 6.683 508.39 719.5 0.4946 1.40024 +FS_23 Duct1.Fl_O 96.96 7.881 533.30 127.46 0.0000 183.34 6.667 508.39 721.3 0.4946 1.40024 +FS_24 LPC.Fl_O 96.96 19.611 715.49 171.31 0.0000 85.33 17.159 688.89 366.0 0.4416 1.39549 +FS_25 Duct2.Fl_O 96.96 19.562 715.49 171.31 0.0000 85.55 17.116 688.89 366.9 0.4416 1.39549 +FS_3 HPC.Fl_O 96.96 109.686 1222.13 296.96 0.0000 19.94 103.228 1202.37 119.9 0.2991 1.36675 +FS_36 Bld3.Fl_O 88.23 109.686 1222.13 296.96 0.0000 18.15 103.228 1202.37 109.1 0.2991 1.36675 +FS_4 Burner.Fl_O 89.90 103.653 2399.35 631.76 0.0190 27.41 102.985 2395.74 483.4 0.0997 1.30314 +FS_45 HPT.Fl_O 98.63 38.835 1872.81 478.62 0.0172 70.92 36.683 1847.03 439.1 0.2947 1.32079 +FS_48 Duct3.Fl_O 98.63 38.641 1872.81 478.62 0.0172 71.28 36.500 1847.03 441.4 0.2947 1.32079 +FS_5 LPT.Fl_O 98.63 7.915 1299.67 321.77 0.0172 289.88 7.245 1270.17 1477.4 0.3637 1.35003 +FS_7 Duct4.Fl_O 98.63 7.836 1299.67 321.77 0.0172 292.81 7.491 1284.57 2018.9 0.2589 1.35003 +FS_9 Core_Nozz.Fl_O 98.63 7.836 1299.67 321.77 0.0172 292.81 4.186 1102.36 862.9 1.0000 1.35003 +FS_15 BypBld.Fl_O 488.73 7.900 533.30 127.46 0.0000 921.86 6.812 511.17 3795.6 0.4650 1.40024 +FS_17 Duct5.Fl_O 488.73 7.841 533.30 127.46 0.0000 928.83 6.761 511.17 3824.3 0.4650 1.40024 +FS_19 Byp_Nozz.Fl_O 488.73 7.841 533.30 127.46 0.0000 928.83 4.140 444.22 2706.3 1.0000 1.40024 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.645 0.8675 3944.235 1.1764 0.8766 -15871.2 24.71 17.45 +LPC 183.34 2.489 0.8683 3636.584 1.3416 0.8840 -6015.5 28.36 23.27 +HPC 85.55 5.607 0.8652 6325.393 1.7081 0.8922 -17236.2 20.11 20.16 +HPT 27.41 2.669 0.9133 151.669 1.2332 0.9035 17236.6 +LPT 71.28 4.882 0.9323 85.210 1.4410 0.9180 21886.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8963 1.000 2.3706 0.5215 1.4369 0.9679 3943.9586 +LPC 196.65 1.456 0.9045 0.993 1.7660 0.9323 3.2631 0.9600 3662.6571 +HPC 203.37 22.297 0.8535 0.995 2.0420 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.928 0.9317 99.058 4.9284 1.4085 0.4249 0.9803 1.5311 +LPT 148.10 6.415 0.9311 105.053 6.4152 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4898.48 15867.0 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 896.00 215.29 32.766 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 896.00 215.29 32.766 +Duct1 0.0025 0.4946 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 896.00 215.29 32.766 +Duct2 0.0025 0.4416 365.99 +Duct3 0.0050 0.2947 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3637 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.3934 1222.13 296.96 109.686 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 5.3326 1222.13 296.96 109.686 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 533.30 127.46 7.900 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0408 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7429.2 12185.4 17236.6 +LP_Shaft 3687.5 31173.0 21886.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2399.35 0.9940 0.0550 1.67234 0.01895 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.747 0.9942 1.0000 0.9975 2706.36 1.000 1031.1 19144.3 +Core_Nozz 2.746 0.9955 1.0000 0.9999 862.88 1.000 1605.5 6070.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 387 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.900 39000.0 0.00 571.06 8412.8 0.6334 5329.10 5.3028 871.64 20.829 2313.1 2254.6 1798.9 + core size:20.03 Q: 233.22 Maximum Thrust: 9348.1 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 571.06 4.828 453.35 108.31 0.0000 1625.09 2.854 389.97 4776.1 0.9000 1.40131 +FS_2 Inlet.Fl_O 571.06 4.804 453.35 108.31 0.0000 1633.27 3.899 427.05 5943.4 0.5539 1.40131 +FS_21 Fan.Fl_O 571.06 7.722 527.27 126.01 0.0000 1095.73 6.660 505.43 4515.2 0.4645 1.40036 +FS_13 Splitter.Fl_O2 480.46 7.722 527.27 126.01 0.0000 921.88 6.658 505.38 3795.6 0.4650 1.40036 +FS_22 Splitter.Fl_O1 90.60 7.722 527.27 126.01 0.0000 173.85 6.672 505.67 719.5 0.4618 1.40036 +FS_23 Duct1.Fl_O 90.60 7.703 527.27 126.01 0.0000 174.28 6.655 505.67 721.3 0.4618 1.40036 +FS_24 LPC.Fl_O 90.60 17.953 693.38 165.97 0.0000 85.75 15.682 667.25 366.0 0.4442 1.39624 +FS_25 Duct2.Fl_O 90.60 17.909 693.38 165.97 0.0000 85.97 15.643 667.25 366.9 0.4442 1.39624 +FS_3 HPC.Fl_O 90.60 100.566 1187.41 288.11 0.0000 20.03 94.586 1167.93 119.9 0.3004 1.36894 +FS_36 Bld3.Fl_O 82.45 100.566 1187.41 288.11 0.0000 18.23 94.586 1167.93 109.1 0.3004 1.36894 +FS_4 Burner.Fl_O 83.93 95.034 2313.12 605.71 0.0180 27.41 94.422 2309.61 483.4 0.0996 1.30608 +FS_45 HPT.Fl_O 92.08 35.254 1798.92 457.40 0.0163 71.49 33.268 1773.50 439.1 0.2969 1.32450 +FS_48 Duct3.Fl_O 92.08 35.078 1798.92 457.40 0.0163 71.85 33.101 1773.50 441.4 0.2969 1.32450 +FS_5 LPT.Fl_O 92.08 7.237 1249.39 308.29 0.0163 290.21 6.624 1220.74 1477.4 0.3636 1.35379 +FS_7 Duct4.Fl_O 92.08 7.165 1249.39 308.29 0.0163 293.14 6.849 1234.72 2018.9 0.2589 1.35379 +FS_9 Core_Nozz.Fl_O 92.08 7.165 1249.39 308.29 0.0163 293.14 3.824 1058.11 862.9 1.0000 1.35379 +FS_15 BypBld.Fl_O 480.46 7.722 527.27 126.01 0.0000 921.88 6.658 505.38 3795.6 0.4650 1.40036 +FS_17 Duct5.Fl_O 480.46 7.664 527.27 126.01 0.0000 928.85 6.608 505.38 3824.3 0.4650 1.40036 +FS_19 Byp_Nozz.Fl_O 480.46 7.664 527.27 126.01 0.0000 928.85 4.047 439.19 2706.4 1.0000 1.40036 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1633.27 1.608 0.8924 3743.196 1.1630 0.8994 -14305.9 28.20 17.74 +LPC 174.28 2.331 0.8660 3470.914 1.3150 0.8810 -5121.7 28.89 22.18 +HPC 85.97 5.616 0.8640 6335.966 1.7125 0.8915 -15657.5 20.50 20.53 +HPT 27.41 2.696 0.9138 152.319 1.2381 0.9039 15657.5 +LPT 71.85 4.847 0.9279 82.511 1.4398 0.9125 19427.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3131.39 1.423 0.9220 0.949 2.1758 0.5215 1.4369 0.9679 3943.9586 +LPC 186.94 1.408 0.9021 0.948 1.7522 0.9323 3.2631 0.9600 3662.6571 +HPC 204.37 22.337 0.8524 0.997 2.0712 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.991 0.9322 99.482 4.9910 1.4085 0.4249 0.9803 1.5311 +LPT 149.29 6.366 0.9267 101.725 6.3662 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4776.13 15470.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 869.21 208.72 30.018 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 869.21 208.72 30.018 +Duct1 0.0025 0.4618 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 869.21 208.72 30.018 +Duct2 0.0025 0.4442 365.99 +Duct3 0.0050 0.2969 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 3.1711 1187.41 288.11 100.566 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.9832 1187.41 288.11 100.566 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 527.27 126.01 7.722 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3028 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7325.8 11225.4 15657.5 +LP_Shaft 3499.6 29156.8 19427.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2313.12 0.9940 0.0550 1.48031 0.01795 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.686 0.9947 1.0000 0.9975 2706.36 1.000 1025.3 18538.9 +Core_Nozz 2.511 0.9976 1.0000 0.9999 862.88 1.000 1574.9 5344.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 388 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.900 39000.0 0.00 554.44 7478.5 0.6286 4701.31 5.5077 871.64 19.191 2223.9 2168.2 1725.2 + core size:20.19 Q: 233.22 Maximum Thrust: 9348.1 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 554.44 4.828 453.35 108.31 0.0000 1577.79 2.854 389.97 4637.1 0.9000 1.40131 +FS_2 Inlet.Fl_O 554.44 4.804 453.35 108.31 0.0000 1585.73 3.967 429.16 5943.4 0.5299 1.40131 +FS_21 Fan.Fl_O 554.44 7.503 521.73 124.69 0.0000 1089.22 6.486 500.44 4515.2 0.4608 1.40046 +FS_13 Splitter.Fl_O2 469.24 7.503 521.73 124.69 0.0000 921.85 6.469 500.07 3795.6 0.4650 1.40046 +FS_22 Splitter.Fl_O1 85.20 7.503 521.73 124.69 0.0000 167.38 6.570 502.30 719.5 0.4395 1.40046 +FS_23 Duct1.Fl_O 85.20 7.484 521.73 124.69 0.0000 167.79 6.554 502.30 721.3 0.4395 1.40046 +FS_24 LPC.Fl_O 85.20 16.887 679.65 162.65 0.0000 84.88 14.802 654.66 366.0 0.4383 1.39672 +FS_25 Duct2.Fl_O 85.20 16.844 679.65 162.65 0.0000 85.09 14.765 654.66 366.9 0.4383 1.39672 +FS_3 HPC.Fl_O 85.20 92.658 1157.50 280.52 0.0000 20.19 87.057 1138.12 119.9 0.3027 1.37082 +FS_36 Bld3.Fl_O 77.53 92.658 1157.50 280.52 0.0000 18.37 87.057 1138.12 109.1 0.3027 1.37082 +FS_4 Burner.Fl_O 78.84 87.562 2223.86 578.93 0.0168 27.40 86.997 2220.46 483.4 0.0994 1.30924 +FS_45 HPT.Fl_O 86.50 32.323 1725.16 436.39 0.0153 71.73 30.489 1700.38 439.1 0.2975 1.32847 +FS_48 Duct3.Fl_O 86.50 32.162 1725.16 436.39 0.0153 72.09 30.337 1700.38 441.4 0.2975 1.32847 +FS_5 LPT.Fl_O 86.50 6.642 1195.75 294.02 0.0153 290.62 6.077 1168.03 1477.4 0.3636 1.35787 +FS_7 Duct4.Fl_O 86.50 6.575 1195.75 294.02 0.0153 293.56 6.284 1181.56 2018.9 0.2589 1.35787 +FS_9 Core_Nozz.Fl_O 86.50 6.575 1195.75 294.02 0.0153 293.56 3.507 1011.03 862.9 1.0000 1.35787 +FS_15 BypBld.Fl_O 469.24 7.503 521.73 124.69 0.0000 921.85 6.469 500.07 3795.6 0.4650 1.40046 +FS_17 Duct5.Fl_O 469.24 7.446 521.73 124.69 0.0000 928.81 6.420 500.07 3824.3 0.4650 1.40046 +FS_19 Byp_Nozz.Fl_O 469.24 7.446 521.73 124.69 0.0000 928.81 3.932 434.56 2706.4 1.0000 1.40046 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1585.73 1.562 0.9023 3614.265 1.1508 0.9083 -12847.7 31.66 18.32 +LPC 167.79 2.256 0.8631 3369.106 1.3027 0.8778 -4576.6 28.06 20.50 +HPC 85.09 5.501 0.8648 6313.197 1.7031 0.8920 -14207.5 22.13 22.20 +HPT 27.40 2.709 0.9145 153.247 1.2420 0.9044 14207.3 +LPT 72.09 4.842 0.9258 81.354 1.4427 0.9100 17424.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3040.45 1.391 0.9322 0.916 2.0969 0.5215 1.4369 0.9679 3943.9586 +LPC 179.98 1.385 0.8991 0.920 1.7165 0.9323 3.2631 0.9600 3662.6571 +HPC 202.29 21.806 0.8531 0.993 2.0972 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.022 0.9328 100.089 5.0221 1.4085 0.4249 0.9803 1.5311 +LPT 149.79 6.360 0.9246 100.299 6.3601 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4637.13 15020.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 849.55 203.90 27.951 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 849.55 203.90 27.951 +Duct1 0.0025 0.4395 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 849.55 203.90 27.951 +Duct2 0.0025 0.4383 365.99 +Duct3 0.0050 0.2975 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.9819 1157.50 280.52 92.658 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.6859 1157.50 280.52 92.658 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 521.73 124.69 7.503 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5077 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7226.8 10325.2 14207.3 +LP_Shaft 3379.0 27083.3 17424.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2223.86 0.9940 0.0550 1.30592 0.01684 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.609 0.9953 1.0000 0.9975 2706.36 1.000 1019.8 17790.8 +Core_Nozz 2.304 0.9990 1.0000 0.9999 862.88 1.000 1541.5 4708.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 389 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.900 39000.0 0.00 518.63 5608.8 0.6331 3550.88 5.9851 871.64 15.992 2040.0 1990.4 1576.2 + core size:20.55 Q: 233.22 Maximum Thrust: 9348.1 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 518.63 4.828 453.35 108.31 0.0000 1475.88 2.854 389.97 4337.6 0.9000 1.40131 +FS_2 Inlet.Fl_O 518.63 4.804 453.35 108.31 0.0000 1483.31 4.097 433.14 5943.4 0.4822 1.40131 +FS_21 Fan.Fl_O 518.63 7.029 510.67 122.04 0.0000 1075.88 6.104 490.47 4515.2 0.4534 1.40065 +FS_13 Splitter.Fl_O2 444.38 7.029 510.67 122.04 0.0000 921.85 6.061 489.46 3795.6 0.4649 1.40065 +FS_22 Splitter.Fl_O1 74.25 7.029 510.67 122.04 0.0000 154.03 6.309 495.12 719.5 0.3960 1.40065 +FS_23 Duct1.Fl_O 74.25 7.012 510.67 122.04 0.0000 154.41 6.293 495.12 721.3 0.3960 1.40065 +FS_24 LPC.Fl_O 74.25 14.994 655.57 156.85 0.0000 81.82 13.295 633.51 366.0 0.4182 1.39762 +FS_25 Duct2.Fl_O 74.25 14.956 655.57 156.85 0.0000 82.02 13.262 633.51 366.9 0.4182 1.39762 +FS_3 HPC.Fl_O 74.25 77.211 1096.72 265.17 0.0000 20.55 72.363 1077.48 119.9 0.3084 1.37465 +FS_36 Bld3.Fl_O 67.57 77.211 1096.72 265.17 0.0000 18.70 72.363 1077.48 109.1 0.3084 1.37465 +FS_4 Burner.Fl_O 68.55 72.965 2039.98 524.59 0.0146 27.38 72.495 2036.82 483.4 0.0991 1.31637 +FS_45 HPT.Fl_O 75.23 26.780 1576.23 394.65 0.0133 71.97 25.250 1553.00 439.1 0.2976 1.33702 +FS_48 Duct3.Fl_O 75.23 26.646 1576.23 394.65 0.0133 72.33 25.124 1553.00 441.4 0.2976 1.33702 +FS_5 LPT.Fl_O 75.23 5.497 1087.56 265.66 0.0133 291.24 5.028 1061.81 1477.4 0.3634 1.36616 +FS_7 Duct4.Fl_O 75.23 5.442 1087.56 265.66 0.0133 294.19 5.200 1074.38 2018.9 0.2587 1.36616 +FS_9 Core_Nozz.Fl_O 75.23 5.442 1087.56 265.66 0.0133 294.19 2.896 916.54 862.9 1.0000 1.36616 +FS_15 BypBld.Fl_O 444.38 7.029 510.67 122.04 0.0000 921.85 6.061 489.46 3795.6 0.4649 1.40065 +FS_17 Duct5.Fl_O 444.38 6.977 510.67 122.04 0.0000 928.82 6.015 489.46 3824.3 0.4649 1.40065 +FS_19 Byp_Nozz.Fl_O 444.38 6.977 510.67 122.04 0.0000 928.82 3.684 425.34 2706.4 1.0000 1.40065 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1483.31 1.463 0.9105 3373.913 1.1264 0.9152 -10073.1 39.22 19.66 +LPC 154.41 2.138 0.8539 3178.924 1.2837 0.8686 -3656.7 24.91 16.43 +HPC 82.02 5.162 0.8659 6248.765 1.6729 0.8923 -11379.5 26.57 26.73 +HPT 27.38 2.725 0.9149 155.541 1.2487 0.9047 11379.7 +LPT 72.33 4.847 0.9207 79.450 1.4493 0.9037 13729.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2844.00 1.322 0.9406 0.855 2.0393 0.5215 1.4369 0.9679 3943.9586 +LPC 165.63 1.349 0.8894 0.868 1.6157 0.9323 3.2631 0.9600 3662.6571 +HPC 194.99 20.242 0.8542 0.983 2.1336 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.059 0.9332 101.587 5.0590 1.4085 0.4249 0.9803 1.5311 +LPT 150.30 6.367 0.9195 97.952 6.3668 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4337.60 14050.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 812.08 194.76 24.077 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 812.08 194.76 24.077 +Duct1 0.0025 0.3960 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 812.08 194.76 24.077 +Duct2 0.0025 0.4182 365.99 +Duct3 0.0050 0.2976 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3634 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.5987 1096.72 265.17 77.211 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.0836 1096.72 265.17 77.211 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 510.67 122.04 7.029 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9851 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7025.2 8507.6 11379.7 +LP_Shaft 3154.3 22860.7 13729.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2039.98 0.9940 0.0550 0.98636 0.01460 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.445 0.9963 1.0000 0.9975 2706.36 1.000 1009.0 16181.2 +Core_Nozz 1.907 0.9999 1.0000 0.9999 862.88 1.000 1471.7 3477.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 390 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 8/ 18/ 1/ 6 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.900 39000.0 0.00 478.39 3739.2 0.6669 2493.55 6.6832 871.64 12.699 1834.7 1791.8 1410.2 + core size:20.99 Q: 233.22 Maximum Thrust: 9348.1 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 478.39 4.828 453.35 108.31 0.0000 1361.36 2.854 389.97 4001.1 0.9000 1.40131 +FS_2 Inlet.Fl_O 478.39 4.804 453.35 108.31 0.0000 1368.22 4.221 436.87 5943.4 0.4335 1.40131 +FS_21 Fan.Fl_O 478.39 6.503 498.44 119.10 0.0000 1059.82 5.677 479.44 4515.2 0.4446 1.40084 +FS_13 Splitter.Fl_O2 416.12 6.503 498.44 119.10 0.0000 921.88 5.607 477.73 3795.6 0.4649 1.40084 +FS_22 Splitter.Fl_O1 62.26 6.503 498.44 119.10 0.0000 137.94 5.982 486.68 719.5 0.3472 1.40084 +FS_23 Duct1.Fl_O 62.26 6.487 498.44 119.10 0.0000 138.29 5.967 486.68 721.3 0.3472 1.40084 +FS_24 LPC.Fl_O 62.26 12.809 625.42 149.59 0.0000 78.44 11.493 606.37 366.0 0.3969 1.39854 +FS_25 Duct2.Fl_O 62.26 12.777 625.42 149.59 0.0000 78.64 11.464 606.37 366.9 0.3969 1.39854 +FS_3 HPC.Fl_O 62.26 61.312 1025.87 247.43 0.0000 20.99 57.283 1006.86 119.9 0.3153 1.37910 +FS_36 Bld3.Fl_O 56.66 61.312 1025.87 247.43 0.0000 19.10 57.283 1006.86 109.1 0.3153 1.37910 +FS_4 Burner.Fl_O 57.35 57.940 1834.73 465.39 0.0122 27.36 57.568 1831.82 483.4 0.0986 1.32579 +FS_45 HPT.Fl_O 62.96 21.096 1410.19 349.23 0.0111 72.32 19.878 1388.72 439.1 0.2980 1.34745 +FS_48 Duct3.Fl_O 62.96 20.990 1410.19 349.23 0.0111 72.68 19.779 1388.72 441.4 0.2980 1.34745 +FS_5 LPT.Fl_O 62.96 4.482 976.33 237.05 0.0111 283.25 4.122 954.30 1477.4 0.3505 1.37472 +FS_7 Duct4.Fl_O 62.96 4.437 976.33 237.05 0.0111 286.11 4.251 964.99 2018.9 0.2502 1.37472 +FS_9 Core_Nozz.Fl_O 62.96 4.437 976.33 237.05 0.0111 286.11 2.854 865.05 862.9 0.8237 1.37472 +FS_15 BypBld.Fl_O 416.12 6.503 498.44 119.10 0.0000 921.88 5.607 477.73 3795.6 0.4649 1.40084 +FS_17 Duct5.Fl_O 416.12 6.454 498.44 119.10 0.0000 928.85 5.565 477.73 3824.3 0.4649 1.40084 +FS_19 Byp_Nozz.Fl_O 416.12 6.454 498.44 119.10 0.0000 928.85 3.408 415.14 2706.4 1.0000 1.40084 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1368.22 1.354 0.9105 3071.228 1.0994 0.9143 -7307.0 46.49 21.24 +LPC 138.29 1.975 0.8422 2929.037 1.2548 0.8565 -2685.4 21.92 12.65 +HPC 78.64 4.798 0.8647 6190.750 1.6403 0.8904 -8619.1 31.97 32.24 +HPT 27.36 2.747 0.9155 158.708 1.2577 0.9047 8619.1 +LPT 72.68 4.684 0.9147 76.462 1.4444 0.8965 9992.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2623.37 1.246 0.9407 0.779 2.0686 0.5215 1.4369 0.9679 3943.9586 +LPC 148.33 1.299 0.8773 0.800 1.5237 0.9323 3.2631 0.9600 3662.6571 +HPC 186.95 18.560 0.8531 0.974 2.1709 0.4206 0.2163 1.0137 6357.1603 +HPT 30.10 5.111 0.9338 103.655 5.1107 1.4085 0.4249 0.9803 1.5311 +LPT 151.02 6.139 0.9135 94.268 6.1387 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4001.05 12960.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 767.16 183.83 19.888 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 767.16 183.83 19.888 +Duct1 0.0025 0.3472 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 767.16 183.83 19.888 +Duct2 0.0025 0.3969 365.99 +Duct3 0.0050 0.2980 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3505 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.1792 1025.87 247.43 61.312 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.4245 1025.87 247.43 61.312 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 498.44 119.10 6.503 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6832 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6798.0 6659.0 8619.1 +LP_Shaft 2871.3 18277.6 9992.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1834.73 0.9940 0.0550 0.69265 0.01222 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.261 0.9971 1.0000 0.9975 2706.36 1.000 996.8 14391.1 +Core_Nozz 1.555 0.9999 1.0000 0.9999 862.88 0.824 1179.6 2308.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 391 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.900 39000.0 0.00 429.75 1869.6 0.7972 1490.51 7.8695 871.64 9.135 1572.6 1538.2 1200.1 + core size:21.64 Q: 233.22 Maximum Thrust: 9348.1 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 429.75 4.828 453.35 108.31 0.0000 1222.96 2.854 389.97 3594.3 0.9000 1.40131 +FS_2 Inlet.Fl_O 429.75 4.804 453.35 108.31 0.0000 1229.11 4.349 440.61 5943.4 0.3797 1.40131 +FS_21 Fan.Fl_O 429.75 5.867 483.30 115.48 0.0000 1039.11 5.156 465.76 4515.2 0.4334 1.40105 +FS_13 Splitter.Fl_O2 381.30 5.867 483.30 115.48 0.0000 921.95 5.058 463.21 3795.6 0.4650 1.40105 +FS_22 Splitter.Fl_O1 48.45 5.867 483.30 115.48 0.0000 117.15 5.537 475.37 719.5 0.2884 1.40105 +FS_23 Duct1.Fl_O 48.45 5.852 483.30 115.48 0.0000 117.45 5.524 475.37 721.3 0.2884 1.40105 +FS_24 LPC.Fl_O 48.45 10.215 584.14 139.66 0.0000 73.97 9.295 568.62 366.0 0.3697 1.39929 +FS_25 Duct2.Fl_O 48.45 10.190 584.14 139.66 0.0000 74.16 9.272 568.62 366.9 0.3697 1.39929 +FS_3 HPC.Fl_O 48.45 44.102 931.57 224.04 0.0000 21.64 41.007 912.90 119.9 0.3257 1.38493 +FS_36 Bld3.Fl_O 44.09 44.102 931.57 224.04 0.0000 19.69 41.007 912.90 109.1 0.3257 1.38493 +FS_4 Burner.Fl_O 44.51 41.677 1572.65 392.15 0.0094 27.33 41.410 1570.08 483.4 0.0980 1.33988 +FS_45 HPT.Fl_O 48.87 15.003 1200.12 293.49 0.0085 72.81 14.125 1181.02 439.1 0.2986 1.36214 +FS_48 Duct3.Fl_O 48.87 14.928 1200.12 293.49 0.0085 73.18 14.054 1181.02 441.4 0.2986 1.36214 +FS_5 LPT.Fl_O 48.87 3.706 855.12 206.44 0.0085 248.81 3.482 840.45 1477.4 0.3014 1.38379 +FS_7 Duct4.Fl_O 48.87 3.669 855.12 206.44 0.0085 251.32 3.552 847.45 2018.9 0.2171 1.38379 +FS_9 Core_Nozz.Fl_O 48.87 3.669 855.12 206.44 0.0085 251.32 2.854 797.41 862.9 0.6127 1.38379 +FS_15 BypBld.Fl_O 381.30 5.867 483.30 115.48 0.0000 921.95 5.058 463.21 3795.6 0.4650 1.40105 +FS_17 Duct5.Fl_O 381.30 5.823 483.30 115.48 0.0000 928.92 5.020 463.21 3824.3 0.4650 1.40105 +FS_19 Byp_Nozz.Fl_O 381.30 5.823 483.30 115.48 0.0000 928.92 3.075 402.54 2706.3 1.0000 1.40105 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1229.11 1.221 0.8916 2653.781 1.0661 0.8947 -4360.2 56.15 23.76 +LPC 117.45 1.745 0.8275 2570.234 1.2086 0.8405 -1657.9 20.78 9.05 +HPC 74.16 4.328 0.8622 6105.398 1.5948 0.8868 -5784.4 40.01 40.64 +HPT 27.33 2.778 0.9165 163.384 1.2707 0.9054 5784.5 +LPT 73.18 4.028 0.9115 71.618 1.4035 0.8943 6018.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2356.65 1.154 0.9211 0.673 2.2334 0.5215 1.4369 0.9679 3943.9586 +LPC 125.98 1.228 0.8620 0.702 1.4594 0.9323 3.2631 0.9600 3662.6571 +HPC 176.30 16.385 0.8506 0.960 2.2642 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.185 0.9349 106.709 5.1846 1.4085 0.4249 0.9803 1.5311 +LPT 152.06 5.224 0.9103 88.297 5.2238 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3594.27 11642.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 706.74 169.20 15.158 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 706.74 169.20 15.158 +Duct1 0.0025 0.2884 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 706.74 169.20 15.158 +Duct2 0.0025 0.3697 365.99 +Duct3 0.0050 0.2986 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3014 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.6958 931.57 224.04 44.102 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.6649 931.57 224.04 44.102 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 483.30 115.48 5.867 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8695 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6479.3 4688.9 5784.5 +LP_Shaft 2481.1 12739.8 6018.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1572.65 0.9940 0.0550 0.41403 0.00939 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.040 0.9976 1.0000 0.9975 2706.36 1.000 981.5 12230.3 +Core_Nozz 1.286 0.9999 1.0000 0.9999 862.88 0.613 844.0 1281.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 392 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 10/ 30/ 2/ 7 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.900 39000.0 0.00 384.19 467.4 1.6317 762.66 9.7788 871.64 6.076 1288.4 1263.2 976.0 + core size:22.55 Q: 233.22 Maximum Thrust: 9348.1 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 384.19 4.828 453.35 108.31 0.0000 1093.32 2.854 389.97 3213.3 0.9000 1.40131 +FS_2 Inlet.Fl_O 384.19 4.804 453.35 108.31 0.0000 1098.82 4.449 443.49 5943.4 0.3329 1.40131 +FS_21 Fan.Fl_O 384.19 5.287 469.26 112.12 0.0000 1015.74 4.680 453.14 4515.2 0.4210 1.40120 +FS_13 Splitter.Fl_O2 348.55 5.287 469.26 112.12 0.0000 921.50 4.559 449.77 3795.6 0.4646 1.40120 +FS_22 Splitter.Fl_O1 35.64 5.287 469.26 112.12 0.0000 94.24 5.099 464.42 719.5 0.2277 1.40120 +FS_23 Duct1.Fl_O 35.64 5.274 469.26 112.12 0.0000 94.47 5.087 464.42 721.3 0.2277 1.40120 +FS_24 LPC.Fl_O 35.64 7.842 538.59 128.73 0.0000 68.07 7.254 526.74 366.0 0.3353 1.40014 +FS_25 Duct2.Fl_O 35.64 7.822 538.59 128.73 0.0000 68.24 7.236 526.74 366.9 0.3353 1.40014 +FS_3 HPC.Fl_O 35.64 29.336 826.99 198.39 0.0000 22.55 27.084 808.62 119.9 0.3407 1.39066 +FS_36 Bld3.Fl_O 32.44 29.336 826.99 198.39 0.0000 20.52 27.084 808.62 109.1 0.3407 1.39066 +FS_4 Burner.Fl_O 32.65 27.723 1288.45 315.82 0.0065 27.28 27.546 1286.27 483.4 0.0972 1.35797 +FS_45 HPT.Fl_O 35.86 9.860 975.99 236.06 0.0059 73.31 9.275 959.73 439.1 0.2990 1.37816 +FS_48 Duct3.Fl_O 35.86 9.810 975.99 236.06 0.0059 73.68 9.228 959.73 441.4 0.2990 1.37816 +FS_5 LPT.Fl_O 35.86 3.263 743.62 178.75 0.0059 193.33 3.148 736.12 1477.4 0.2284 1.39088 +FS_7 Duct4.Fl_O 35.86 3.231 743.62 178.75 0.0059 195.29 3.169 739.62 2018.9 0.1664 1.39088 +FS_9 Core_Nozz.Fl_O 35.86 3.231 743.62 178.75 0.0059 195.29 2.854 718.13 862.9 0.4259 1.39088 +FS_15 BypBld.Fl_O 348.55 5.287 469.26 112.12 0.0000 921.50 4.559 449.77 3795.6 0.4646 1.40120 +FS_17 Duct5.Fl_O 348.55 5.248 469.26 112.12 0.0000 928.47 4.525 449.77 3824.3 0.4646 1.40120 +FS_19 Byp_Nozz.Fl_O 348.55 5.248 469.26 112.12 0.0000 928.47 2.854 394.14 2706.4 0.9746 1.40120 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1098.82 1.101 0.7932 2146.115 1.0351 0.7961 -2069.5 78.43 26.39 +LPC 94.47 1.487 0.8134 2109.434 1.1477 0.8237 -837.8 23.29 7.11 +HPC 68.24 3.750 0.8508 5997.476 1.5355 0.8754 -3513.3 51.92 52.98 +HPT 27.28 2.812 0.9181 170.262 1.2865 0.9068 3513.3 +LPT 73.68 3.006 0.9033 64.225 1.3125 0.8888 2907.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2106.84 1.070 0.8195 0.544 2.6111 0.5215 1.4369 0.9679 3943.9586 +LPC 101.33 1.149 0.8473 0.576 1.4654 0.9323 3.2631 0.9600 3662.6571 +HPC 162.23 13.715 0.8394 0.943 2.3928 0.4206 0.2163 1.0137 6357.1603 +HPT 30.01 5.264 0.9365 111.201 5.2641 1.4085 0.4249 0.9803 1.5311 +LPT 153.10 3.798 0.9022 79.181 3.7985 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3213.26 10408.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 640.07 153.11 10.974 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 640.07 153.11 10.974 +Duct1 0.0025 0.2277 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 640.07 153.11 10.974 +Duct2 0.0025 0.3353 365.99 +Duct3 0.0050 0.2990 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2284 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.2475 826.99 198.39 29.336 +Duct5 0.0075 0.4646 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 1.9604 826.99 198.39 29.336 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 469.26 112.12 5.287 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.7788 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6111.5 3019.2 3513.3 +LP_Shaft 2006.4 7610.2 2907.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1288.45 0.9940 0.0550 0.21185 0.00653 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.839 0.9975 1.0000 0.9975 2706.36 0.975 946.5 10254.2 +Core_Nozz 1.132 0.9999 1.0000 0.9999 862.88 0.426 557.8 621.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 393 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 8/ 18/ 1/ 6 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 43000.0 0.00 407.69 6935.1 0.5651 3919.33 5.0388 677.94 22.739 2275.3 2217.3 1771.2 + core size:19.96 Q: 116.41 Maximum Thrust: 6935.1 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 407.69 3.267 428.31 102.31 0.0000 1666.72 2.355 389.97 5313.4 0.7000 1.40132 +FS_2 Inlet.Fl_O 407.69 3.250 428.31 102.31 0.0000 1675.11 2.595 401.55 5943.4 0.5763 1.40132 +FS_21 Fan.Fl_O 407.69 5.345 503.87 120.41 0.0000 1104.83 4.595 482.54 4515.2 0.4696 1.40076 +FS_13 Splitter.Fl_O2 340.18 5.345 503.87 120.41 0.0000 921.87 4.609 482.94 3795.6 0.4649 1.40076 +FS_22 Splitter.Fl_O1 67.51 5.345 503.87 120.41 0.0000 182.95 4.521 480.29 719.5 0.4948 1.40076 +FS_23 Duct1.Fl_O 67.51 5.332 503.87 120.41 0.0000 183.41 4.510 480.29 721.3 0.4948 1.40076 +FS_24 LPC.Fl_O 67.51 13.255 676.06 161.79 0.0000 85.45 11.592 650.78 366.0 0.4421 1.39685 +FS_25 Duct2.Fl_O 67.51 13.222 676.06 161.79 0.0000 85.67 11.564 650.78 366.9 0.4421 1.39685 +FS_3 HPC.Fl_O 67.51 74.281 1158.78 280.84 0.0000 19.96 69.897 1139.85 119.9 0.2990 1.37074 +FS_36 Bld3.Fl_O 61.44 74.281 1158.78 280.84 0.0000 18.17 69.897 1139.85 109.1 0.2990 1.37074 +FS_4 Burner.Fl_O 62.53 70.196 2275.35 594.51 0.0177 27.42 69.743 2271.89 483.4 0.0995 1.30726 +FS_45 HPT.Fl_O 68.60 26.265 1771.19 449.56 0.0161 70.93 24.810 1746.52 439.1 0.2941 1.32586 +FS_48 Duct3.Fl_O 68.60 26.134 1771.19 449.56 0.0161 71.29 24.686 1746.52 441.4 0.2941 1.32586 +FS_5 LPT.Fl_O 68.60 5.331 1222.98 301.32 0.0161 290.39 4.879 1194.80 1477.4 0.3636 1.35561 +FS_7 Duct4.Fl_O 68.60 5.278 1222.98 301.32 0.0161 293.32 5.044 1208.55 2018.9 0.2589 1.35561 +FS_9 Core_Nozz.Fl_O 68.60 5.278 1222.98 301.32 0.0161 293.32 2.816 1034.99 862.9 1.0000 1.35561 +FS_15 BypBld.Fl_O 340.18 5.345 503.87 120.41 0.0000 921.87 4.609 482.94 3795.6 0.4649 1.40076 +FS_17 Duct5.Fl_O 340.18 5.305 503.87 120.41 0.0000 928.84 4.574 482.94 3824.3 0.4649 1.40076 +FS_19 Byp_Nozz.Fl_O 340.18 5.305 503.87 120.41 0.0000 928.84 2.801 419.67 2706.4 1.0000 1.40076 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.644 0.8675 3944.235 1.1764 0.8765 -10435.9 24.71 17.46 +LPC 183.41 2.486 0.8684 3636.487 1.3417 0.8841 -3952.7 28.49 23.39 +HPC 85.67 5.618 0.8650 6328.569 1.7140 0.8924 -11372.0 20.01 20.06 +HPT 27.42 2.673 0.9132 151.471 1.2365 0.9032 11372.3 +LPT 71.29 4.902 0.9320 85.165 1.4483 0.9173 14388.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8962 1.000 2.3710 0.5215 1.4369 0.9679 3943.9586 +LPC 196.75 1.455 0.9046 0.993 1.7693 0.9323 3.2631 0.9600 3662.6571 +HPC 203.66 22.347 0.8533 0.996 2.0429 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.937 0.9315 98.929 4.9365 1.4085 0.4249 0.9803 1.5311 +LPT 148.12 6.444 0.9308 104.998 6.4436 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5313.37 8590.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 847.71 203.46 22.167 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 847.71 203.46 22.167 +Duct1 0.0025 0.4948 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 847.71 203.46 22.167 +Duct2 0.0025 0.4421 365.99 +Duct3 0.0050 0.2941 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.3629 1158.78 280.84 74.281 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.7132 1158.78 280.84 74.281 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 503.87 120.41 5.345 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0388 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7225.3 8266.7 11372.3 +LP_Shaft 3584.2 21083.7 14388.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2275.35 0.9940 0.0550 1.08870 0.01772 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.253 0.9972 1.0000 0.9975 2706.36 1.000 1002.2 11804.5 +Core_Nozz 2.241 0.9992 1.0000 0.9999 862.88 1.000 1558.5 3721.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 394 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 43000.0 0.00 397.36 6241.3 0.5550 3463.83 5.3043 677.94 20.822 2192.1 2136.4 1700.1 + core size:20.06 Q: 116.41 Maximum Thrust: 6935.1 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 397.36 3.267 428.31 102.31 0.0000 1624.48 2.355 389.97 5178.7 0.7000 1.40132 +FS_2 Inlet.Fl_O 397.36 3.250 428.31 102.31 0.0000 1632.66 2.639 403.49 5943.4 0.5536 1.40132 +FS_21 Fan.Fl_O 397.36 5.223 498.10 119.02 0.0000 1095.70 4.505 477.45 4515.2 0.4644 1.40085 +FS_13 Splitter.Fl_O2 334.33 5.223 498.10 119.02 0.0000 921.90 4.503 477.40 3795.6 0.4649 1.40085 +FS_22 Splitter.Fl_O1 63.03 5.223 498.10 119.02 0.0000 173.80 4.513 477.69 719.5 0.4616 1.40085 +FS_23 Duct1.Fl_O 63.03 5.210 498.10 119.02 0.0000 174.24 4.501 477.69 721.3 0.4616 1.40085 +FS_24 LPC.Fl_O 63.03 12.128 655.01 156.71 0.0000 85.83 10.590 630.21 366.0 0.4445 1.39764 +FS_25 Duct2.Fl_O 63.03 12.097 655.01 156.71 0.0000 86.05 10.564 630.21 366.9 0.4445 1.39764 +FS_3 HPC.Fl_O 63.03 68.020 1125.10 272.32 0.0000 20.06 63.966 1106.46 119.9 0.3003 1.37286 +FS_36 Bld3.Fl_O 57.36 68.020 1125.10 272.32 0.0000 18.25 63.966 1106.46 109.1 0.3003 1.37286 +FS_4 Burner.Fl_O 58.32 64.279 2192.06 569.66 0.0168 27.41 63.864 2188.70 483.4 0.0994 1.31015 +FS_45 HPT.Fl_O 63.99 23.813 1700.10 429.43 0.0153 71.50 22.470 1675.79 439.1 0.2963 1.32967 +FS_48 Duct3.Fl_O 63.99 23.694 1700.10 429.43 0.0153 71.86 22.358 1675.79 441.4 0.2963 1.32967 +FS_5 LPT.Fl_O 63.99 4.867 1174.80 288.57 0.0153 290.78 4.453 1147.46 1477.4 0.3637 1.35925 +FS_7 Duct4.Fl_O 63.99 4.819 1174.80 288.57 0.0153 293.72 4.605 1160.80 2018.9 0.2589 1.35925 +FS_9 Core_Nozz.Fl_O 63.99 4.819 1174.80 288.57 0.0153 293.72 2.570 992.77 862.9 1.0000 1.35925 +FS_15 BypBld.Fl_O 334.33 5.223 498.10 119.02 0.0000 921.90 4.503 477.40 3795.6 0.4649 1.40085 +FS_17 Duct5.Fl_O 334.33 5.184 498.10 119.02 0.0000 928.87 4.469 477.40 3824.3 0.4649 1.40085 +FS_19 Byp_Nozz.Fl_O 334.33 5.184 498.10 119.02 0.0000 928.87 2.737 414.86 2706.4 1.0000 1.40085 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1632.66 1.607 0.8926 3741.084 1.1629 0.8996 -9393.6 28.25 17.75 +LPC 174.24 2.328 0.8661 3469.124 1.3150 0.8809 -3360.9 28.97 22.23 +HPC 86.05 5.623 0.8639 6338.142 1.7177 0.8917 -10310.3 20.44 20.46 +HPT 27.41 2.699 0.9137 152.129 1.2414 0.9035 10310.5 +LPT 71.86 4.868 0.9275 82.451 1.4471 0.9119 12753.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3130.14 1.422 0.9222 0.949 2.1743 0.5215 1.4369 0.9679 3943.9586 +LPC 186.89 1.407 0.9022 0.947 1.7539 0.9323 3.2631 0.9600 3662.6571 +HPC 204.56 22.370 0.8523 0.997 2.0719 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 5.000 0.9320 99.358 4.9996 1.4085 0.4249 0.9803 1.5311 +LPT 149.31 6.395 0.9263 101.651 6.3954 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5178.73 8372.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 821.99 197.17 20.290 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 821.99 197.17 20.290 +Duct1 0.0025 0.4616 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 821.99 197.17 20.290 +Duct2 0.0025 0.4445 365.99 +Duct3 0.0050 0.2963 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3637 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.2061 1125.10 272.32 68.020 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.4667 1125.10 272.32 68.020 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 498.10 119.02 5.223 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3043 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7122.6 7602.8 10310.5 +LP_Shaft 3399.6 19703.3 12753.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2192.06 0.9940 0.0550 0.96218 0.01677 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.201 0.9973 1.0000 0.9975 2706.36 1.000 996.4 11389.1 +Core_Nozz 2.046 0.9998 1.0000 0.9999 862.88 1.000 1528.2 3225.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 395 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 43000.0 0.00 385.74 5548.1 0.5507 3055.56 5.5105 677.94 19.179 2107.2 2054.3 1630.3 + core size:20.21 Q: 116.41 Maximum Thrust: 6935.1 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 385.74 3.267 428.31 102.31 0.0000 1576.96 2.355 389.97 5027.2 0.7000 1.40132 +FS_2 Inlet.Fl_O 385.74 3.250 428.31 102.31 0.0000 1584.90 2.685 405.49 5943.4 0.5296 1.40132 +FS_21 Fan.Fl_O 385.74 5.073 492.84 117.76 0.0000 1089.21 4.386 472.71 4515.2 0.4607 1.40092 +FS_13 Splitter.Fl_O2 326.49 5.073 492.84 117.76 0.0000 921.91 4.374 472.36 3795.6 0.4649 1.40092 +FS_22 Splitter.Fl_O1 59.25 5.073 492.84 117.76 0.0000 167.30 4.443 474.49 719.5 0.4391 1.40092 +FS_23 Duct1.Fl_O 59.25 5.061 492.84 117.76 0.0000 167.72 4.432 474.49 721.3 0.4391 1.40092 +FS_24 LPC.Fl_O 59.25 11.410 642.08 153.60 0.0000 84.91 10.000 618.41 366.0 0.4383 1.39807 +FS_25 Duct2.Fl_O 59.25 11.382 642.08 153.60 0.0000 85.12 9.975 618.41 366.9 0.4383 1.39807 +FS_3 HPC.Fl_O 59.25 62.651 1096.40 265.09 0.0000 20.21 58.857 1077.87 119.9 0.3026 1.37467 +FS_36 Bld3.Fl_O 53.92 62.651 1096.40 265.09 0.0000 18.39 58.857 1077.87 109.1 0.3026 1.37467 +FS_4 Burner.Fl_O 54.76 59.205 2107.20 544.53 0.0157 27.40 58.824 2103.95 483.4 0.0993 1.31338 +FS_45 HPT.Fl_O 60.10 21.826 1630.28 409.81 0.0143 71.74 20.588 1606.59 439.1 0.2969 1.33364 +FS_48 Duct3.Fl_O 60.10 21.717 1630.28 409.81 0.0143 72.10 20.485 1606.59 441.4 0.2969 1.33364 +FS_5 LPT.Fl_O 60.10 4.467 1124.36 275.32 0.0143 291.08 4.086 1097.93 1477.4 0.3636 1.36311 +FS_7 Duct4.Fl_O 60.10 4.423 1124.36 275.32 0.0143 294.02 4.226 1110.83 2018.9 0.2588 1.36311 +FS_9 Core_Nozz.Fl_O 60.10 4.423 1124.36 275.32 0.0143 294.02 2.356 948.70 862.9 1.0000 1.36311 +FS_15 BypBld.Fl_O 326.49 5.073 492.84 117.76 0.0000 921.91 4.374 472.36 3795.6 0.4649 1.40092 +FS_17 Duct5.Fl_O 326.49 5.035 492.84 117.76 0.0000 928.88 4.341 472.36 3824.3 0.4649 1.40092 +FS_19 Byp_Nozz.Fl_O 326.49 5.035 492.84 117.76 0.0000 928.88 2.659 410.48 2706.4 1.0000 1.40092 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1584.90 1.561 0.9024 3612.231 1.1507 0.9084 -8431.4 31.73 18.34 +LPC 167.72 2.255 0.8631 3367.456 1.3028 0.8778 -3003.8 28.09 20.51 +HPC 85.12 5.505 0.8648 6313.955 1.7076 0.8922 -9346.3 22.07 22.14 +HPT 27.40 2.713 0.9144 153.038 1.2452 0.9041 9346.3 +LPT 72.10 4.861 0.9255 81.298 1.4500 0.9095 11435.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3038.85 1.390 0.9323 0.916 2.0962 0.5215 1.4369 0.9679 3943.9586 +LPC 179.90 1.385 0.8991 0.919 1.7169 0.9323 3.2631 0.9600 3662.6571 +HPC 202.36 21.824 0.8531 0.993 2.0964 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 5.031 0.9328 99.952 5.0307 1.4085 0.4249 0.9803 1.5311 +LPT 149.82 6.386 0.9243 100.230 6.3865 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5027.23 8127.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 803.30 192.62 18.893 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 803.30 192.62 18.893 +Duct1 0.0025 0.4391 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 803.30 192.62 18.893 +Duct2 0.0025 0.4383 365.99 +Duct3 0.0050 0.2969 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.0737 1096.40 265.09 62.651 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.2587 1096.40 265.09 62.651 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 492.84 117.76 5.073 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5105 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7025.1 6987.5 9346.3 +LP_Shaft 3282.5 18296.8 11435.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2107.20 0.9940 0.0550 0.84877 0.01574 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.138 0.9975 1.0000 0.9975 2706.36 1.000 991.1 10880.8 +Core_Nozz 1.878 0.9999 1.0000 0.9999 862.88 1.000 1495.8 2795.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 396 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 43000.0 0.00 359.63 4161.0 0.5555 2311.42 5.9880 677.94 15.941 1935.1 1887.8 1490.5 + core size:20.54 Q: 116.41 Maximum Thrust: 6935.1 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 359.63 3.267 428.31 102.31 0.0000 1470.20 2.355 389.97 4686.9 0.7000 1.40132 +FS_2 Inlet.Fl_O 359.63 3.250 428.31 102.31 0.0000 1477.60 2.776 409.40 5943.4 0.4797 1.40132 +FS_21 Fan.Fl_O 359.63 4.734 481.80 115.12 0.0000 1075.94 4.111 462.72 4515.2 0.4534 1.40107 +FS_13 Splitter.Fl_O2 308.16 4.734 481.80 115.12 0.0000 921.97 4.082 461.77 3795.6 0.4650 1.40107 +FS_22 Splitter.Fl_O1 51.46 4.734 481.80 115.12 0.0000 153.97 4.249 467.12 719.5 0.3957 1.40107 +FS_23 Duct1.Fl_O 51.46 4.722 481.80 115.12 0.0000 154.36 4.239 467.12 721.3 0.3957 1.40107 +FS_24 LPC.Fl_O 51.46 10.017 616.88 147.53 0.0000 82.34 8.865 595.77 366.0 0.4215 1.39874 +FS_25 Duct2.Fl_O 51.46 9.992 616.88 147.53 0.0000 82.55 8.843 595.77 366.9 0.4215 1.39874 +FS_3 HPC.Fl_O 51.46 52.073 1037.35 250.29 0.0000 20.54 48.807 1019.05 119.9 0.3078 1.37838 +FS_36 Bld3.Fl_O 46.83 52.073 1037.35 250.29 0.0000 18.69 48.807 1019.05 109.1 0.3078 1.37838 +FS_4 Burner.Fl_O 47.47 49.209 1935.13 494.34 0.0137 27.39 48.892 1932.10 483.4 0.0989 1.32076 +FS_45 HPT.Fl_O 52.11 18.025 1490.48 371.15 0.0125 72.02 16.994 1468.24 439.1 0.2972 1.34204 +FS_48 Duct3.Fl_O 52.11 17.934 1490.48 371.15 0.0125 72.38 16.909 1468.24 441.4 0.2972 1.34204 +FS_5 LPT.Fl_O 52.11 3.783 1029.70 250.77 0.0125 285.23 3.474 1006.28 1477.4 0.3540 1.37042 +FS_7 Duct4.Fl_O 52.11 3.745 1029.70 250.77 0.0125 288.11 3.586 1017.67 2018.9 0.2525 1.37042 +FS_9 Core_Nozz.Fl_O 52.11 3.745 1029.70 250.77 0.0125 288.11 2.355 907.42 862.9 0.8473 1.37042 +FS_15 BypBld.Fl_O 308.16 4.734 481.80 115.12 0.0000 921.97 4.082 461.77 3795.6 0.4650 1.40107 +FS_17 Duct5.Fl_O 308.16 4.699 481.80 115.12 0.0000 928.93 4.051 461.77 3824.3 0.4650 1.40107 +FS_19 Byp_Nozz.Fl_O 308.16 4.699 481.80 115.12 0.0000 928.93 2.481 401.28 2706.4 1.0000 1.40107 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1477.60 1.457 0.9104 3358.929 1.1249 0.9151 -6514.7 39.79 19.81 +LPC 154.36 2.121 0.8550 3167.007 1.2804 0.8694 -2360.3 25.62 16.86 +HPC 82.55 5.212 0.8657 6258.619 1.6816 0.8923 -7482.2 26.02 26.16 +HPT 27.39 2.730 0.9148 155.159 1.2525 0.9044 7482.3 +LPT 72.38 4.741 0.9210 79.063 1.4475 0.9042 8875.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2833.07 1.318 0.9406 0.852 2.0423 0.5215 1.4369 0.9679 3943.9586 +LPC 165.56 1.344 0.8906 0.865 1.6319 0.9323 3.2631 0.9600 3662.6571 +HPC 196.24 20.469 0.8541 0.984 2.1344 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.072 0.9332 101.337 5.0720 1.4085 0.4249 0.9803 1.5311 +LPT 150.39 6.219 0.9198 97.475 6.2190 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4686.90 7577.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 765.79 183.50 16.157 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 765.79 183.50 16.157 +Duct1 0.0025 0.3957 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 765.79 183.50 16.157 +Duct2 0.0025 0.4215 365.99 +Duct3 0.0050 0.2972 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3540 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.8012 1037.35 250.29 52.073 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.8305 1037.35 250.29 52.073 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 481.80 115.12 4.734 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9880 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6825.5 5757.5 7482.3 +LP_Shaft 3052.4 15271.0 8875.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1935.13 0.9940 0.0550 0.64206 0.01371 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.995 0.9976 1.0000 0.9975 2706.36 1.000 980.0 9728.6 +Core_Nozz 1.590 0.9999 1.0000 0.9999 862.88 0.847 1241.2 2010.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:56 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 397 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 43000.0 0.00 329.10 2774.1 0.5853 1623.67 6.7042 677.94 12.543 1743.8 1702.5 1335.6 + core size:20.92 Q: 116.41 Maximum Thrust: 6935.1 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 329.10 3.267 428.31 102.31 0.0000 1345.40 2.355 389.97 4289.0 0.7000 1.40132 +FS_2 Inlet.Fl_O 329.10 3.250 428.31 102.31 0.0000 1352.17 2.867 413.19 5943.4 0.4271 1.40132 +FS_21 Fan.Fl_O 329.10 4.344 469.10 112.08 0.0000 1058.77 3.794 451.25 4515.2 0.4439 1.40121 +FS_13 Splitter.Fl_O2 286.38 4.344 469.10 112.08 0.0000 921.34 3.746 449.63 3795.6 0.4645 1.40121 +FS_22 Splitter.Fl_O1 42.72 4.344 469.10 112.08 0.0000 137.43 3.999 458.12 719.5 0.3456 1.40121 +FS_23 Duct1.Fl_O 42.72 4.333 469.10 112.08 0.0000 137.77 3.989 458.12 721.3 0.3456 1.40121 +FS_24 LPC.Fl_O 42.72 8.371 584.07 139.65 0.0000 79.58 7.482 565.64 366.0 0.4039 1.39929 +FS_25 Duct2.Fl_O 42.72 8.350 584.07 139.65 0.0000 79.78 7.463 565.64 366.9 0.4039 1.39929 +FS_3 HPC.Fl_O 42.72 40.974 966.61 232.70 0.0000 20.92 38.302 948.71 119.9 0.3136 1.38278 +FS_36 Bld3.Fl_O 38.87 40.974 966.61 232.70 0.0000 19.03 38.302 948.71 109.1 0.3136 1.38278 +FS_4 Burner.Fl_O 39.32 38.720 1743.84 439.87 0.0116 27.37 38.471 1741.05 483.4 0.0985 1.33017 +FS_45 HPT.Fl_O 43.17 14.049 1335.65 329.33 0.0106 72.46 13.235 1315.02 439.1 0.2981 1.35229 +FS_48 Duct3.Fl_O 43.17 13.979 1335.65 329.33 0.0106 72.83 13.169 1315.02 441.4 0.2981 1.35229 +FS_5 LPT.Fl_O 43.17 3.242 939.10 227.61 0.0106 263.34 3.020 921.04 1477.4 0.3220 1.37745 +FS_7 Duct4.Fl_O 43.17 3.209 939.10 227.61 0.0106 266.00 3.094 929.71 2018.9 0.2312 1.37745 +FS_9 Core_Nozz.Fl_O 43.17 3.209 939.10 227.61 0.0106 266.00 2.355 862.46 862.8 0.6834 1.37745 +FS_15 BypBld.Fl_O 286.38 4.344 469.10 112.08 0.0000 921.34 3.746 449.63 3795.6 0.4645 1.40121 +FS_17 Duct5.Fl_O 286.38 4.312 469.10 112.08 0.0000 928.30 3.718 449.63 3824.3 0.4645 1.40121 +FS_19 Byp_Nozz.Fl_O 286.38 4.312 469.10 112.08 0.0000 928.30 2.355 394.48 2706.3 0.9709 1.40121 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1352.17 1.337 0.9095 3024.228 1.0952 0.9131 -4546.4 47.74 21.62 +LPC 137.77 1.932 0.8453 2889.753 1.2451 0.8590 -1666.2 23.83 13.56 +HPC 79.78 4.907 0.8648 6210.168 1.6550 0.8908 -5623.9 30.51 30.73 +HPT 27.37 2.756 0.9153 157.811 1.2615 0.9046 5623.9 +LPT 72.83 4.312 0.9173 75.197 1.4223 0.9004 6212.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2592.62 1.234 0.9396 0.767 2.0842 0.5215 1.4369 0.9679 3943.9586 +LPC 147.78 1.286 0.8805 0.789 1.5652 0.9323 3.2631 0.9600 3662.6571 +HPC 189.67 19.061 0.8532 0.977 2.1668 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.133 0.9337 103.069 5.1330 1.4085 0.4249 0.9803 1.5311 +LPT 151.32 5.621 0.9161 92.709 5.6207 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4289.04 6934.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 719.22 172.21 13.129 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 719.22 172.21 13.129 +Duct1 0.0025 0.3456 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 719.22 172.21 13.129 +Duct2 0.0025 0.4039 365.99 +Duct3 0.0050 0.2981 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3220 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.4951 966.61 232.70 40.974 +Duct5 0.0075 0.4645 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.3494 966.61 232.70 40.974 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 469.10 112.08 4.344 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.7042 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6590.1 4482.1 5623.9 +LP_Shaft 2748.2 11873.2 6212.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1743.84 0.9940 0.0550 0.45102 0.01160 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.831 0.9975 1.0000 0.9975 2706.36 0.971 943.4 8397.2 +Core_Nozz 1.363 0.9999 1.0000 0.9999 862.88 0.683 977.4 1311.4 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 398 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 43000.0 0.00 290.69 1387.0 0.6998 970.67 7.8609 677.94 8.910 1496.3 1462.7 1137.5 + core size:21.49 Q: 116.41 Maximum Thrust: 6935.1 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 290.69 3.267 428.31 102.31 0.0000 1188.38 2.355 389.97 3788.5 0.7000 1.40132 +FS_2 Inlet.Fl_O 290.69 3.250 428.31 102.31 0.0000 1194.36 2.961 417.05 5943.4 0.3669 1.40132 +FS_21 Fan.Fl_O 290.69 3.902 454.18 108.51 0.0000 1024.55 3.444 438.25 4515.2 0.4257 1.40131 +FS_13 Splitter.Fl_O2 257.88 3.902 454.18 108.51 0.0000 908.93 3.382 435.97 3795.6 0.4563 1.40131 +FS_22 Splitter.Fl_O1 32.81 3.902 454.18 108.51 0.0000 115.63 3.689 446.94 719.5 0.2842 1.40131 +FS_23 Duct1.Fl_O 32.81 3.892 454.18 108.51 0.0000 115.92 3.679 446.94 721.3 0.2842 1.40131 +FS_24 LPC.Fl_O 32.81 6.515 540.73 129.24 0.0000 75.56 5.899 525.62 366.0 0.3791 1.40009 +FS_25 Duct2.Fl_O 32.81 6.498 540.73 129.24 0.0000 75.75 5.885 525.62 366.9 0.3791 1.40009 +FS_3 HPC.Fl_O 32.81 29.105 872.75 209.59 0.0000 21.49 27.093 855.43 119.9 0.3227 1.38841 +FS_36 Bld3.Fl_O 29.85 29.105 872.75 209.59 0.0000 19.55 27.093 855.43 109.1 0.3227 1.38841 +FS_4 Burner.Fl_O 30.12 27.504 1496.25 371.47 0.0090 27.34 27.327 1493.79 483.4 0.0979 1.34410 +FS_45 HPT.Fl_O 33.08 9.861 1137.50 277.33 0.0082 73.00 9.281 1119.14 439.1 0.2989 1.36635 +FS_48 Duct3.Fl_O 33.08 9.812 1137.50 277.33 0.0082 73.36 9.235 1119.14 441.4 0.2989 1.36635 +FS_5 LPT.Fl_O 33.08 2.823 838.67 202.34 0.0082 218.93 2.693 827.75 1477.4 0.2616 1.38484 +FS_7 Duct4.Fl_O 33.08 2.795 838.67 202.34 0.0082 221.15 2.726 832.89 2018.9 0.1897 1.38484 +FS_9 Core_Nozz.Fl_O 33.08 2.795 838.67 202.34 0.0082 221.15 2.355 799.58 862.9 0.5033 1.38484 +FS_15 BypBld.Fl_O 257.88 3.902 454.18 108.51 0.0000 908.93 3.382 435.97 3795.6 0.4563 1.40131 +FS_17 Duct5.Fl_O 257.88 3.873 454.18 108.51 0.0000 915.79 3.357 435.97 3824.3 0.4563 1.40131 +FS_19 Byp_Nozz.Fl_O 257.88 3.873 454.18 108.51 0.0000 915.79 2.355 393.86 2706.4 0.8736 1.40131 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1194.36 1.200 0.8890 2556.810 1.0604 0.8919 -2547.1 57.83 23.56 +LPC 115.92 1.674 0.8334 2482.915 1.1906 0.8451 -962.5 24.86 10.35 +HPC 75.75 4.479 0.8630 6135.133 1.6140 0.8881 -3729.1 37.56 38.08 +HPT 27.34 2.789 0.9163 161.945 1.2744 0.9051 3729.1 +LPT 73.36 3.475 0.9101 68.890 1.3563 0.8948 3509.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2290.02 1.139 0.9185 0.648 2.2529 0.5215 1.4369 0.9679 3943.9586 +LPC 124.33 1.207 0.8681 0.678 1.5394 0.9323 3.2631 0.9600 3662.6571 +HPC 180.09 17.082 0.8514 0.965 2.2377 0.4206 0.2163 1.0137 6357.1603 +HPT 30.08 5.211 0.9346 105.769 5.2109 1.4085 0.4249 0.9803 1.5311 +LPT 152.44 4.453 0.9090 84.933 4.4532 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3788.46 6125.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 657.72 157.36 9.810 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 657.72 157.36 9.810 +Duct1 0.0025 0.2842 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 657.72 157.36 9.810 +Duct2 0.0025 0.3791 365.99 +Duct3 0.0050 0.2989 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2616 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.1482 872.75 209.59 29.105 +Duct5 0.0075 0.4563 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 1.8043 872.75 209.59 29.105 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 454.18 108.51 3.902 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8609 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6264.3 3126.6 3729.1 +LP_Shaft 2323.4 7933.4 3509.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1496.25 0.9940 0.0550 0.26963 0.00903 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.645 0.9975 1.0000 0.9975 2706.36 0.874 848.2 6798.4 +Core_Nozz 1.187 0.9999 1.0000 0.9999 862.88 0.503 694.2 713.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 399 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 11/ 21/ 1/ 9 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.700 43000.0 0.00 251.92 346.8 1.4017 486.06 9.6188 677.94 5.798 1213.7 1189.3 916.0 + core size:22.39 Q: 116.41 Maximum Thrust: 6935.1 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 251.92 3.267 428.31 102.31 0.0000 1029.90 2.355 389.97 3283.3 0.7000 1.40132 +FS_2 Inlet.Fl_O 251.92 3.250 428.31 102.31 0.0000 1035.09 3.039 420.16 5943.4 0.3110 1.40132 +FS_21 Fan.Fl_O 251.92 3.523 440.96 105.34 0.0000 969.06 3.159 427.42 4515.2 0.3972 1.40134 +FS_13 Splitter.Fl_O2 228.20 3.523 440.96 105.34 0.0000 877.80 3.091 424.74 3795.6 0.4361 1.40134 +FS_22 Splitter.Fl_O1 23.72 3.523 440.96 105.34 0.0000 91.26 3.406 436.71 719.5 0.2201 1.40134 +FS_23 Duct1.Fl_O 23.72 3.514 440.96 105.34 0.0000 91.49 3.397 436.71 721.3 0.2201 1.40134 +FS_24 LPC.Fl_O 23.72 4.906 494.82 118.24 0.0000 69.41 4.523 483.43 366.0 0.3428 1.40090 +FS_25 Duct2.Fl_O 23.72 4.894 494.82 118.24 0.0000 69.59 4.511 483.43 366.9 0.3428 1.40090 +FS_3 HPC.Fl_O 23.72 18.939 767.27 183.86 0.0000 22.39 17.507 750.42 119.9 0.3376 1.39352 +FS_36 Bld3.Fl_O 21.59 18.939 767.27 183.86 0.0000 20.38 17.507 750.42 109.1 0.3376 1.39352 +FS_4 Burner.Fl_O 21.72 17.898 1213.75 296.42 0.0063 27.29 17.783 1211.68 483.4 0.0970 1.36286 +FS_45 HPT.Fl_O 23.86 6.349 916.02 221.10 0.0057 73.39 5.972 900.62 439.1 0.2990 1.38207 +FS_48 Duct3.Fl_O 23.86 6.318 916.02 221.10 0.0057 73.76 5.942 900.62 441.4 0.2990 1.38207 +FS_5 LPT.Fl_O 23.86 2.579 733.74 176.32 0.0057 161.68 2.516 728.63 1477.4 0.1891 1.39143 +FS_7 Duct4.Fl_O 23.86 2.554 733.74 176.32 0.0057 163.32 2.520 730.99 2018.9 0.1384 1.39143 +FS_9 Core_Nozz.Fl_O 23.86 2.554 733.74 176.32 0.0057 163.32 2.355 717.19 862.8 0.3432 1.39143 +FS_15 BypBld.Fl_O 228.20 3.523 440.96 105.34 0.0000 877.80 3.091 424.74 3795.6 0.4361 1.40134 +FS_17 Duct5.Fl_O 228.20 3.496 440.96 105.34 0.0000 884.43 3.068 424.74 3824.3 0.4361 1.40134 +FS_19 Byp_Nozz.Fl_O 228.20 3.496 440.96 105.34 0.0000 884.43 2.355 393.75 2706.4 0.7730 1.40134 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1035.09 1.084 0.7896 1986.771 1.0295 0.7920 -1078.8 83.26 24.31 +LPC 91.49 1.396 0.8207 1958.079 1.1222 0.8290 -432.9 31.03 8.64 +HPC 69.59 3.870 0.8541 6022.192 1.5506 0.8786 -2202.7 49.40 50.39 +HPT 27.29 2.819 0.9179 168.838 1.2900 0.9062 2202.7 +LPT 73.76 2.449 0.8999 59.652 1.2484 0.8879 1511.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 1984.64 1.058 0.8157 0.504 2.6195 0.5215 1.4369 0.9679 3943.9586 +LPC 98.13 1.121 0.8549 0.535 1.6024 0.9323 3.2631 0.9600 3662.6571 +HPC 165.43 14.268 0.8426 0.947 2.3784 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.281 0.9363 110.271 5.2808 1.4085 0.4249 0.9803 1.5311 +LPT 153.26 3.022 0.8987 73.544 3.0217 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3283.26 5308.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 590.56 141.21 6.951 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 590.56 141.21 6.951 +Duct1 0.0025 0.2201 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 590.56 141.21 6.951 +Duct2 0.0025 0.3428 365.99 +Duct3 0.0050 0.2990 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1891 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 0.8304 767.27 183.86 18.939 +Duct5 0.0075 0.4361 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 1.3048 767.27 183.86 18.939 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 440.96 105.34 3.523 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.6188 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 5882.1 1966.7 2202.7 +LP_Shaft 1805.4 4397.6 1511.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1213.75 0.9940 0.0550 0.13502 0.00625 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.485 0.9975 1.0000 0.9975 2706.36 0.773 750.3 5321.9 +Core_Nozz 1.084 0.9999 1.0000 0.9999 862.88 0.343 449.3 333.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 400 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 43000.0 0.00 424.07 7082.6 0.5846 4140.48 5.0391 726.36 22.736 2303.6 2244.8 1794.3 + core size:19.96 Q: 133.63 Maximum Thrust: 7082.6 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 424.07 3.420 433.98 103.67 0.0000 1666.72 2.355 389.97 5158.3 0.7500 1.40134 +FS_2 Inlet.Fl_O 424.07 3.403 433.98 103.67 0.0000 1675.11 2.717 406.87 5943.4 0.5763 1.40134 +FS_21 Fan.Fl_O 424.07 5.597 510.54 122.00 0.0000 1104.79 4.811 488.93 4515.2 0.4696 1.40066 +FS_13 Splitter.Fl_O2 353.85 5.597 510.54 122.00 0.0000 921.85 4.825 489.34 3795.6 0.4649 1.40066 +FS_22 Splitter.Fl_O1 70.22 5.597 510.54 122.00 0.0000 182.94 4.734 486.66 719.5 0.4948 1.40066 +FS_23 Duct1.Fl_O 70.22 5.583 510.54 122.00 0.0000 183.40 4.722 486.66 721.3 0.4948 1.40066 +FS_24 LPC.Fl_O 70.22 13.883 685.02 163.95 0.0000 85.42 12.143 659.44 366.0 0.4420 1.39653 +FS_25 Duct2.Fl_O 70.22 13.848 685.02 163.95 0.0000 85.64 12.112 659.44 366.9 0.4420 1.39653 +FS_3 HPC.Fl_O 70.22 77.762 1173.22 284.50 0.0000 19.96 73.175 1154.10 119.9 0.2990 1.36983 +FS_36 Bld3.Fl_O 63.90 77.762 1173.22 284.50 0.0000 18.16 73.175 1154.10 109.1 0.2990 1.36983 +FS_4 Burner.Fl_O 65.05 73.485 2303.56 602.94 0.0180 27.42 73.011 2300.06 483.4 0.0996 1.30631 +FS_45 HPT.Fl_O 71.37 27.504 1794.29 456.13 0.0164 70.93 25.980 1769.37 439.1 0.2943 1.32468 +FS_48 Duct3.Fl_O 71.37 27.367 1794.29 456.13 0.0164 71.28 25.851 1769.37 441.4 0.2943 1.32468 +FS_5 LPT.Fl_O 71.37 5.588 1240.38 305.94 0.0164 290.26 5.114 1211.90 1477.4 0.3636 1.35433 +FS_7 Duct4.Fl_O 71.37 5.532 1240.38 305.94 0.0164 293.20 5.288 1225.80 2018.9 0.2589 1.35433 +FS_9 Core_Nozz.Fl_O 71.37 5.532 1240.38 305.94 0.0164 293.20 2.952 1050.25 862.9 1.0000 1.35433 +FS_15 BypBld.Fl_O 353.85 5.597 510.54 122.00 0.0000 921.85 4.825 489.34 3795.6 0.4649 1.40066 +FS_17 Duct5.Fl_O 353.85 5.555 510.54 122.00 0.0000 928.81 4.789 489.34 3824.3 0.4649 1.40066 +FS_19 Byp_Nozz.Fl_O 353.85 5.555 510.54 122.00 0.0000 928.81 2.933 425.23 2706.4 1.0000 1.40066 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.645 0.8675 3944.235 1.1764 0.8765 -10999.2 24.71 17.45 +LPC 183.40 2.487 0.8684 3636.500 1.3417 0.8841 -4167.2 28.45 23.35 +HPC 85.64 5.615 0.8650 6327.797 1.7127 0.8924 -11977.3 20.04 20.09 +HPT 27.42 2.672 0.9132 151.516 1.2357 0.9033 11977.5 +LPT 71.28 4.897 0.9321 85.174 1.4466 0.9175 15166.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8963 1.000 2.3708 0.5215 1.4369 0.9679 3943.9586 +LPC 196.72 1.456 0.9046 0.993 1.7683 0.9323 3.2631 0.9600 3662.6571 +HPC 203.59 22.335 0.8534 0.995 2.0426 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.935 0.9315 98.958 4.9346 1.4085 0.4249 0.9803 1.5311 +LPT 148.12 6.437 0.9309 105.009 6.4368 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5158.28 9573.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 858.69 206.14 23.212 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 858.69 206.14 23.212 +Duct1 0.0025 0.4948 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 858.69 206.14 23.212 +Duct2 0.0025 0.4420 365.99 +Duct3 0.0050 0.2943 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.4577 1173.22 284.50 77.762 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.8621 1173.22 284.50 77.762 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 510.54 122.00 5.597 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0391 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7272.1 8650.5 11977.5 +LP_Shaft 3607.9 22078.0 15166.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2303.56 0.9940 0.0550 1.15013 0.01800 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.359 0.9968 1.0000 0.9975 2706.36 1.000 1008.8 12659.5 +Core_Nozz 2.349 0.9987 1.0000 0.9999 862.88 1.000 1569.3 3996.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 401 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 43000.0 0.00 413.38 6374.1 0.5744 3661.41 5.3030 726.36 20.829 2219.7 2163.4 1722.6 + core size:20.05 Q: 133.63 Maximum Thrust: 7082.6 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 413.38 3.420 433.98 103.67 0.0000 1624.73 2.355 389.97 5028.3 0.7500 1.40134 +FS_2 Inlet.Fl_O 413.38 3.403 433.98 103.67 0.0000 1632.91 2.763 408.83 5943.4 0.5538 1.40134 +FS_21 Fan.Fl_O 413.38 5.469 504.72 120.61 0.0000 1095.72 4.717 483.80 4515.2 0.4644 1.40075 +FS_13 Splitter.Fl_O2 347.80 5.469 504.72 120.61 0.0000 921.88 4.716 483.75 3795.6 0.4650 1.40075 +FS_22 Splitter.Fl_O1 65.58 5.469 504.72 120.61 0.0000 173.84 4.725 484.03 719.5 0.4617 1.40075 +FS_23 Duct1.Fl_O 65.58 5.456 504.72 120.61 0.0000 174.28 4.713 484.03 721.3 0.4617 1.40075 +FS_24 LPC.Fl_O 65.58 12.704 663.72 158.81 0.0000 85.82 11.094 638.62 366.0 0.4445 1.39731 +FS_25 Duct2.Fl_O 65.58 12.672 663.72 158.81 0.0000 86.04 11.066 638.62 366.9 0.4445 1.39731 +FS_3 HPC.Fl_O 65.58 71.241 1139.37 275.93 0.0000 20.05 66.997 1120.53 119.9 0.3003 1.37196 +FS_36 Bld3.Fl_O 59.68 71.241 1139.37 275.93 0.0000 18.25 66.997 1120.53 109.1 0.3003 1.37196 +FS_4 Burner.Fl_O 60.70 67.322 2219.69 577.85 0.0170 27.41 66.888 2216.30 483.4 0.0995 1.30922 +FS_45 HPT.Fl_O 66.60 24.948 1722.60 435.77 0.0155 71.50 23.542 1698.04 439.1 0.2964 1.32847 +FS_48 Duct3.Fl_O 66.60 24.823 1722.60 435.77 0.0155 71.86 23.424 1698.04 441.4 0.2964 1.32847 +FS_5 LPT.Fl_O 66.60 5.105 1191.75 293.03 0.0155 290.65 4.670 1164.10 1477.4 0.3637 1.35800 +FS_7 Duct4.Fl_O 66.60 5.053 1191.75 293.03 0.0155 293.59 4.830 1177.60 2018.9 0.2589 1.35800 +FS_9 Core_Nozz.Fl_O 66.60 5.053 1191.75 293.03 0.0155 293.59 2.695 1007.59 862.9 1.0000 1.35800 +FS_15 BypBld.Fl_O 347.80 5.469 504.72 120.61 0.0000 921.88 4.716 483.75 3795.6 0.4650 1.40075 +FS_17 Duct5.Fl_O 347.80 5.428 504.72 120.61 0.0000 928.85 4.680 483.75 3824.3 0.4650 1.40075 +FS_19 Byp_Nozz.Fl_O 347.80 5.428 504.72 120.61 0.0000 928.85 2.866 420.38 2706.4 1.0000 1.40075 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1632.91 1.607 0.8925 3741.935 1.1630 0.8995 -9906.1 28.23 17.74 +LPC 174.28 2.329 0.8661 3469.826 1.3150 0.8810 -3544.8 28.96 22.23 +HPC 86.04 5.622 0.8639 6337.938 1.7166 0.8917 -10867.5 20.45 20.48 +HPT 27.41 2.698 0.9137 152.177 1.2407 0.9036 10867.6 +LPT 71.86 4.863 0.9276 82.470 1.4454 0.9121 13450.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3130.65 1.423 0.9221 0.949 2.1749 0.5215 1.4369 0.9679 3943.9586 +LPC 186.93 1.407 0.9022 0.947 1.7539 0.9323 3.2631 0.9600 3662.6571 +HPC 204.54 22.366 0.8523 0.997 2.0720 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.998 0.9321 99.390 4.9976 1.4085 0.4249 0.9803 1.5311 +LPT 149.30 6.389 0.9264 101.675 6.3888 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5028.33 9332.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 832.75 199.80 21.252 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 832.75 199.80 21.252 +Duct1 0.0025 0.4617 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 832.75 199.80 21.252 +Duct2 0.0025 0.4445 365.99 +Duct3 0.0050 0.2964 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3637 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.2955 1139.37 275.93 71.241 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.6071 1139.37 275.93 71.241 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 504.72 120.61 5.469 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3030 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7169.6 7961.1 10867.6 +LP_Shaft 3422.8 20638.7 13450.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2219.69 0.9940 0.0550 1.01706 0.01704 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.305 0.9970 1.0000 0.9975 2706.36 1.000 1003.0 12227.0 +Core_Nozz 2.146 0.9996 1.0000 0.9999 862.88 1.000 1539.0 3479.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 402 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 43000.0 0.00 401.33 5666.1 0.5702 3230.66 5.5090 726.36 19.189 2134.0 2080.5 1652.1 + core size:20.20 Q: 133.63 Maximum Thrust: 7082.6 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 401.33 3.420 433.98 103.67 0.0000 1577.36 2.355 389.97 4881.7 0.7500 1.40134 +FS_2 Inlet.Fl_O 401.33 3.403 433.98 103.67 0.0000 1585.30 2.811 410.85 5943.4 0.5298 1.40134 +FS_21 Fan.Fl_O 401.33 5.313 499.41 119.34 0.0000 1089.22 4.593 479.02 4515.2 0.4608 1.40083 +FS_13 Splitter.Fl_O2 339.67 5.313 499.41 119.34 0.0000 921.88 4.581 478.66 3795.6 0.4649 1.40083 +FS_22 Splitter.Fl_O1 61.66 5.313 499.41 119.34 0.0000 167.34 4.653 480.81 719.5 0.4393 1.40083 +FS_23 Duct1.Fl_O 61.66 5.300 499.41 119.34 0.0000 167.76 4.642 480.81 721.3 0.4393 1.40083 +FS_24 LPC.Fl_O 61.66 11.954 650.66 155.66 0.0000 84.90 10.477 626.68 366.0 0.4383 1.39779 +FS_25 Duct2.Fl_O 61.66 11.924 650.66 155.66 0.0000 85.11 10.451 626.68 366.9 0.4383 1.39779 +FS_3 HPC.Fl_O 61.66 65.630 1110.42 268.62 0.0000 20.20 61.658 1091.69 119.9 0.3026 1.37379 +FS_36 Bld3.Fl_O 56.11 65.630 1110.42 268.62 0.0000 18.38 61.658 1091.69 109.1 0.3026 1.37379 +FS_4 Burner.Fl_O 57.01 62.020 2134.01 552.40 0.0160 27.40 61.621 2130.73 483.4 0.0993 1.31238 +FS_45 HPT.Fl_O 62.56 22.872 1652.07 415.89 0.0146 71.74 21.574 1628.14 439.1 0.2971 1.33243 +FS_48 Duct3.Fl_O 62.56 22.757 1652.07 415.89 0.0146 72.10 21.466 1628.14 441.4 0.2971 1.33243 +FS_5 LPT.Fl_O 62.56 4.685 1140.69 279.58 0.0146 291.00 4.286 1113.95 1477.4 0.3636 1.36191 +FS_7 Duct4.Fl_O 62.56 4.638 1140.69 279.58 0.0146 293.94 4.432 1127.00 2018.9 0.2589 1.36191 +FS_9 Core_Nozz.Fl_O 62.56 4.638 1140.69 279.58 0.0146 293.94 2.472 962.93 862.9 1.0000 1.36191 +FS_15 BypBld.Fl_O 339.67 5.313 499.41 119.34 0.0000 921.88 4.581 478.66 3795.6 0.4649 1.40083 +FS_17 Duct5.Fl_O 339.67 5.273 499.41 119.34 0.0000 928.85 4.547 478.66 3824.3 0.4649 1.40083 +FS_19 Byp_Nozz.Fl_O 339.67 5.273 499.41 119.34 0.0000 928.85 2.785 415.96 2706.4 1.0000 1.40083 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1585.30 1.561 0.9024 3613.219 1.1508 0.9083 -8895.0 31.70 18.33 +LPC 167.76 2.255 0.8632 3368.232 1.3029 0.8778 -3168.9 28.08 20.51 +HPC 85.11 5.504 0.8648 6313.835 1.7066 0.8922 -9854.0 22.08 22.15 +HPT 27.40 2.712 0.9144 153.083 1.2444 0.9042 9853.9 +LPT 72.10 4.857 0.9256 81.315 1.4483 0.9096 12064.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3039.63 1.391 0.9322 0.916 2.0965 0.5215 1.4369 0.9679 3943.9586 +LPC 179.95 1.385 0.8991 0.920 1.7169 0.9323 3.2631 0.9600 3662.6571 +HPC 202.35 21.821 0.8531 0.993 2.0965 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 5.029 0.9328 99.981 5.0286 1.4085 0.4249 0.9803 1.5311 +LPT 149.81 6.381 0.9244 100.251 6.3811 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4881.74 9060.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 813.88 195.20 19.792 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 813.88 195.20 19.792 +Duct1 0.0025 0.4393 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 813.88 195.20 19.792 +Duct2 0.0025 0.4383 365.99 +Duct3 0.0050 0.2971 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.1580 1110.42 268.62 65.630 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.3912 1110.42 268.62 65.630 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 499.41 119.34 5.313 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5090 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7071.7 7318.4 9853.9 +LP_Shaft 3305.1 19170.8 12064.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2134.01 0.9940 0.0550 0.89741 0.01599 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.240 0.9972 1.0000 0.9975 2706.36 1.000 997.7 11696.8 +Core_Nozz 1.970 0.9999 1.0000 0.9999 862.88 1.000 1506.4 3029.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 403 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 43000.0 0.00 374.77 4249.6 0.5752 2444.26 5.9839 726.36 15.977 1959.0 1911.2 1510.0 + core size:20.55 Q: 133.63 Maximum Thrust: 7082.6 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 374.77 3.420 433.98 103.67 0.0000 1472.98 2.355 389.97 4558.7 0.7500 1.40134 +FS_2 Inlet.Fl_O 374.77 3.403 433.98 103.67 0.0000 1480.40 2.904 414.73 5943.4 0.4810 1.40134 +FS_21 Fan.Fl_O 374.77 4.968 488.50 116.72 0.0000 1076.00 4.314 469.16 4515.2 0.4534 1.40098 +FS_13 Splitter.Fl_O2 321.11 4.968 488.50 116.72 0.0000 921.93 4.283 468.20 3795.6 0.4650 1.40098 +FS_22 Splitter.Fl_O1 53.66 4.968 488.50 116.72 0.0000 154.07 4.458 473.60 719.5 0.3961 1.40098 +FS_23 Duct1.Fl_O 53.66 4.955 488.50 116.72 0.0000 154.46 4.447 473.60 721.3 0.3961 1.40098 +FS_24 LPC.Fl_O 53.66 10.547 626.18 149.77 0.0000 82.16 9.340 604.87 366.0 0.4203 1.39852 +FS_25 Duct2.Fl_O 53.66 10.520 626.18 149.77 0.0000 82.37 9.317 604.87 366.9 0.4203 1.39852 +FS_3 HPC.Fl_O 53.66 54.644 1051.35 253.79 0.0000 20.55 51.214 1032.82 119.9 0.3080 1.37750 +FS_36 Bld3.Fl_O 48.83 54.644 1051.35 253.79 0.0000 18.70 51.214 1032.82 109.1 0.3080 1.37750 +FS_4 Burner.Fl_O 49.51 51.639 1959.01 501.19 0.0139 27.38 51.307 1955.94 483.4 0.0990 1.31973 +FS_45 HPT.Fl_O 54.34 18.926 1510.04 376.48 0.0127 72.00 17.844 1487.58 439.1 0.2973 1.34088 +FS_48 Duct3.Fl_O 54.34 18.832 1510.04 376.48 0.0127 72.36 17.755 1487.58 441.4 0.2973 1.34088 +FS_5 LPT.Fl_O 54.34 3.931 1041.67 253.84 0.0127 287.89 3.604 1017.51 1477.4 0.3580 1.36953 +FS_7 Duct4.Fl_O 54.34 3.892 1041.67 253.84 0.0127 290.80 3.723 1029.27 2018.9 0.2551 1.36953 +FS_9 Core_Nozz.Fl_O 54.34 3.892 1041.67 253.84 0.0127 290.80 2.355 908.49 862.9 0.8842 1.36953 +FS_15 BypBld.Fl_O 321.11 4.968 488.50 116.72 0.0000 921.93 4.283 468.20 3795.6 0.4650 1.40098 +FS_17 Duct5.Fl_O 321.11 4.930 488.50 116.72 0.0000 928.90 4.251 468.20 3824.3 0.4650 1.40098 +FS_19 Byp_Nozz.Fl_O 321.11 4.930 488.50 116.72 0.0000 928.90 2.603 406.87 2706.4 1.0000 1.40098 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1480.40 1.460 0.9104 3366.098 1.1256 0.9151 -6920.7 39.52 19.74 +LPC 154.46 2.128 0.8547 3172.713 1.2818 0.8692 -2509.1 25.36 16.72 +HPC 82.37 5.194 0.8658 6255.155 1.6790 0.8923 -7897.7 26.22 26.37 +HPT 27.38 2.728 0.9148 155.284 1.2516 0.9045 7897.8 +LPT 72.36 4.790 0.9208 79.236 1.4496 0.9039 9429.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2838.38 1.320 0.9406 0.853 2.0411 0.5215 1.4369 0.9679 3943.9586 +LPC 165.67 1.346 0.8903 0.866 1.6263 0.9323 3.2631 0.9600 3662.6571 +HPC 195.81 20.389 0.8541 0.984 2.1344 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.068 0.9332 101.418 5.0680 1.4085 0.4249 0.9803 1.5311 +LPT 150.35 6.287 0.9196 97.689 6.2873 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4558.69 8460.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 776.82 186.18 16.985 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 776.82 186.18 16.985 +Duct1 0.0025 0.3961 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 776.82 186.18 16.985 +Duct2 0.0025 0.4203 365.99 +Duct3 0.0050 0.2973 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3580 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.8782 1051.35 253.79 54.644 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.9514 1051.35 253.79 54.644 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 488.50 116.72 4.968 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9839 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6873.0 6035.3 7897.8 +LP_Shaft 3079.1 16084.5 9429.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1959.01 0.9940 0.0550 0.67896 0.01390 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.094 0.9975 1.0000 0.9975 2706.36 1.000 986.8 10521.6 +Core_Nozz 1.653 0.9999 1.0000 0.9999 862.88 0.884 1296.0 2188.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 404 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 43000.0 0.00 343.75 2833.1 0.6068 1719.03 6.6965 726.36 12.606 1765.4 1723.7 1353.4 + core size:20.93 Q: 133.63 Maximum Thrust: 7082.6 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 343.75 3.420 433.98 103.67 0.0000 1351.06 2.355 389.97 4181.4 0.7500 1.40134 +FS_2 Inlet.Fl_O 343.75 3.403 433.98 103.67 0.0000 1357.87 2.998 418.50 5943.4 0.4294 1.40134 +FS_21 Fan.Fl_O 343.75 4.566 475.89 113.70 0.0000 1059.67 3.987 457.75 4515.2 0.4444 1.40114 +FS_13 Splitter.Fl_O2 299.09 4.566 475.89 113.70 0.0000 921.99 3.937 456.10 3795.6 0.4650 1.40114 +FS_22 Splitter.Fl_O1 44.66 4.566 475.89 113.70 0.0000 137.68 4.202 464.70 719.5 0.3464 1.40114 +FS_23 Duct1.Fl_O 44.66 4.555 475.89 113.70 0.0000 138.03 4.192 464.70 721.3 0.3464 1.40114 +FS_24 LPC.Fl_O 44.66 8.861 593.97 142.03 0.0000 79.27 7.928 575.41 366.0 0.4019 1.39913 +FS_25 Duct2.Fl_O 44.66 8.839 593.97 142.03 0.0000 79.47 7.909 575.41 366.9 0.4019 1.39913 +FS_3 HPC.Fl_O 44.66 43.115 980.72 236.20 0.0000 20.93 40.298 962.56 119.9 0.3140 1.38191 +FS_36 Bld3.Fl_O 40.64 43.115 980.72 236.20 0.0000 19.05 40.298 962.56 109.1 0.3140 1.38191 +FS_4 Burner.Fl_O 41.12 40.743 1765.42 445.90 0.0117 27.36 40.481 1762.60 483.4 0.0985 1.32911 +FS_45 HPT.Fl_O 45.14 14.798 1353.40 334.05 0.0107 72.42 13.942 1332.57 439.1 0.2980 1.35112 +FS_48 Duct3.Fl_O 45.14 14.724 1353.40 334.05 0.0107 72.78 13.872 1332.57 441.4 0.2980 1.35112 +FS_5 LPT.Fl_O 45.14 3.333 947.10 229.64 0.0107 268.94 3.095 928.03 1477.4 0.3299 1.37686 +FS_7 Duct4.Fl_O 45.14 3.300 947.10 229.64 0.0107 271.66 3.176 937.22 2018.9 0.2365 1.37686 +FS_9 Core_Nozz.Fl_O 45.14 3.300 947.10 229.64 0.0107 271.66 2.355 863.22 862.9 0.7150 1.37686 +FS_15 BypBld.Fl_O 299.09 4.566 475.89 113.70 0.0000 921.99 3.937 456.10 3795.6 0.4650 1.40114 +FS_17 Duct5.Fl_O 299.09 4.532 475.89 113.70 0.0000 928.96 3.908 456.10 3824.3 0.4650 1.40114 +FS_19 Byp_Nozz.Fl_O 299.09 4.532 475.89 113.70 0.0000 928.96 2.393 396.36 2706.3 1.0000 1.40114 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1357.87 1.342 0.9097 3039.887 1.0966 0.9134 -4878.6 47.39 21.54 +LPC 138.03 1.945 0.8445 2902.968 1.2481 0.8584 -1789.8 23.28 13.31 +HPC 79.47 4.878 0.8648 6205.168 1.6511 0.8907 -5951.0 30.89 31.12 +HPT 27.36 2.753 0.9154 158.040 1.2605 0.9046 5951.0 +LPT 72.78 4.417 0.9165 75.585 1.4290 0.8993 6668.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2603.52 1.238 0.9398 0.771 2.0807 0.5215 1.4369 0.9679 3943.9586 +LPC 148.05 1.290 0.8797 0.793 1.5534 0.9323 3.2631 0.9600 3662.6571 +HPC 188.92 18.926 0.8531 0.976 2.1667 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.127 0.9337 103.219 5.1266 1.4085 0.4249 0.9803 1.5311 +LPT 151.23 5.767 0.9153 93.187 5.7670 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4181.37 7760.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 730.67 174.99 13.861 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 730.67 174.99 13.861 +Duct1 0.0025 0.3464 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 730.67 174.99 13.861 +Duct2 0.0025 0.4019 365.99 +Duct3 0.0050 0.2980 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3299 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.5632 980.72 236.20 43.115 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.4565 980.72 236.20 43.115 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 475.89 113.70 4.566 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6965 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6640.3 4706.9 5951.0 +LP_Shaft 2780.7 12595.5 6668.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1765.42 0.9940 0.0550 0.47751 0.01175 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.925 0.9975 1.0000 0.9975 2706.36 1.000 973.9 9158.5 +Core_Nozz 1.401 0.9999 1.0000 0.9999 862.88 0.715 1023.0 1435.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 405 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 43000.0 0.00 305.94 1416.6 0.7270 1029.86 7.8825 726.36 8.993 1515.5 1481.7 1153.3 + core size:21.52 Q: 133.63 Maximum Thrust: 7082.6 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 305.94 3.420 433.98 103.67 0.0000 1202.44 2.355 389.97 3721.4 0.7500 1.40134 +FS_2 Inlet.Fl_O 305.94 3.403 433.98 103.67 0.0000 1208.49 3.093 422.25 5943.4 0.3721 1.40134 +FS_21 Fan.Fl_O 305.94 4.102 460.84 110.10 0.0000 1033.18 3.611 444.33 4515.2 0.4302 1.40127 +FS_13 Splitter.Fl_O2 271.50 4.102 460.84 110.10 0.0000 916.86 3.544 441.95 3795.6 0.4615 1.40127 +FS_22 Splitter.Fl_O1 34.44 4.102 460.84 110.10 0.0000 116.32 3.875 453.39 719.5 0.2861 1.40127 +FS_23 Duct1.Fl_O 34.44 4.092 460.84 110.10 0.0000 116.61 3.865 453.39 721.3 0.2861 1.40127 +FS_24 LPC.Fl_O 34.44 6.944 551.33 131.79 0.0000 75.15 6.296 536.12 366.0 0.3766 1.39988 +FS_25 Duct2.Fl_O 34.44 6.927 551.33 131.79 0.0000 75.34 6.281 536.12 366.9 0.3766 1.39988 +FS_3 HPC.Fl_O 34.44 30.759 887.19 213.13 0.0000 21.52 28.625 869.54 119.9 0.3234 1.38760 +FS_36 Bld3.Fl_O 31.34 30.759 887.19 213.13 0.0000 19.59 28.625 869.54 109.1 0.3234 1.38760 +FS_4 Burner.Fl_O 31.63 29.067 1515.53 376.67 0.0091 27.33 28.881 1513.04 483.4 0.0979 1.34301 +FS_45 HPT.Fl_O 34.73 10.434 1153.32 281.40 0.0083 72.94 9.822 1134.78 439.1 0.2988 1.36528 +FS_48 Duct3.Fl_O 34.73 10.382 1153.32 281.40 0.0083 73.31 9.772 1134.78 441.4 0.2988 1.36528 +FS_5 LPT.Fl_O 34.73 2.872 842.42 203.27 0.0083 226.48 2.730 830.63 1477.4 0.2715 1.38460 +FS_7 Duct4.Fl_O 34.73 2.843 842.42 203.27 0.0083 228.77 2.768 836.20 2018.9 0.1966 1.38460 +FS_9 Core_Nozz.Fl_O 34.73 2.843 842.42 203.27 0.0083 228.77 2.355 799.34 862.8 0.5285 1.38460 +FS_15 BypBld.Fl_O 271.50 4.102 460.84 110.10 0.0000 916.86 3.544 441.95 3795.6 0.4615 1.40127 +FS_17 Duct5.Fl_O 271.50 4.071 460.84 110.10 0.0000 923.79 3.518 441.95 3824.3 0.4615 1.40127 +FS_19 Byp_Nozz.Fl_O 271.50 4.071 460.84 110.10 0.0000 923.79 2.355 393.95 2706.3 0.9199 1.40127 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1208.49 1.205 0.8878 2589.495 1.0619 0.8907 -2782.3 57.77 23.91 +LPC 116.61 1.697 0.8320 2512.918 1.1964 0.8441 -1056.8 23.64 10.01 +HPC 75.34 4.441 0.8629 6127.394 1.6092 0.8878 -3963.9 38.15 38.70 +HPT 27.33 2.786 0.9163 162.276 1.2734 0.9051 3964.0 +LPT 73.31 3.615 0.9109 69.748 1.3691 0.8951 3839.0 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2317.11 1.143 0.9172 0.657 2.2588 0.5215 1.4369 0.9679 3943.9586 +LPC 125.08 1.214 0.8667 0.686 1.5161 0.9323 3.2631 0.9600 3662.6571 +HPC 179.11 16.905 0.8512 0.964 2.2435 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.203 0.9347 105.985 5.2030 1.4085 0.4249 0.9803 1.5311 +LPT 152.32 4.648 0.9097 85.990 4.6478 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3721.39 6906.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 669.72 160.26 10.418 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 669.72 160.26 10.418 +Duct1 0.0025 0.2861 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 669.72 160.26 10.418 +Duct2 0.0025 0.3766 365.99 +Duct3 0.0050 0.2988 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2715 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.2055 887.19 213.13 30.759 +Duct5 0.0075 0.4615 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 1.8943 887.19 213.13 30.759 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 460.84 110.10 4.102 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8825 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6317.4 3295.6 3964.0 +LP_Shaft 2368.7 8512.3 3839.0 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1515.53 0.9940 0.0550 0.28607 0.00913 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.729 0.9975 1.0000 0.9975 2706.36 0.920 893.2 7536.8 +Core_Nozz 1.207 0.9999 1.0000 0.9999 862.88 0.528 728.8 786.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 406 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 11/ 21/ 1/ 9 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.750 43000.0 0.00 267.92 354.1 1.4705 520.74 9.6951 726.36 5.897 1234.1 1209.4 932.3 + core size:22.42 Q: 133.63 Maximum Thrust: 7082.6 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 267.92 3.420 433.98 103.67 0.0000 1053.00 2.355 389.97 3258.9 0.7500 1.40134 +FS_2 Inlet.Fl_O 267.92 3.403 433.98 103.67 0.0000 1058.31 3.171 425.31 5943.4 0.3189 1.40134 +FS_21 Fan.Fl_O 267.92 3.701 447.43 106.89 0.0000 988.05 3.302 433.05 4515.2 0.4068 1.40133 +FS_13 Splitter.Fl_O2 242.87 3.701 447.43 106.89 0.0000 895.67 3.225 430.14 3795.6 0.4476 1.40133 +FS_22 Splitter.Fl_O1 25.05 3.701 447.43 106.89 0.0000 92.38 3.575 443.01 719.5 0.2230 1.40133 +FS_23 Duct1.Fl_O 25.05 3.692 447.43 106.89 0.0000 92.61 3.566 443.01 721.3 0.2230 1.40133 +FS_24 LPC.Fl_O 25.05 5.256 505.53 120.80 0.0000 69.15 4.848 493.99 366.0 0.3414 1.40074 +FS_25 Duct2.Fl_O 25.05 5.243 505.53 120.80 0.0000 69.32 4.836 493.99 366.9 0.3414 1.40074 +FS_3 HPC.Fl_O 25.05 20.168 782.36 187.52 0.0000 22.42 18.640 765.14 119.9 0.3382 1.39280 +FS_36 Bld3.Fl_O 22.80 20.168 782.36 187.52 0.0000 20.40 18.640 765.14 109.1 0.3382 1.39280 +FS_4 Burner.Fl_O 22.94 19.059 1234.13 301.70 0.0063 27.29 18.937 1232.03 483.4 0.0971 1.36151 +FS_45 HPT.Fl_O 25.20 6.766 932.28 225.15 0.0058 73.37 6.364 916.64 439.1 0.2990 1.38101 +FS_48 Duct3.Fl_O 25.20 6.732 932.28 225.15 0.0058 73.74 6.332 916.64 441.4 0.2990 1.38101 +FS_5 LPT.Fl_O 25.20 2.604 736.86 177.09 0.0058 169.50 2.533 731.21 1477.4 0.1987 1.39126 +FS_7 Duct4.Fl_O 25.20 2.578 736.86 177.09 0.0058 171.22 2.540 733.83 2018.9 0.1453 1.39126 +FS_9 Core_Nozz.Fl_O 25.20 2.578 736.86 177.09 0.0058 171.22 2.355 718.35 862.8 0.3628 1.39126 +FS_15 BypBld.Fl_O 242.87 3.701 447.43 106.89 0.0000 895.67 3.225 430.14 3795.6 0.4476 1.40133 +FS_17 Duct5.Fl_O 242.87 3.673 447.43 106.89 0.0000 902.43 3.201 430.14 3824.3 0.4476 1.40133 +FS_19 Byp_Nozz.Fl_O 242.87 3.673 447.43 106.89 0.0000 902.43 2.355 393.92 2706.4 0.8228 1.40133 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1058.31 1.088 0.7852 2037.363 1.0310 0.7878 -1220.0 82.22 25.26 +LPC 92.61 1.424 0.8194 2006.515 1.1298 0.8282 -493.1 28.71 8.25 +HPC 69.32 3.847 0.8535 6017.366 1.5476 0.8781 -2364.7 49.87 50.87 +HPT 27.29 2.817 0.9179 169.104 1.2890 0.9064 2364.7 +LPT 73.74 2.586 0.9011 61.036 1.2652 0.8885 1713.1 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2029.16 1.061 0.8112 0.517 2.6314 0.5215 1.4369 0.9679 3943.9586 +LPC 99.34 1.130 0.8535 0.548 1.5624 0.9323 3.2631 0.9600 3662.6571 +HPC 164.81 14.161 0.8420 0.947 2.3811 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.276 0.9363 110.445 5.2762 1.4085 0.4249 0.9803 1.5311 +LPT 153.22 3.212 0.9000 75.250 3.2120 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3258.92 6048.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 602.83 144.15 7.429 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 602.83 144.15 7.429 +Duct1 0.0025 0.2230 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 602.83 144.15 7.429 +Duct2 0.0025 0.3414 365.99 +Duct3 0.0050 0.2990 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.1987 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 0.8768 782.36 187.52 20.168 +Duct5 0.0075 0.4476 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 1.3778 782.36 187.52 20.168 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 447.43 106.89 3.701 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.6951 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 5940.6 2090.7 2364.7 +LP_Shaft 1863.6 4827.9 1713.1 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1234.13 0.9940 0.0550 0.14465 0.00635 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.560 0.9975 1.0000 0.9975 2706.36 0.823 798.9 6030.6 +Core_Nozz 1.095 0.9999 1.0000 0.9999 862.88 0.363 475.2 372.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 407 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 43000.0 0.00 442.05 7261.9 0.6041 4387.22 5.0397 774.79 22.730 2333.7 2274.2 1819.0 + core size:19.95 Q: 152.04 Maximum Thrust: 7261.9 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 442.05 3.590 440.05 105.12 0.0000 1666.72 2.355 389.97 5040.9 0.8000 1.40134 +FS_2 Inlet.Fl_O 442.05 3.572 440.05 105.12 0.0000 1675.11 2.852 412.55 5943.4 0.5763 1.40134 +FS_21 Fan.Fl_O 442.05 5.875 517.67 123.71 0.0000 1104.76 5.050 495.76 4515.2 0.4696 1.40053 +FS_13 Splitter.Fl_O2 368.85 5.875 517.67 123.71 0.0000 921.84 5.065 496.18 3795.6 0.4650 1.40053 +FS_22 Splitter.Fl_O1 73.19 5.875 517.67 123.71 0.0000 182.92 4.969 493.47 719.5 0.4947 1.40053 +FS_23 Duct1.Fl_O 73.19 5.860 517.67 123.71 0.0000 183.38 4.957 493.47 721.3 0.4947 1.40053 +FS_24 LPC.Fl_O 73.19 14.576 694.57 166.26 0.0000 85.39 12.751 668.67 366.0 0.4418 1.39620 +FS_25 Duct2.Fl_O 73.19 14.540 694.57 166.26 0.0000 85.61 12.719 668.67 366.9 0.4418 1.39620 +FS_3 HPC.Fl_O 73.19 81.604 1188.59 288.41 0.0000 19.95 76.793 1169.26 119.9 0.2990 1.36886 +FS_36 Bld3.Fl_O 66.60 81.604 1188.59 288.41 0.0000 18.16 76.793 1169.26 109.1 0.2990 1.36886 +FS_4 Burner.Fl_O 67.82 77.116 2333.66 611.97 0.0183 27.42 76.618 2330.12 483.4 0.0996 1.30529 +FS_45 HPT.Fl_O 74.41 28.873 1818.96 463.17 0.0167 70.93 27.273 1793.76 439.1 0.2944 1.32343 +FS_48 Duct3.Fl_O 74.41 28.728 1818.96 463.17 0.0167 71.28 27.136 1793.76 441.4 0.2944 1.32343 +FS_5 LPT.Fl_O 74.41 5.872 1258.99 310.89 0.0167 290.13 5.375 1230.19 1477.4 0.3636 1.35297 +FS_7 Duct4.Fl_O 74.41 5.813 1258.99 310.89 0.0167 293.06 5.557 1244.24 2018.9 0.2589 1.35297 +FS_9 Core_Nozz.Fl_O 74.41 5.813 1258.99 310.89 0.0167 293.06 3.103 1066.59 862.9 1.0000 1.35297 +FS_15 BypBld.Fl_O 368.85 5.875 517.67 123.71 0.0000 921.84 5.065 496.18 3795.6 0.4650 1.40053 +FS_17 Duct5.Fl_O 368.85 5.831 517.67 123.71 0.0000 928.81 5.027 496.18 3824.3 0.4650 1.40053 +FS_19 Byp_Nozz.Fl_O 368.85 5.831 517.67 123.71 0.0000 928.81 3.079 431.18 2706.3 1.0000 1.40053 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.645 0.8675 3944.235 1.1764 0.8766 -11626.2 24.71 17.45 +LPC 183.38 2.487 0.8684 3636.521 1.3417 0.8840 -4405.4 28.42 23.33 +HPC 85.61 5.612 0.8651 6326.949 1.7112 0.8923 -12649.4 20.06 20.11 +HPT 27.42 2.671 0.9133 151.562 1.2349 0.9034 12649.5 +LPT 71.28 4.892 0.9322 85.184 1.4448 0.9176 16031.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8963 1.000 2.3706 0.5215 1.4369 0.9679 3943.9586 +LPC 196.69 1.456 0.9045 0.993 1.7675 0.9323 3.2631 0.9600 3662.6571 +HPC 203.51 22.322 0.8534 0.995 2.0423 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.933 0.9316 98.988 4.9326 1.4085 0.4249 0.9803 1.5311 +LPT 148.11 6.430 0.9310 105.021 6.4296 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 5040.92 10644.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 870.40 209.01 24.365 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 870.40 209.01 24.365 +Duct1 0.0025 0.4947 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 870.40 209.01 24.365 +Duct2 0.0025 0.4418 365.99 +Duct3 0.0050 0.2944 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.5617 1188.59 288.41 81.604 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.0255 1188.59 288.41 81.604 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 517.67 123.71 5.875 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0397 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7321.6 9074.0 12649.5 +LP_Shaft 3633.0 23176.4 16031.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2333.66 0.9940 0.0550 1.21867 0.01830 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.476 0.9962 1.0000 0.9975 2706.36 1.000 1015.9 13605.0 +Core_Nozz 2.469 0.9979 1.0000 0.9999 862.88 1.000 1580.8 4301.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 408 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 43000.0 0.00 430.95 6535.3 0.5939 3881.30 5.3025 774.79 20.832 2249.1 2192.1 1746.6 + core size:20.05 Q: 152.04 Maximum Thrust: 7261.9 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 430.95 3.590 440.05 105.12 0.0000 1624.90 2.355 389.97 4914.4 0.8000 1.40134 +FS_2 Inlet.Fl_O 430.95 3.572 440.05 105.12 0.0000 1633.08 2.900 414.53 5943.4 0.5539 1.40134 +FS_21 Fan.Fl_O 430.95 5.742 511.79 122.30 0.0000 1095.73 4.952 490.58 4515.2 0.4645 1.40063 +FS_13 Splitter.Fl_O2 362.58 5.742 511.79 122.30 0.0000 921.87 4.950 490.53 3795.6 0.4650 1.40063 +FS_22 Splitter.Fl_O1 68.38 5.742 511.79 122.30 0.0000 173.86 4.960 490.81 719.5 0.4618 1.40063 +FS_23 Duct1.Fl_O 68.38 5.727 511.79 122.30 0.0000 174.29 4.948 490.81 721.3 0.4618 1.40063 +FS_24 LPC.Fl_O 68.38 13.340 673.03 161.05 0.0000 85.81 11.650 647.59 366.0 0.4445 1.39696 +FS_25 Duct2.Fl_O 68.38 13.307 673.03 161.05 0.0000 86.02 11.621 647.59 366.9 0.4445 1.39696 +FS_3 HPC.Fl_O 68.38 74.788 1154.51 279.76 0.0000 20.05 70.335 1135.47 119.9 0.3003 1.37101 +FS_36 Bld3.Fl_O 62.22 74.788 1154.51 279.76 0.0000 18.24 70.335 1135.47 109.1 0.3003 1.37101 +FS_4 Burner.Fl_O 63.30 70.675 2249.09 586.59 0.0173 27.41 70.219 2245.67 483.4 0.0995 1.30824 +FS_45 HPT.Fl_O 69.46 26.199 1746.58 442.54 0.0158 71.49 24.723 1721.75 439.1 0.2966 1.32720 +FS_48 Duct3.Fl_O 69.46 26.068 1746.58 442.54 0.0158 71.85 24.599 1721.75 441.4 0.2966 1.32720 +FS_5 LPT.Fl_O 69.46 5.366 1209.85 297.80 0.0158 290.51 4.910 1181.88 1477.4 0.3636 1.35668 +FS_7 Duct4.Fl_O 69.46 5.312 1209.85 297.80 0.0158 293.45 5.078 1195.53 2018.9 0.2589 1.35668 +FS_9 Core_Nozz.Fl_O 69.46 5.312 1209.85 297.80 0.0158 293.45 2.834 1023.43 862.9 1.0000 1.35668 +FS_15 BypBld.Fl_O 362.58 5.742 511.79 122.30 0.0000 921.87 4.950 490.53 3795.6 0.4650 1.40063 +FS_17 Duct5.Fl_O 362.58 5.698 511.79 122.30 0.0000 928.84 4.913 490.53 3824.3 0.4650 1.40063 +FS_19 Byp_Nozz.Fl_O 362.58 5.698 511.79 122.30 0.0000 928.84 3.009 426.27 2706.4 1.0000 1.40063 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1633.08 1.607 0.8925 3742.521 1.1630 0.8995 -10474.8 28.21 17.74 +LPC 174.29 2.329 0.8661 3470.317 1.3150 0.8810 -3748.9 28.95 22.22 +HPC 86.02 5.620 0.8639 6337.462 1.7154 0.8916 -11484.0 20.47 20.49 +HPT 27.41 2.698 0.9138 152.224 1.2399 0.9037 11484.1 +LPT 71.85 4.858 0.9277 82.485 1.4436 0.9122 14223.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3130.99 1.423 0.9220 0.949 2.1753 0.5215 1.4369 0.9679 3943.9586 +LPC 186.95 1.407 0.9021 0.947 1.7535 0.9323 3.2631 0.9600 3662.6571 +HPC 204.50 22.358 0.8523 0.997 2.0718 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.995 0.9321 99.420 4.9955 1.4085 0.4249 0.9803 1.5311 +LPT 149.30 6.382 0.9265 101.694 6.3817 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4914.43 10377.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 844.21 202.60 22.314 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 844.21 202.60 22.314 +Duct1 0.0025 0.4618 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 844.21 202.60 22.314 +Duct2 0.0025 0.4445 365.99 +Duct3 0.0050 0.2966 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.3932 1154.51 279.76 74.788 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.7608 1154.51 279.76 74.788 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 511.79 122.30 5.742 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3025 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7219.1 8355.0 11484.1 +LP_Shaft 3447.2 21670.7 14223.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2249.09 0.9940 0.0550 1.07814 0.01733 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.420 0.9965 1.0000 0.9975 2706.36 1.000 1010.1 13152.7 +Core_Nozz 2.256 0.9992 1.0000 0.9999 862.88 1.000 1550.4 3760.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 409 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 43000.0 0.00 418.41 5809.5 0.5895 3424.90 5.5080 774.79 19.193 2162.4 2108.2 1675.1 + core size:20.20 Q: 152.04 Maximum Thrust: 7261.9 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 418.41 3.590 440.05 105.12 0.0000 1577.61 2.355 389.97 4771.4 0.8000 1.40134 +FS_2 Inlet.Fl_O 418.41 3.572 440.05 105.12 0.0000 1585.56 2.950 416.58 5943.4 0.5299 1.40134 +FS_21 Fan.Fl_O 418.41 5.578 506.42 121.02 0.0000 1089.22 4.822 485.74 4515.2 0.4608 1.40072 +FS_13 Splitter.Fl_O2 354.12 5.578 506.42 121.02 0.0000 921.86 4.810 485.38 3795.6 0.4649 1.40072 +FS_22 Splitter.Fl_O1 64.29 5.578 506.42 121.02 0.0000 167.37 4.885 487.55 719.5 0.4394 1.40072 +FS_23 Duct1.Fl_O 64.29 5.564 506.42 121.02 0.0000 167.79 4.873 487.55 721.3 0.4394 1.40072 +FS_24 LPC.Fl_O 64.29 12.552 659.77 157.86 0.0000 84.90 11.002 635.47 366.0 0.4383 1.39746 +FS_25 Duct2.Fl_O 64.29 12.521 659.77 157.86 0.0000 85.11 10.974 635.47 366.9 0.4383 1.39746 +FS_3 HPC.Fl_O 64.29 68.906 1125.27 272.36 0.0000 20.20 64.737 1106.34 119.9 0.3027 1.37285 +FS_36 Bld3.Fl_O 58.51 68.906 1125.27 272.36 0.0000 18.38 64.737 1106.34 109.1 0.3027 1.37285 +FS_4 Burner.Fl_O 59.46 65.116 2162.37 560.74 0.0163 27.40 64.697 2159.05 483.4 0.0993 1.31135 +FS_45 HPT.Fl_O 65.24 24.021 1675.12 422.33 0.0148 71.73 22.658 1650.92 439.1 0.2972 1.33116 +FS_48 Duct3.Fl_O 65.24 23.901 1675.12 422.33 0.0148 72.09 22.545 1650.92 441.4 0.2972 1.33116 +FS_5 LPT.Fl_O 65.24 4.925 1158.01 284.11 0.0148 290.90 4.506 1130.96 1477.4 0.3636 1.36063 +FS_7 Duct4.Fl_O 65.24 4.876 1158.01 284.11 0.0148 293.83 4.660 1144.16 2018.9 0.2589 1.36063 +FS_9 Core_Nozz.Fl_O 65.24 4.876 1158.01 284.11 0.0148 293.83 2.599 978.04 862.9 1.0000 1.36063 +FS_15 BypBld.Fl_O 354.12 5.578 506.42 121.02 0.0000 921.86 4.810 485.38 3795.6 0.4649 1.40072 +FS_17 Duct5.Fl_O 354.12 5.536 506.42 121.02 0.0000 928.82 4.773 485.38 3824.3 0.4649 1.40072 +FS_19 Byp_Nozz.Fl_O 354.12 5.536 506.42 121.02 0.0000 928.82 2.923 421.79 2706.4 1.0000 1.40072 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1585.56 1.562 0.9023 3613.838 1.1508 0.9083 -9407.7 31.67 18.33 +LPC 167.79 2.256 0.8632 3368.727 1.3028 0.8778 -3351.4 28.08 20.51 +HPC 85.11 5.503 0.8648 6313.705 1.7055 0.8922 -10415.9 22.09 22.16 +HPT 27.40 2.711 0.9145 153.134 1.2436 0.9042 10415.8 +LPT 72.09 4.853 0.9256 81.330 1.4466 0.9098 12759.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3040.11 1.391 0.9322 0.916 2.0967 0.5215 1.4369 0.9679 3943.9586 +LPC 179.97 1.385 0.8991 0.920 1.7168 0.9323 3.2631 0.9600 3662.6571 +HPC 202.34 21.818 0.8531 0.993 2.0967 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 5.026 0.9328 100.014 5.0265 1.4085 0.4249 0.9803 1.5311 +LPT 149.80 6.375 0.9244 100.270 6.3748 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4771.43 10075.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 825.11 197.94 20.781 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 825.11 197.94 20.781 +Duct1 0.0025 0.4394 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 825.11 197.94 20.781 +Duct2 0.0025 0.4383 365.99 +Duct3 0.0050 0.2972 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.2502 1125.27 272.36 68.906 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.5361 1125.27 272.36 68.906 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 506.42 121.02 5.578 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5080 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7120.9 7682.3 10415.8 +LP_Shaft 3328.7 20131.8 12759.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2162.37 0.9940 0.0550 0.95136 0.01626 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.351 0.9968 1.0000 0.9975 2706.36 1.000 1004.7 12597.1 +Core_Nozz 2.071 0.9998 1.0000 0.9999 862.88 1.000 1517.6 3288.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 410 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 43000.0 0.00 391.17 4357.1 0.5946 2590.64 5.9821 774.79 15.997 1984.4 1936.0 1530.8 + core size:20.55 Q: 152.04 Maximum Thrust: 7261.9 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 391.17 3.590 440.05 105.12 0.0000 1474.89 2.355 389.97 4460.7 0.8000 1.40134 +FS_2 Inlet.Fl_O 391.17 3.572 440.05 105.12 0.0000 1482.31 3.047 420.46 5943.4 0.4818 1.40134 +FS_21 Fan.Fl_O 391.17 5.222 495.56 118.41 0.0000 1076.01 4.535 475.94 4515.2 0.4534 1.40089 +FS_13 Splitter.Fl_O2 335.14 5.222 495.56 118.41 0.0000 921.90 4.503 474.97 3795.6 0.4649 1.40089 +FS_22 Splitter.Fl_O1 56.02 5.222 495.56 118.41 0.0000 154.11 4.686 480.44 719.5 0.3962 1.40089 +FS_23 Duct1.Fl_O 56.02 5.209 495.56 118.41 0.0000 154.50 4.675 480.44 721.3 0.3962 1.40089 +FS_24 LPC.Fl_O 56.02 11.116 635.77 152.08 0.0000 82.00 9.850 614.24 366.0 0.4194 1.39826 +FS_25 Duct2.Fl_O 56.02 11.088 635.77 152.08 0.0000 82.21 9.825 614.24 366.9 0.4194 1.39826 +FS_3 HPC.Fl_O 56.02 57.431 1065.93 257.44 0.0000 20.55 53.825 1047.16 119.9 0.3082 1.37659 +FS_36 Bld3.Fl_O 50.98 57.431 1065.93 257.44 0.0000 18.70 53.825 1047.16 109.1 0.3082 1.37659 +FS_4 Burner.Fl_O 51.70 54.273 1984.39 508.50 0.0141 27.38 53.923 1981.29 483.4 0.0990 1.31865 +FS_45 HPT.Fl_O 56.74 19.902 1530.81 382.16 0.0128 71.98 18.765 1508.12 439.1 0.2974 1.33965 +FS_48 Duct3.Fl_O 56.74 19.803 1530.81 382.16 0.0128 72.34 18.671 1508.12 441.4 0.2974 1.33965 +FS_5 LPT.Fl_O 56.74 4.103 1055.18 257.31 0.0128 289.87 3.757 1030.36 1477.4 0.3610 1.36854 +FS_7 Duct4.Fl_O 56.74 4.062 1055.18 257.31 0.0128 292.80 3.884 1042.46 2018.9 0.2571 1.36854 +FS_9 Core_Nozz.Fl_O 56.74 4.062 1055.18 257.31 0.0128 292.80 2.355 909.74 862.9 0.9240 1.36854 +FS_15 BypBld.Fl_O 335.14 5.222 495.56 118.41 0.0000 921.90 4.503 474.97 3795.6 0.4649 1.40089 +FS_17 Duct5.Fl_O 335.14 5.183 495.56 118.41 0.0000 928.86 4.469 474.97 3824.3 0.4649 1.40089 +FS_19 Byp_Nozz.Fl_O 335.14 5.183 495.56 118.41 0.0000 928.86 2.737 412.75 2706.4 1.0000 1.40089 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1482.31 1.462 0.9104 3371.101 1.1261 0.9151 -7355.5 39.34 19.69 +LPC 154.50 2.134 0.8543 3176.690 1.2829 0.8689 -2668.3 25.15 16.59 +HPC 82.21 5.180 0.8658 6252.250 1.6766 0.8923 -8351.8 26.38 26.54 +HPT 27.38 2.727 0.9148 155.392 1.2506 0.9046 8351.9 +LPT 72.34 4.826 0.9207 79.363 1.4508 0.9037 10023.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2842.06 1.321 0.9406 0.855 2.0402 0.5215 1.4369 0.9679 3943.9586 +LPC 165.72 1.348 0.8899 0.867 1.6215 0.9323 3.2631 0.9600 3662.6571 +HPC 195.44 20.321 0.8542 0.983 2.1343 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.065 0.9332 101.489 5.0645 1.4085 0.4249 0.9803 1.5311 +LPT 150.32 6.337 0.9195 97.844 6.3373 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4460.74 9419.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 788.24 188.95 17.877 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 788.24 188.95 17.877 +Duct1 0.0025 0.3962 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 788.24 188.95 17.877 +Duct2 0.0025 0.4194 365.99 +Duct3 0.0050 0.2974 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3610 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.9609 1065.93 257.44 57.431 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.0814 1065.93 257.44 57.431 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 495.56 118.41 5.222 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9821 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6922.1 6336.9 8351.9 +LP_Shaft 3105.1 16954.5 10023.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1984.39 0.9940 0.0550 0.71962 0.01412 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.201 0.9973 1.0000 0.9975 2706.36 1.000 993.9 11386.9 +Core_Nozz 1.725 0.9999 1.0000 0.9999 862.88 0.924 1355.1 2390.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 411 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 7/ 17/ 1/ 5 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 43000.0 0.00 359.44 2904.8 0.6273 1822.30 6.6891 774.79 12.651 1787.7 1745.6 1371.7 + core size:20.95 Q: 152.04 Maximum Thrust: 7261.9 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 359.44 3.590 440.05 105.12 0.0000 1355.26 2.355 389.97 4098.9 0.8000 1.40134 +FS_2 Inlet.Fl_O 359.44 3.572 440.05 105.12 0.0000 1362.08 3.143 424.23 5943.4 0.4311 1.40134 +FS_21 Fan.Fl_O 359.44 4.810 483.05 115.42 0.0000 1059.79 4.199 464.63 4515.2 0.4445 1.40105 +FS_13 Splitter.Fl_O2 312.69 4.810 483.05 115.42 0.0000 921.96 4.147 462.97 3795.6 0.4650 1.40105 +FS_22 Splitter.Fl_O1 46.75 4.810 483.05 115.42 0.0000 137.83 4.426 471.67 719.5 0.3468 1.40105 +FS_23 Duct1.Fl_O 46.75 4.798 483.05 115.42 0.0000 138.18 4.415 471.67 721.3 0.3468 1.40105 +FS_24 LPC.Fl_O 46.75 9.389 604.16 144.48 0.0000 78.97 8.409 585.46 366.0 0.4001 1.39898 +FS_25 Duct2.Fl_O 46.75 9.366 604.16 144.48 0.0000 79.16 8.388 585.46 366.9 0.4001 1.39898 +FS_3 HPC.Fl_O 46.75 45.418 995.29 239.81 0.0000 20.95 42.445 976.85 119.9 0.3145 1.38101 +FS_36 Bld3.Fl_O 42.54 45.418 995.29 239.81 0.0000 19.07 42.445 976.85 109.1 0.3145 1.38101 +FS_4 Burner.Fl_O 43.05 42.920 1787.65 452.13 0.0119 27.36 42.644 1784.81 483.4 0.0986 1.32803 +FS_45 HPT.Fl_O 47.25 15.602 1371.65 338.91 0.0108 72.38 14.701 1350.62 439.1 0.2980 1.34993 +FS_48 Duct3.Fl_O 47.25 15.524 1371.65 338.91 0.0108 72.74 14.627 1350.62 441.4 0.2980 1.34993 +FS_5 LPT.Fl_O 47.25 3.438 955.87 231.86 0.0108 274.20 3.181 935.78 1477.4 0.3374 1.37621 +FS_7 Duct4.Fl_O 47.25 3.404 955.87 231.86 0.0108 276.97 3.270 945.48 2018.9 0.2415 1.37621 +FS_9 Core_Nozz.Fl_O 47.25 3.404 955.87 231.86 0.0108 276.97 2.355 863.88 862.9 0.7487 1.37621 +FS_15 BypBld.Fl_O 312.69 4.810 483.05 115.42 0.0000 921.96 4.147 462.97 3795.6 0.4650 1.40105 +FS_17 Duct5.Fl_O 312.69 4.774 483.05 115.42 0.0000 928.93 4.116 462.97 3824.3 0.4650 1.40105 +FS_19 Byp_Nozz.Fl_O 312.69 4.774 483.05 115.42 0.0000 928.93 2.521 402.32 2706.3 1.0000 1.40105 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1362.08 1.347 0.9101 3052.582 1.0977 0.9138 -5235.3 47.03 21.42 +LPC 138.18 1.957 0.8437 2913.545 1.2507 0.8577 -1921.8 22.77 13.08 +HPC 79.16 4.849 0.8647 6200.454 1.6474 0.8905 -6305.6 31.27 31.51 +HPT 27.36 2.751 0.9154 158.276 1.2596 0.9046 6305.6 +LPT 72.74 4.515 0.9158 75.919 1.4350 0.8982 7157.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2611.61 1.241 0.9402 0.774 2.0759 0.5215 1.4369 0.9679 3943.9586 +LPC 148.21 1.293 0.8789 0.795 1.5425 0.9323 3.2631 0.9600 3662.6571 +HPC 188.20 18.794 0.8531 0.975 2.1667 0.4206 0.2163 1.0137 6357.1603 +HPT 30.11 5.121 0.9338 103.373 5.1209 1.4085 0.4249 0.9803 1.5311 +LPT 151.15 5.904 0.9146 93.599 5.9039 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4098.92 8655.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 742.47 177.84 14.648 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 742.47 177.84 14.648 +Duct1 0.0025 0.3468 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 742.47 177.84 14.648 +Duct2 0.0025 0.4001 365.99 +Duct3 0.0050 0.2980 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3374 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.6361 995.29 239.81 45.418 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.5711 995.29 239.81 45.418 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 483.05 115.42 4.810 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6891 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6692.0 4948.9 6305.6 +LP_Shaft 2811.7 13369.3 7157.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1787.65 0.9940 0.0550 0.50619 0.01190 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.027 0.9976 1.0000 0.9975 2706.36 1.000 981.2 9986.7 +Core_Nozz 1.445 0.9999 1.0000 0.9999 862.88 0.749 1071.6 1573.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 412 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 43000.0 0.00 321.56 1452.4 0.7522 1092.46 7.8875 774.79 9.058 1534.6 1500.5 1168.9 + core size:21.56 Q: 152.04 Maximum Thrust: 7261.9 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 321.56 3.590 440.05 105.12 0.0000 1212.43 2.355 389.97 3666.9 0.8000 1.40134 +FS_2 Inlet.Fl_O 321.56 3.572 440.05 105.12 0.0000 1218.53 3.240 427.92 5943.4 0.3758 1.40134 +FS_21 Fan.Fl_O 321.56 4.324 467.92 111.80 0.0000 1037.93 3.802 450.98 4515.2 0.4327 1.40122 +FS_13 Splitter.Fl_O2 285.38 4.324 467.92 111.80 0.0000 921.15 3.730 448.51 3795.6 0.4644 1.40122 +FS_22 Splitter.Fl_O1 36.18 4.324 467.92 111.80 0.0000 116.78 4.083 460.29 719.5 0.2874 1.40122 +FS_23 Duct1.Fl_O 36.18 4.314 467.92 111.80 0.0000 117.08 4.073 460.29 721.3 0.2874 1.40122 +FS_24 LPC.Fl_O 36.18 7.405 562.10 134.37 0.0000 74.75 6.723 546.79 366.0 0.3742 1.39967 +FS_25 Duct2.Fl_O 36.18 7.387 562.10 134.37 0.0000 74.93 6.706 546.79 366.9 0.3742 1.39967 +FS_3 HPC.Fl_O 36.18 32.519 901.80 216.71 0.0000 21.56 30.255 883.81 119.9 0.3241 1.38674 +FS_36 Bld3.Fl_O 32.92 32.519 901.80 216.71 0.0000 19.62 30.255 883.81 109.1 0.3241 1.38674 +FS_4 Burner.Fl_O 33.23 30.731 1534.56 381.82 0.0092 27.33 30.534 1532.04 483.4 0.0979 1.34195 +FS_45 HPT.Fl_O 36.48 11.043 1168.93 285.42 0.0084 72.89 10.396 1150.20 439.1 0.2987 1.36423 +FS_48 Duct3.Fl_O 36.48 10.988 1168.93 285.42 0.0084 73.26 10.344 1150.20 441.4 0.2987 1.36423 +FS_5 LPT.Fl_O 36.48 2.926 846.25 204.23 0.0084 234.02 2.771 833.54 1477.4 0.2815 1.38435 +FS_7 Duct4.Fl_O 36.48 2.897 846.25 204.23 0.0084 236.39 2.816 839.56 2018.9 0.2035 1.38435 +FS_9 Core_Nozz.Fl_O 36.48 2.897 846.25 204.23 0.0084 236.39 2.355 798.80 862.9 0.5549 1.38435 +FS_15 BypBld.Fl_O 285.38 4.324 467.92 111.80 0.0000 921.15 3.730 448.51 3795.6 0.4644 1.40122 +FS_17 Duct5.Fl_O 285.38 4.292 467.92 111.80 0.0000 928.11 3.702 448.51 3824.3 0.4644 1.40122 +FS_19 Byp_Nozz.Fl_O 285.38 4.292 467.92 111.80 0.0000 928.11 2.355 394.00 2706.3 0.9670 1.40122 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1218.53 1.211 0.8881 2616.190 1.0633 0.8911 -3035.6 57.40 24.02 +LPC 117.08 1.717 0.8306 2537.074 1.2013 0.8430 -1155.7 22.56 9.67 +HPC 74.93 4.402 0.8627 6119.812 1.6043 0.8875 -4215.2 38.76 39.34 +HPT 27.33 2.783 0.9164 162.633 1.2724 0.9052 4215.3 +LPT 73.26 3.755 0.9114 70.482 1.3813 0.8953 4191.2 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2336.36 1.147 0.9175 0.663 2.2560 0.5215 1.4369 0.9679 3943.9586 +LPC 125.58 1.220 0.8651 0.693 1.4952 0.9323 3.2631 0.9600 3662.6571 +HPC 178.14 16.728 0.8511 0.963 2.2500 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.196 0.9347 106.219 5.1961 1.4085 0.4249 0.9803 1.5311 +LPT 152.22 4.843 0.9103 86.896 4.8426 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3666.94 7743.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 681.88 163.19 11.069 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 681.88 163.19 11.069 +Duct1 0.0025 0.2874 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 681.88 163.19 11.069 +Duct2 0.0025 0.3742 365.99 +Duct3 0.0050 0.2987 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2815 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.2663 901.80 216.71 32.519 +Duct5 0.0075 0.4644 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 1.9899 901.80 216.71 32.519 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 467.92 111.80 4.324 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8875 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6370.9 3475.0 4215.3 +LP_Shaft 2409.8 9134.8 4191.2 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1534.56 0.9940 0.0550 0.30346 0.00922 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.823 0.9975 1.0000 0.9975 2706.36 0.967 939.0 8328.4 +Core_Nozz 1.230 0.9999 1.0000 0.9999 862.88 0.555 765.1 867.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 413 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 12/ 32/ 2/ 9 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.800 43000.0 0.00 284.10 363.1 1.5324 556.43 9.7435 774.79 5.978 1253.5 1228.5 947.8 + core size:22.45 Q: 152.04 Maximum Thrust: 7261.9 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 284.10 3.590 440.05 105.12 0.0000 1071.19 2.355 389.97 3239.8 0.8000 1.40134 +FS_2 Inlet.Fl_O 284.10 3.572 440.05 105.12 0.0000 1076.59 3.320 430.91 5943.4 0.3252 1.40134 +FS_21 Fan.Fl_O 284.10 3.899 454.31 108.54 0.0000 1002.08 3.465 439.21 4515.2 0.4140 1.40131 +FS_13 Splitter.Fl_O2 257.66 3.899 454.31 108.54 0.0000 908.80 3.380 436.10 3795.6 0.4562 1.40131 +FS_22 Splitter.Fl_O1 26.44 3.899 454.31 108.54 0.0000 93.27 3.764 449.73 719.5 0.2252 1.40131 +FS_23 Duct1.Fl_O 26.44 3.890 454.31 108.54 0.0000 93.51 3.754 449.73 721.3 0.2252 1.40131 +FS_24 LPC.Fl_O 26.44 5.633 516.43 123.42 0.0000 68.84 5.200 504.76 366.0 0.3396 1.40056 +FS_25 Duct2.Fl_O 26.44 5.619 516.43 123.42 0.0000 69.01 5.187 504.76 366.9 0.3396 1.40056 +FS_3 HPC.Fl_O 26.44 21.460 797.41 191.18 0.0000 22.45 19.828 779.82 119.9 0.3389 1.39207 +FS_36 Bld3.Fl_O 24.06 21.460 797.41 191.18 0.0000 20.43 19.828 779.82 109.1 0.3389 1.39207 +FS_4 Burner.Fl_O 24.22 20.280 1253.49 306.72 0.0064 27.28 20.150 1251.36 483.4 0.0971 1.36023 +FS_45 HPT.Fl_O 26.60 7.204 947.77 229.01 0.0058 73.35 6.776 931.91 439.1 0.2990 1.37999 +FS_48 Duct3.Fl_O 26.60 7.168 947.77 229.01 0.0058 73.72 6.742 931.91 441.4 0.2990 1.37999 +FS_5 LPT.Fl_O 26.60 2.631 739.58 177.76 0.0058 177.44 2.552 733.34 1477.4 0.2085 1.39111 +FS_7 Duct4.Fl_O 26.60 2.604 739.58 177.76 0.0058 179.23 2.563 736.24 2018.9 0.1523 1.39111 +FS_9 Core_Nozz.Fl_O 26.60 2.604 739.58 177.76 0.0058 179.23 2.355 718.92 862.9 0.3831 1.39111 +FS_15 BypBld.Fl_O 257.66 3.899 454.31 108.54 0.0000 908.80 3.380 436.10 3795.6 0.4562 1.40131 +FS_17 Duct5.Fl_O 257.66 3.870 454.31 108.54 0.0000 915.67 3.355 436.10 3824.3 0.4562 1.40131 +FS_19 Byp_Nozz.Fl_O 257.66 3.870 454.31 108.54 0.0000 915.67 2.355 394.04 2706.4 0.8731 1.40131 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1076.59 1.092 0.7844 2081.051 1.0324 0.7872 -1372.0 81.07 25.92 +LPC 93.51 1.448 0.8176 2048.130 1.1367 0.8270 -556.7 26.66 7.87 +HPC 69.01 3.819 0.8528 6011.678 1.5441 0.8774 -2535.5 50.44 51.46 +HPT 27.28 2.815 0.9180 169.432 1.2881 0.9065 2535.6 +LPT 73.72 2.725 0.9020 62.264 1.2815 0.8887 1928.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2064.21 1.064 0.8104 0.528 2.6336 0.5215 1.4369 0.9679 3943.9586 +LPC 100.30 1.137 0.8517 0.559 1.5266 0.9323 3.2631 0.9600 3662.6571 +HPC 164.07 14.033 0.8413 0.946 2.3845 0.4206 0.2163 1.0137 6357.1603 +HPT 30.02 5.272 0.9364 110.659 5.2723 1.4085 0.4249 0.9803 1.5311 +LPT 153.18 3.406 0.9009 76.763 3.4060 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3239.78 6841.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 615.22 147.13 7.940 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 615.22 147.13 7.940 +Duct1 0.0025 0.2252 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 615.22 147.13 7.940 +Duct2 0.0025 0.3396 365.99 +Duct3 0.0050 0.2990 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2085 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 0.9255 797.41 191.18 21.460 +Duct5 0.0075 0.4562 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 1.4544 797.41 191.18 21.460 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 454.31 108.54 3.899 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.7435 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 5998.7 2220.0 2535.6 +LP_Shaft 1916.8 5284.9 1928.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1253.49 0.9940 0.0550 0.15456 0.00642 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.644 0.9975 1.0000 0.9975 2706.36 0.873 847.8 6789.6 +Core_Nozz 1.106 0.9999 1.0000 0.9999 862.88 0.383 502.0 415.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 414 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 43000.0 0.00 461.74 7472.2 0.6239 4662.05 5.0403 823.21 22.724 2365.6 2305.4 1845.2 + core size:19.95 Q: 171.64 Maximum Thrust: 7472.2 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 461.74 3.777 446.51 106.67 0.0000 1666.72 2.355 389.97 4955.7 0.8500 1.40133 +FS_2 Inlet.Fl_O 461.74 3.759 446.51 106.67 0.0000 1675.11 3.000 418.61 5943.4 0.5763 1.40133 +FS_21 Fan.Fl_O 461.74 6.181 525.26 125.53 0.0000 1104.75 5.314 503.03 4515.2 0.4696 1.40040 +FS_13 Splitter.Fl_O2 385.29 6.181 525.26 125.53 0.0000 921.85 5.329 503.45 3795.6 0.4650 1.40040 +FS_22 Splitter.Fl_O1 76.44 6.181 525.26 125.53 0.0000 182.90 5.229 500.71 719.5 0.4947 1.40040 +FS_23 Duct1.Fl_O 76.44 6.166 525.26 125.53 0.0000 183.36 5.216 500.71 721.3 0.4947 1.40040 +FS_24 LPC.Fl_O 76.44 15.341 704.73 168.71 0.0000 85.36 13.421 678.49 366.0 0.4417 1.39585 +FS_25 Duct2.Fl_O 76.44 15.302 704.73 168.71 0.0000 85.57 13.387 678.49 366.9 0.4417 1.39585 +FS_3 HPC.Fl_O 76.44 85.840 1204.89 292.56 0.0000 19.95 80.782 1185.35 119.9 0.2990 1.36784 +FS_36 Bld3.Fl_O 69.56 85.840 1204.89 292.56 0.0000 18.15 80.782 1185.35 109.1 0.2990 1.36784 +FS_4 Burner.Fl_O 70.86 81.119 2365.61 621.58 0.0186 27.42 80.595 2362.04 483.4 0.0997 1.30423 +FS_45 HPT.Fl_O 77.74 30.381 1845.16 470.67 0.0169 70.92 28.698 1819.67 439.1 0.2945 1.32214 +FS_48 Duct3.Fl_O 77.74 30.230 1845.16 470.67 0.0169 71.28 28.555 1819.67 441.4 0.2945 1.32214 +FS_5 LPT.Fl_O 77.74 6.186 1278.77 316.17 0.0169 290.00 5.662 1249.63 1477.4 0.3636 1.35154 +FS_7 Duct4.Fl_O 77.74 6.124 1278.77 316.17 0.0169 292.93 5.854 1263.85 2018.9 0.2589 1.35154 +FS_9 Core_Nozz.Fl_O 77.74 6.124 1278.77 316.17 0.0169 292.93 3.270 1083.97 862.9 1.0000 1.35154 +FS_15 BypBld.Fl_O 385.29 6.181 525.26 125.53 0.0000 921.85 5.329 503.45 3795.6 0.4650 1.40040 +FS_17 Duct5.Fl_O 385.29 6.135 525.26 125.53 0.0000 928.82 5.289 503.45 3824.3 0.4650 1.40040 +FS_19 Byp_Nozz.Fl_O 385.29 6.135 525.26 125.53 0.0000 928.82 3.239 437.51 2706.3 1.0000 1.40040 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.645 0.8675 3944.235 1.1764 0.8766 -12322.8 24.71 17.45 +LPC 183.36 2.488 0.8683 3636.548 1.3417 0.8840 -4670.1 28.39 23.30 +HPC 85.57 5.610 0.8651 6326.125 1.7097 0.8923 -13395.1 20.08 20.14 +HPT 27.42 2.670 0.9133 151.612 1.2341 0.9035 13395.3 +LPT 71.28 4.887 0.9322 85.195 1.4429 0.9178 16992.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8963 1.000 2.3706 0.5215 1.4369 0.9679 3943.9586 +LPC 196.67 1.456 0.9045 0.993 1.7667 0.9323 3.2631 0.9600 3662.6571 +HPC 203.43 22.309 0.8535 0.995 2.0421 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.931 0.9316 99.020 4.9305 1.4085 0.4249 0.9803 1.5311 +LPT 148.11 6.422 0.9310 105.035 6.4224 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4955.73 11814.1 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 882.84 212.06 25.636 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 882.84 212.06 25.636 +Duct1 0.0025 0.4947 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 882.84 212.06 25.636 +Duct2 0.0025 0.4417 365.99 +Duct3 0.0050 0.2945 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.6755 1204.89 292.56 85.840 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.2044 1204.89 292.56 85.840 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 525.26 125.53 6.181 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0403 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7374.0 9540.8 13395.3 +LP_Shaft 3659.6 24387.7 16992.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2365.61 0.9940 0.0550 1.29501 0.01862 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.605 0.9953 1.0000 0.9975 2706.36 1.000 1023.3 14647.9 +Core_Nozz 2.601 0.9969 1.0000 0.9999 862.88 1.000 1592.8 4638.3 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 415 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 43000.0 0.00 450.18 6724.6 0.6135 4125.71 5.3025 823.21 20.832 2280.2 2222.5 1772.0 + core size:20.04 Q: 171.64 Maximum Thrust: 7472.2 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 450.18 3.777 446.51 106.67 0.0000 1625.01 2.355 389.97 4831.7 0.8500 1.40133 +FS_2 Inlet.Fl_O 450.18 3.759 446.51 106.67 0.0000 1633.19 3.051 420.61 5943.4 0.5539 1.40133 +FS_21 Fan.Fl_O 450.18 6.042 519.31 124.10 0.0000 1095.73 5.211 497.79 4515.2 0.4645 1.40051 +FS_13 Splitter.Fl_O2 378.75 6.042 519.31 124.10 0.0000 921.87 5.209 497.74 3795.6 0.4650 1.40051 +FS_22 Splitter.Fl_O1 71.43 6.042 519.31 124.10 0.0000 173.86 5.219 498.02 719.5 0.4618 1.40051 +FS_23 Duct1.Fl_O 71.43 6.026 519.31 124.10 0.0000 174.29 5.206 498.02 721.3 0.4618 1.40051 +FS_24 LPC.Fl_O 71.43 14.042 682.91 163.44 0.0000 85.78 12.264 657.14 366.0 0.4444 1.39661 +FS_25 Duct2.Fl_O 71.43 14.007 682.91 163.44 0.0000 86.00 12.233 657.14 366.9 0.4444 1.39661 +FS_3 HPC.Fl_O 71.43 78.691 1170.52 283.82 0.0000 20.04 74.008 1151.27 119.9 0.3004 1.37000 +FS_36 Bld3.Fl_O 65.00 78.691 1170.52 283.82 0.0000 18.24 74.008 1151.27 109.1 0.3004 1.37000 +FS_4 Burner.Fl_O 66.15 74.363 2280.24 595.87 0.0176 27.41 73.883 2276.78 483.4 0.0995 1.30719 +FS_45 HPT.Fl_O 72.58 27.576 1772.03 449.75 0.0160 71.49 26.022 1746.91 439.1 0.2967 1.32588 +FS_48 Duct3.Fl_O 72.58 27.438 1772.03 449.75 0.0160 71.85 25.892 1746.91 441.4 0.2967 1.32588 +FS_5 LPT.Fl_O 72.58 5.654 1229.06 302.89 0.0160 290.36 5.175 1200.77 1477.4 0.3636 1.35527 +FS_7 Duct4.Fl_O 72.58 5.598 1229.06 302.89 0.0160 293.30 5.351 1214.58 2018.9 0.2589 1.35527 +FS_9 Core_Nozz.Fl_O 72.58 5.598 1229.06 302.89 0.0160 293.30 2.987 1040.27 862.9 1.0000 1.35527 +FS_15 BypBld.Fl_O 378.75 6.042 519.31 124.10 0.0000 921.87 5.209 497.74 3795.6 0.4650 1.40051 +FS_17 Duct5.Fl_O 378.75 5.996 519.31 124.10 0.0000 928.84 5.170 497.74 3824.3 0.4650 1.40051 +FS_19 Byp_Nozz.Fl_O 378.75 5.996 519.31 124.10 0.0000 928.84 3.166 432.54 2706.4 1.0000 1.40051 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1633.19 1.607 0.8925 3742.932 1.1630 0.8995 -11105.5 28.20 17.74 +LPC 174.29 2.330 0.8661 3470.673 1.3150 0.8810 -3975.3 28.92 22.20 +HPC 86.00 5.618 0.8640 6336.793 1.7140 0.8916 -12165.8 20.48 20.51 +HPT 27.41 2.697 0.9138 152.270 1.2390 0.9038 12165.8 +LPT 71.85 4.852 0.9278 82.498 1.4418 0.9124 15080.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3131.23 1.423 0.9220 0.949 2.1756 0.5215 1.4369 0.9679 3943.9586 +LPC 186.95 1.408 0.9021 0.948 1.7529 0.9323 3.2631 0.9600 3662.6571 +HPC 204.44 22.349 0.8523 0.997 2.0716 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.993 0.9321 99.451 4.9933 1.4085 0.4249 0.9803 1.5311 +LPT 149.29 6.374 0.9266 101.710 6.3741 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4831.73 11518.5 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 856.36 205.57 23.483 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 856.36 205.57 23.483 +Duct1 0.0025 0.4618 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 856.36 205.57 23.483 +Duct2 0.0025 0.4444 365.99 +Duct3 0.0050 0.2967 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.5000 1170.52 283.82 78.691 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.9286 1170.52 283.82 78.691 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 519.31 124.10 6.042 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3025 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7271.2 8787.6 12165.8 +LP_Shaft 3472.8 22807.4 15080.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2280.24 0.9940 0.0550 1.14603 0.01763 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.546 0.9957 1.0000 0.9975 2706.36 1.000 1017.5 14173.4 +Core_Nozz 2.377 0.9985 1.0000 0.9999 862.88 1.000 1562.3 4069.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 416 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 43000.0 0.00 437.09 5977.8 0.6090 3640.30 5.5076 823.21 19.194 2192.3 2137.4 1699.5 + core size:20.19 Q: 171.64 Maximum Thrust: 7472.2 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 437.09 3.777 446.51 106.67 0.0000 1577.75 2.355 389.97 4691.2 0.8500 1.40133 +FS_2 Inlet.Fl_O 437.09 3.759 446.51 106.67 0.0000 1585.69 3.104 422.68 5943.4 0.5299 1.40133 +FS_21 Fan.Fl_O 437.09 5.870 513.85 122.80 0.0000 1089.23 5.074 492.88 4515.2 0.4608 1.40060 +FS_13 Splitter.Fl_O2 369.92 5.870 513.85 122.80 0.0000 921.85 5.061 492.51 3795.6 0.4650 1.40060 +FS_22 Splitter.Fl_O1 67.17 5.870 513.85 122.80 0.0000 167.38 5.140 494.71 719.5 0.4394 1.40060 +FS_23 Duct1.Fl_O 67.17 5.855 513.85 122.80 0.0000 167.80 5.127 494.71 721.3 0.4394 1.40060 +FS_24 LPC.Fl_O 67.17 13.210 669.43 160.19 0.0000 84.89 11.579 644.80 366.0 0.4383 1.39710 +FS_25 Duct2.Fl_O 67.17 13.177 669.43 160.19 0.0000 85.10 11.550 644.80 366.9 0.4383 1.39710 +FS_3 HPC.Fl_O 67.17 72.505 1140.96 276.33 0.0000 20.19 68.120 1121.81 119.9 0.3027 1.37186 +FS_36 Bld3.Fl_O 61.12 72.505 1140.96 276.33 0.0000 18.37 68.120 1121.81 109.1 0.3027 1.37186 +FS_4 Burner.Fl_O 62.13 68.517 2192.31 569.58 0.0165 27.40 68.075 2188.95 483.4 0.0994 1.31031 +FS_45 HPT.Fl_O 68.18 25.284 1699.47 429.16 0.0151 71.73 23.849 1674.99 439.1 0.2973 1.32985 +FS_48 Duct3.Fl_O 68.18 25.158 1699.47 429.16 0.0151 72.09 23.730 1674.99 441.4 0.2973 1.32985 +FS_5 LPT.Fl_O 68.18 5.189 1176.36 288.92 0.0151 290.77 4.748 1148.98 1477.4 0.3636 1.35929 +FS_7 Duct4.Fl_O 68.18 5.137 1176.36 288.92 0.0151 293.71 4.910 1162.34 2018.9 0.2589 1.35929 +FS_9 Core_Nozz.Fl_O 68.18 5.137 1176.36 288.92 0.0151 293.71 2.739 994.07 862.9 1.0000 1.35929 +FS_15 BypBld.Fl_O 369.92 5.870 513.85 122.80 0.0000 921.85 5.061 492.51 3795.6 0.4650 1.40060 +FS_17 Duct5.Fl_O 369.92 5.826 513.85 122.80 0.0000 928.81 5.023 492.51 3824.3 0.4650 1.40060 +FS_19 Byp_Nozz.Fl_O 369.92 5.826 513.85 122.80 0.0000 928.81 3.076 428.00 2706.4 1.0000 1.40060 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1585.69 1.562 0.9023 3614.167 1.1508 0.9083 -9974.4 31.66 18.33 +LPC 167.80 2.256 0.8632 3369.003 1.3028 0.8778 -3553.1 28.07 20.51 +HPC 85.10 5.502 0.8648 6313.517 1.7044 0.8921 -11037.1 22.11 22.18 +HPT 27.40 2.710 0.9145 153.189 1.2428 0.9043 11037.0 +LPT 72.09 4.848 0.9257 81.343 1.4447 0.9099 13527.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3040.37 1.391 0.9322 0.916 2.0968 0.5215 1.4369 0.9679 3943.9586 +LPC 179.99 1.385 0.8991 0.920 1.7167 0.9323 3.2631 0.9600 3662.6571 +HPC 202.32 21.813 0.8531 0.993 2.0970 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.024 0.9328 100.051 5.0243 1.4085 0.4249 0.9803 1.5311 +LPT 149.80 6.368 0.9245 100.286 6.3678 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4691.20 11183.4 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 837.00 200.84 21.869 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 837.00 200.84 21.869 +Duct1 0.0025 0.4394 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 837.00 200.84 21.869 +Duct2 0.0025 0.4383 365.99 +Duct3 0.0050 0.2973 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.3508 1140.96 276.33 72.505 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.6941 1140.96 276.33 72.505 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 513.85 122.80 5.870 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5076 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7172.6 8081.7 11037.0 +LP_Shaft 3353.3 21187.6 13527.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2192.31 0.9940 0.0550 1.01120 0.01654 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.474 0.9962 1.0000 0.9975 2706.36 1.000 1012.1 13588.8 +Core_Nozz 2.182 0.9995 1.0000 0.9999 862.88 1.000 1529.3 3572.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 417 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 43000.0 0.00 408.86 4483.3 0.6138 2751.99 5.9826 823.21 16.002 2011.4 1962.4 1552.9 + core size:20.55 Q: 171.64 Maximum Thrust: 7472.2 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 408.86 3.777 446.51 106.67 0.0000 1475.87 2.355 389.97 4388.3 0.8500 1.40133 +FS_2 Inlet.Fl_O 408.86 3.759 446.51 106.67 0.0000 1483.30 3.205 426.60 5943.4 0.4822 1.40133 +FS_21 Fan.Fl_O 408.86 5.499 502.95 120.19 0.0000 1075.96 4.775 483.04 4515.2 0.4534 1.40078 +FS_13 Splitter.Fl_O2 350.31 5.499 502.95 120.19 0.0000 921.87 4.741 482.06 3795.6 0.4649 1.40078 +FS_22 Splitter.Fl_O1 58.56 5.499 502.95 120.19 0.0000 154.09 4.935 487.61 719.5 0.3962 1.40078 +FS_23 Duct1.Fl_O 58.56 5.485 502.95 120.19 0.0000 154.48 4.923 487.61 721.3 0.3962 1.40078 +FS_24 LPC.Fl_O 58.56 11.724 645.58 154.44 0.0000 81.89 10.393 623.80 366.0 0.4186 1.39796 +FS_25 Duct2.Fl_O 58.56 11.695 645.58 154.44 0.0000 82.09 10.367 623.80 366.9 0.4186 1.39796 +FS_3 HPC.Fl_O 58.56 60.447 1081.06 261.24 0.0000 20.55 56.651 1062.06 119.9 0.3083 1.37564 +FS_36 Bld3.Fl_O 53.29 60.447 1081.06 261.24 0.0000 18.70 56.651 1062.06 109.1 0.3083 1.37564 +FS_4 Burner.Fl_O 54.05 57.123 2011.37 516.30 0.0143 27.38 56.755 2008.24 483.4 0.0990 1.31754 +FS_45 HPT.Fl_O 59.32 20.958 1552.88 388.21 0.0131 71.97 19.760 1529.92 439.1 0.2975 1.33837 +FS_48 Duct3.Fl_O 59.32 20.853 1552.88 388.21 0.0131 72.34 19.661 1529.92 441.4 0.2975 1.33837 +FS_5 LPT.Fl_O 59.32 4.303 1070.43 261.24 0.0131 291.02 3.937 1045.07 1477.4 0.3629 1.36742 +FS_7 Duct4.Fl_O 59.32 4.260 1070.43 261.24 0.0131 293.96 4.071 1057.44 2018.9 0.2583 1.36742 +FS_9 Core_Nozz.Fl_O 59.32 4.260 1070.43 261.24 0.0131 293.96 2.355 911.20 862.9 0.9668 1.36742 +FS_15 BypBld.Fl_O 350.31 5.499 502.95 120.19 0.0000 921.87 4.741 482.06 3795.6 0.4649 1.40078 +FS_17 Duct5.Fl_O 350.31 5.458 502.95 120.19 0.0000 928.83 4.706 482.06 3824.3 0.4649 1.40078 +FS_19 Byp_Nozz.Fl_O 350.31 5.458 502.95 120.19 0.0000 928.83 2.882 418.91 2706.4 1.0000 1.40078 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1483.30 1.463 0.9104 3373.753 1.1264 0.9152 -7819.1 39.23 19.66 +LPC 154.48 2.137 0.8541 3178.797 1.2836 0.8687 -2837.8 25.00 16.49 +HPC 82.09 5.169 0.8659 6250.070 1.6745 0.8923 -8847.7 26.50 26.66 +HPT 27.38 2.726 0.9149 155.478 1.2497 0.9047 8847.8 +LPT 72.34 4.846 0.9206 79.435 1.4507 0.9037 10656.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2843.97 1.322 0.9406 0.855 2.0396 0.5215 1.4369 0.9679 3943.9586 +LPC 165.70 1.349 0.8896 0.868 1.6179 0.9323 3.2631 0.9600 3662.6571 +HPC 195.16 20.271 0.8542 0.983 2.1340 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.061 0.9332 101.546 5.0615 1.4085 0.4249 0.9803 1.5311 +LPT 150.30 6.365 0.9194 97.934 6.3647 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4388.26 10461.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 800.01 191.82 18.837 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 800.01 191.82 18.837 +Duct1 0.0025 0.3962 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 800.01 191.82 18.837 +Duct2 0.0025 0.4186 365.99 +Duct3 0.0050 0.2975 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3629 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.0494 1081.06 261.24 60.447 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.2205 1081.06 261.24 60.447 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 502.95 120.19 5.499 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9826 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6972.9 6664.3 8847.8 +LP_Shaft 3130.3 17880.6 10656.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2011.37 0.9940 0.0550 0.76444 0.01435 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.318 0.9969 1.0000 0.9975 2706.36 1.000 1001.3 12328.6 +Core_Nozz 1.809 0.9999 1.0000 0.9999 862.88 0.967 1418.9 2616.0 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 418 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 43000.0 0.00 376.40 2988.8 0.6473 1934.74 6.6848 823.21 12.681 1810.7 1768.2 1390.5 + core size:20.97 Q: 171.64 Maximum Thrust: 7472.2 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 376.40 3.777 446.51 106.67 0.0000 1358.68 2.355 389.97 4039.8 0.8500 1.40133 +FS_2 Inlet.Fl_O 376.40 3.759 446.51 106.67 0.0000 1365.52 3.305 430.35 5943.4 0.4324 1.40133 +FS_21 Fan.Fl_O 376.40 5.076 490.57 117.22 0.0000 1059.83 4.431 471.86 4515.2 0.4445 1.40096 +FS_13 Splitter.Fl_O2 327.42 5.076 490.57 117.22 0.0000 921.92 4.376 470.18 3795.6 0.4649 1.40096 +FS_22 Splitter.Fl_O1 48.98 5.076 490.57 117.22 0.0000 137.91 4.670 479.00 719.5 0.3471 1.40096 +FS_23 Duct1.Fl_O 48.98 5.063 490.57 117.22 0.0000 138.26 4.658 479.00 721.3 0.3471 1.40096 +FS_24 LPC.Fl_O 48.98 9.958 614.64 146.99 0.0000 78.69 8.926 595.78 366.0 0.3984 1.39879 +FS_25 Duct2.Fl_O 48.98 9.933 614.64 146.99 0.0000 78.89 8.904 595.78 366.9 0.3984 1.39879 +FS_3 HPC.Fl_O 48.98 47.901 1010.31 243.55 0.0000 20.97 44.759 991.59 119.9 0.3149 1.38007 +FS_36 Bld3.Fl_O 44.57 47.901 1010.31 243.55 0.0000 19.09 44.759 991.59 109.1 0.3149 1.38007 +FS_4 Burner.Fl_O 45.11 45.267 1810.71 458.62 0.0121 27.36 44.976 1807.83 483.4 0.0986 1.32692 +FS_45 HPT.Fl_O 49.52 16.469 1390.54 343.96 0.0110 72.35 15.518 1369.29 439.1 0.2980 1.34870 +FS_48 Duct3.Fl_O 49.52 16.386 1390.54 343.96 0.0110 72.71 15.440 1369.29 441.4 0.2980 1.34870 +FS_5 LPT.Fl_O 49.52 3.559 965.58 234.32 0.0110 279.00 3.283 944.50 1477.4 0.3444 1.37550 +FS_7 Duct4.Fl_O 49.52 3.523 965.58 234.32 0.0110 281.82 3.380 954.71 2018.9 0.2461 1.37550 +FS_9 Core_Nozz.Fl_O 49.52 3.523 965.58 234.32 0.0110 281.82 2.355 864.49 862.9 0.7849 1.37550 +FS_15 BypBld.Fl_O 327.42 5.076 490.57 117.22 0.0000 921.92 4.376 470.18 3795.6 0.4649 1.40096 +FS_17 Duct5.Fl_O 327.42 5.038 490.57 117.22 0.0000 928.89 4.344 470.18 3824.3 0.4649 1.40096 +FS_19 Byp_Nozz.Fl_O 327.42 5.038 490.57 117.22 0.0000 928.89 2.660 408.59 2706.4 1.0000 1.40096 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1365.52 1.351 0.9103 3062.985 1.0987 0.9141 -5618.0 46.73 21.33 +LPC 138.26 1.967 0.8430 2922.195 1.2529 0.8571 -2063.5 22.32 12.86 +HPC 78.89 4.823 0.8647 6195.689 1.6437 0.8904 -6691.3 31.65 31.89 +HPT 27.36 2.749 0.9154 158.501 1.2586 0.9047 6691.4 +LPT 72.71 4.605 0.9152 76.212 1.4401 0.8973 7681.5 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2618.19 1.244 0.9405 0.777 2.0719 0.5215 1.4369 0.9679 3943.9586 +LPC 148.30 1.296 0.8781 0.798 1.5327 0.9323 3.2631 0.9600 3662.6571 +HPC 187.55 18.671 0.8530 0.975 2.1685 0.4206 0.2163 1.0137 6357.1603 +HPT 30.10 5.116 0.9338 103.520 5.1156 1.4085 0.4249 0.9803 1.5311 +LPT 151.08 6.028 0.9140 93.959 6.0283 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4039.82 9630.6 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 754.62 180.79 15.495 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 754.62 180.79 15.495 +Duct1 0.0025 0.3471 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 754.62 180.79 15.495 +Duct2 0.0025 0.3984 365.99 +Duct3 0.0050 0.2980 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3444 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.7143 1010.31 243.55 47.901 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.6939 1010.31 243.55 47.901 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 490.57 117.22 5.076 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6848 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6744.6 5210.7 6691.4 +LP_Shaft 2841.9 14196.1 7681.5 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1810.71 0.9940 0.0550 0.53743 0.01206 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.139 0.9975 1.0000 0.9975 2706.36 1.000 988.9 10889.9 +Core_Nozz 1.496 0.9999 1.0000 0.9999 862.88 0.785 1123.8 1729.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 419 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 43000.0 0.00 337.55 1494.5 0.7753 1158.65 7.8781 823.21 9.104 1553.4 1519.1 1184.4 + core size:21.60 Q: 171.64 Maximum Thrust: 7472.2 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 337.55 3.777 446.51 106.67 0.0000 1218.45 2.355 389.97 3622.9 0.8500 1.40133 +FS_2 Inlet.Fl_O 337.55 3.759 446.51 106.67 0.0000 1224.59 3.405 434.06 5943.4 0.3780 1.40133 +FS_21 Fan.Fl_O 337.55 4.571 475.43 113.59 0.0000 1039.01 4.017 458.17 4515.2 0.4333 1.40114 +FS_13 Splitter.Fl_O2 299.53 4.571 475.43 113.59 0.0000 921.98 3.941 455.66 3795.6 0.4650 1.40114 +FS_22 Splitter.Fl_O1 38.02 4.571 475.43 113.59 0.0000 117.03 4.315 467.64 719.5 0.2881 1.40114 +FS_23 Duct1.Fl_O 38.02 4.560 475.43 113.59 0.0000 117.32 4.304 467.64 721.3 0.2881 1.40114 +FS_24 LPC.Fl_O 38.02 7.899 573.00 136.99 0.0000 74.35 7.179 557.59 366.0 0.3719 1.39948 +FS_25 Duct2.Fl_O 38.02 7.879 573.00 136.99 0.0000 74.54 7.161 557.59 366.9 0.3719 1.39948 +FS_3 HPC.Fl_O 38.02 34.388 916.53 220.33 0.0000 21.60 31.984 898.20 119.9 0.3249 1.38584 +FS_36 Bld3.Fl_O 34.60 34.388 916.53 220.33 0.0000 19.66 31.984 898.20 109.1 0.3249 1.38584 +FS_4 Burner.Fl_O 34.92 32.497 1553.38 386.92 0.0093 27.33 32.288 1550.84 483.4 0.0980 1.34092 +FS_45 HPT.Fl_O 38.34 11.688 1184.35 289.41 0.0085 72.85 11.004 1165.44 439.1 0.2986 1.36320 +FS_48 Duct3.Fl_O 38.34 11.630 1184.35 289.41 0.0085 73.22 10.949 1165.44 441.4 0.2986 1.36320 +FS_5 LPT.Fl_O 38.34 2.988 850.34 205.25 0.0085 241.47 2.819 836.67 1477.4 0.2915 1.38409 +FS_7 Duct4.Fl_O 38.34 2.958 850.34 205.25 0.0085 243.91 2.869 843.17 2018.9 0.2103 1.38409 +FS_9 Core_Nozz.Fl_O 38.34 2.958 850.34 205.25 0.0085 243.91 2.355 798.05 863.0 0.5829 1.38409 +FS_15 BypBld.Fl_O 299.53 4.571 475.43 113.59 0.0000 921.98 3.941 455.66 3795.6 0.4650 1.40114 +FS_17 Duct5.Fl_O 299.53 4.537 475.43 113.59 0.0000 928.95 3.911 455.66 3824.3 0.4650 1.40114 +FS_19 Byp_Nozz.Fl_O 299.53 4.537 475.43 113.59 0.0000 928.95 2.396 395.97 2706.3 1.0000 1.40114 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1224.59 1.216 0.8898 2636.754 1.0648 0.8929 -3306.7 56.77 23.91 +LPC 117.32 1.732 0.8291 2555.294 1.2052 0.8418 -1258.5 21.63 9.36 +HPC 74.54 4.365 0.8625 6112.439 1.5995 0.8871 -4483.5 39.39 39.99 +HPT 27.33 2.780 0.9164 163.008 1.2715 0.9053 4483.6 +LPT 73.22 3.892 0.9117 71.088 1.3928 0.8950 4565.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2347.97 1.150 0.9193 0.669 2.2450 0.5215 1.4369 0.9679 3943.9586 +LPC 125.84 1.224 0.8636 0.698 1.4766 0.9323 3.2631 0.9600 3662.6571 +HPC 177.20 16.554 0.8508 0.962 2.2570 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.190 0.9348 106.463 5.1901 1.4085 0.4249 0.9803 1.5311 +LPT 152.13 5.035 0.9105 87.643 5.0347 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3622.88 8636.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 694.17 166.16 11.762 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 694.17 166.16 11.762 +Duct1 0.0025 0.2881 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 694.17 166.16 11.762 +Duct2 0.0025 0.3719 365.99 +Duct3 0.0050 0.2986 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2915 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.3307 916.53 220.33 34.388 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.0911 916.53 220.33 34.388 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 475.43 113.59 4.571 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8781 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6424.6 3665.3 4483.6 +LP_Shaft 2446.5 9801.1 4565.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1553.38 0.9940 0.0550 0.32185 0.00930 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.927 0.9975 1.0000 0.9975 2706.36 1.000 973.5 9173.9 +Core_Nozz 1.256 0.9999 1.0000 0.9999 862.88 0.583 803.2 957.2 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 420 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 11/ 31/ 2/ 8 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.850 43000.0 0.00 300.46 373.6 1.5861 592.56 9.7707 823.21 6.037 1271.5 1246.4 962.3 + core size:22.50 Q: 171.64 Maximum Thrust: 7472.2 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 300.46 3.777 446.51 106.67 0.0000 1084.58 2.355 389.97 3224.8 0.8500 1.40133 +FS_2 Inlet.Fl_O 300.46 3.759 446.51 106.67 0.0000 1090.04 3.486 436.97 5943.4 0.3298 1.40133 +FS_21 Fan.Fl_O 300.46 4.119 461.59 110.28 0.0000 1011.24 3.651 445.90 4515.2 0.4187 1.40126 +FS_13 Splitter.Fl_O2 272.57 4.119 461.59 110.28 0.0000 917.35 3.558 442.64 3795.6 0.4619 1.40126 +FS_22 Splitter.Fl_O1 27.90 4.119 461.59 110.28 0.0000 93.89 3.974 456.87 719.5 0.2268 1.40126 +FS_23 Duct1.Fl_O 27.90 4.109 461.59 110.28 0.0000 94.12 3.964 456.87 721.3 0.2268 1.40126 +FS_24 LPC.Fl_O 27.90 6.038 527.47 126.06 0.0000 68.48 5.579 515.70 366.0 0.3376 1.40036 +FS_25 Duct2.Fl_O 27.90 6.022 527.47 126.06 0.0000 68.65 5.565 515.70 366.9 0.3376 1.40036 +FS_3 HPC.Fl_O 27.90 22.805 812.29 194.81 0.0000 22.50 21.063 794.32 119.9 0.3398 1.39136 +FS_36 Bld3.Fl_O 25.39 22.805 812.29 194.81 0.0000 20.47 21.063 794.32 109.1 0.3398 1.39136 +FS_4 Burner.Fl_O 25.55 21.551 1271.52 311.41 0.0065 27.28 21.413 1269.37 483.4 0.0971 1.35906 +FS_45 HPT.Fl_O 28.06 7.660 962.29 232.64 0.0059 73.33 7.205 946.22 439.1 0.2990 1.37905 +FS_48 Duct3.Fl_O 28.06 7.621 962.29 232.64 0.0059 73.70 7.169 946.22 441.4 0.2990 1.37905 +FS_5 LPT.Fl_O 28.06 2.660 741.76 178.30 0.0059 185.39 2.574 734.91 1477.4 0.2184 1.39099 +FS_7 Duct4.Fl_O 28.06 2.634 741.76 178.30 0.0059 187.26 2.588 738.10 2018.9 0.1593 1.39099 +FS_9 Core_Nozz.Fl_O 28.06 2.634 741.76 178.30 0.0059 187.26 2.355 718.79 862.9 0.4041 1.39099 +FS_15 BypBld.Fl_O 272.57 4.119 461.59 110.28 0.0000 917.35 3.558 442.64 3795.6 0.4619 1.40126 +FS_17 Duct5.Fl_O 272.57 4.088 461.59 110.28 0.0000 924.29 3.532 442.64 3824.3 0.4619 1.40126 +FS_19 Byp_Nozz.Fl_O 272.57 4.088 461.59 110.28 0.0000 924.29 2.355 394.11 2706.4 0.9237 1.40126 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1090.04 1.096 0.7872 2117.362 1.0338 0.7900 -1534.5 79.81 26.30 +LPC 94.12 1.469 0.8156 2082.489 1.1427 0.8254 -622.9 24.86 7.48 +HPC 68.65 3.787 0.8519 6004.954 1.5400 0.8765 -2713.5 51.13 52.18 +HPT 27.28 2.813 0.9180 169.824 1.2873 0.9067 2713.5 +LPT 73.70 2.865 0.9028 63.330 1.2973 0.8889 2157.4 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2090.00 1.067 0.8133 0.537 2.6267 0.5215 1.4369 0.9679 3943.9586 +LPC 100.96 1.144 0.8496 0.569 1.4943 0.9323 3.2631 0.9600 3662.6571 +HPC 163.20 13.882 0.8404 0.945 2.3885 0.4206 0.2163 1.0137 6357.1603 +HPT 30.01 5.268 0.9365 110.915 5.2682 1.4085 0.4249 0.9803 1.5311 +LPT 153.14 3.602 0.9017 78.078 3.6017 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3224.82 7687.7 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 627.65 150.12 8.481 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 627.65 150.12 8.481 +Duct1 0.0025 0.2268 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 627.65 150.12 8.481 +Duct2 0.0025 0.3376 365.99 +Duct3 0.0050 0.2990 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2184 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 0.9764 812.29 194.81 22.805 +Duct5 0.0075 0.4619 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 1.5343 812.29 194.81 22.805 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 461.59 110.28 4.119 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.7707 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6055.7 2353.4 2713.5 +LP_Shaft 1964.5 5767.8 2157.4 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1271.52 0.9940 0.0550 0.16460 0.00648 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.736 0.9975 1.0000 0.9975 2706.36 0.924 897.1 7599.5 +Core_Nozz 1.118 0.9999 1.0000 0.9999 862.88 0.404 529.5 461.8 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 421 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 3/ 13/ 1/ 1 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.900 43000.0 0.00 483.25 7713.1 0.6440 4967.44 5.0408 871.64 22.718 2399.3 2338.3 1872.8 + core size:19.94 Q: 192.43 Maximum Thrust: 7713.1 % Thrust:100.0 Power code:100.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 483.25 3.984 453.35 108.31 0.0000 1666.72 2.355 389.97 4898.5 0.9000 1.40131 +FS_2 Inlet.Fl_O 483.25 3.964 453.35 108.31 0.0000 1675.11 3.164 425.02 5943.4 0.5763 1.40131 +FS_21 Fan.Fl_O 483.25 6.519 533.30 127.46 0.0000 1104.74 5.604 510.74 4515.2 0.4696 1.40024 +FS_13 Splitter.Fl_O2 403.25 6.519 533.30 127.46 0.0000 921.86 5.620 511.17 3795.6 0.4650 1.40024 +FS_22 Splitter.Fl_O1 80.00 6.519 533.30 127.46 0.0000 182.88 5.514 508.39 719.5 0.4946 1.40024 +FS_23 Duct1.Fl_O 80.00 6.502 533.30 127.46 0.0000 183.34 5.501 508.39 721.3 0.4946 1.40024 +FS_24 LPC.Fl_O 80.00 16.181 715.49 171.31 0.0000 85.33 14.158 688.89 366.0 0.4416 1.39549 +FS_25 Duct2.Fl_O 80.00 16.141 715.49 171.31 0.0000 85.55 14.123 688.89 366.9 0.4416 1.39549 +FS_3 HPC.Fl_O 80.00 90.502 1222.14 296.96 0.0000 19.94 85.173 1202.37 119.9 0.2991 1.36675 +FS_36 Bld3.Fl_O 72.80 90.502 1222.14 296.96 0.0000 18.15 85.173 1202.37 109.1 0.2991 1.36675 +FS_4 Burner.Fl_O 74.18 85.524 2399.35 631.76 0.0190 27.41 84.972 2395.74 483.4 0.0997 1.30314 +FS_45 HPT.Fl_O 81.38 32.042 1872.81 478.62 0.0172 70.92 30.267 1847.03 439.1 0.2947 1.32079 +FS_48 Duct3.Fl_O 81.38 31.882 1872.81 478.62 0.0172 71.28 30.116 1847.03 441.4 0.2947 1.32079 +FS_5 LPT.Fl_O 81.38 6.531 1299.67 321.77 0.0172 289.88 5.978 1270.17 1477.4 0.3637 1.35003 +FS_7 Duct4.Fl_O 81.38 6.465 1299.67 321.77 0.0172 292.81 6.181 1284.57 2018.9 0.2589 1.35003 +FS_9 Core_Nozz.Fl_O 81.38 6.465 1299.67 321.77 0.0172 292.81 3.454 1102.36 862.9 1.0000 1.35003 +FS_15 BypBld.Fl_O 403.25 6.519 533.30 127.46 0.0000 921.86 5.620 511.17 3795.6 0.4650 1.40024 +FS_17 Duct5.Fl_O 403.25 6.470 533.30 127.46 0.0000 928.83 5.578 511.17 3824.3 0.4650 1.40024 +FS_19 Byp_Nozz.Fl_O 403.25 6.470 533.30 127.46 0.0000 928.83 3.416 444.22 2706.3 1.0000 1.40024 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1675.11 1.645 0.8675 3944.235 1.1764 0.8766 -13095.3 24.71 17.45 +LPC 183.34 2.489 0.8683 3636.584 1.3416 0.8840 -4963.3 28.36 23.27 +HPC 85.55 5.607 0.8652 6325.393 1.7081 0.8922 -14221.6 20.11 20.16 +HPT 27.41 2.669 0.9133 151.669 1.2332 0.9035 14221.8 +LPT 71.28 4.882 0.9323 85.210 1.4410 0.9180 18058.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3211.79 1.449 0.8963 1.000 2.3706 0.5215 1.4369 0.9679 3943.9586 +LPC 196.65 1.456 0.9045 0.993 1.7660 0.9323 3.2631 0.9600 3662.6571 +HPC 203.37 22.297 0.8535 0.995 2.0420 0.4206 0.2163 1.0137 6357.1603 +HPT 30.16 4.928 0.9317 99.058 4.9284 1.4085 0.4249 0.9803 1.5311 +LPT 148.10 6.415 0.9311 105.053 6.4152 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4898.48 13091.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 896.00 215.29 27.035 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 896.00 215.29 27.035 +Duct1 0.0025 0.4946 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 896.00 215.29 27.035 +Duct2 0.0025 0.4416 365.99 +Duct3 0.0050 0.2947 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3637 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.7999 1222.14 296.96 90.502 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.3999 1222.14 296.96 90.502 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 533.30 127.46 6.519 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.0408 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7429.2 10054.2 14221.8 +LP_Shaft 3687.5 25720.7 18058.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2399.35 0.9940 0.0550 1.37984 0.01895 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.747 0.9942 1.0000 0.9975 2706.36 1.000 1031.1 15795.9 +Core_Nozz 2.746 0.9955 1.0000 0.9999 862.88 1.000 1605.5 5009.1 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:57 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 422 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.900 43000.0 0.00 471.18 6941.4 0.6334 4397.02 5.3028 871.64 20.829 2313.1 2254.6 1798.9 + core size:20.03 Q: 192.43 Maximum Thrust: 7713.1 % Thrust: 90.0 Power code: 90.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 471.18 3.984 453.35 108.31 0.0000 1625.09 2.355 389.97 4776.1 0.9000 1.40131 +FS_2 Inlet.Fl_O 471.18 3.964 453.35 108.31 0.0000 1633.27 3.217 427.05 5943.4 0.5539 1.40131 +FS_21 Fan.Fl_O 471.18 6.372 527.27 126.01 0.0000 1095.73 5.495 505.43 4515.2 0.4645 1.40036 +FS_13 Splitter.Fl_O2 396.42 6.372 527.27 126.01 0.0000 921.88 5.494 505.38 3795.6 0.4650 1.40036 +FS_22 Splitter.Fl_O1 74.76 6.372 527.27 126.01 0.0000 173.85 5.505 505.67 719.5 0.4618 1.40036 +FS_23 Duct1.Fl_O 74.76 6.356 527.27 126.01 0.0000 174.28 5.491 505.67 721.3 0.4618 1.40036 +FS_24 LPC.Fl_O 74.76 14.813 693.38 165.97 0.0000 85.75 12.939 667.25 366.0 0.4442 1.39624 +FS_25 Duct2.Fl_O 74.76 14.776 693.38 165.97 0.0000 85.97 12.907 667.25 366.9 0.4442 1.39624 +FS_3 HPC.Fl_O 74.76 82.976 1187.41 288.11 0.0000 20.03 78.042 1167.93 119.9 0.3004 1.36894 +FS_36 Bld3.Fl_O 68.03 82.976 1187.41 288.11 0.0000 18.23 78.042 1167.93 109.1 0.3004 1.36894 +FS_4 Burner.Fl_O 69.25 78.412 2313.12 605.71 0.0180 27.41 77.907 2309.61 483.4 0.0996 1.30608 +FS_45 HPT.Fl_O 75.98 29.088 1798.92 457.40 0.0163 71.49 27.449 1773.50 439.1 0.2969 1.32450 +FS_48 Duct3.Fl_O 75.98 28.943 1798.92 457.40 0.0163 71.85 27.312 1773.50 441.4 0.2969 1.32450 +FS_5 LPT.Fl_O 75.98 5.971 1249.39 308.29 0.0163 290.21 5.465 1220.74 1477.4 0.3636 1.35379 +FS_7 Duct4.Fl_O 75.98 5.912 1249.39 308.29 0.0163 293.14 5.651 1234.72 2018.9 0.2589 1.35379 +FS_9 Core_Nozz.Fl_O 75.98 5.912 1249.39 308.29 0.0163 293.14 3.155 1058.11 862.9 1.0000 1.35379 +FS_15 BypBld.Fl_O 396.42 6.372 527.27 126.01 0.0000 921.88 5.494 505.38 3795.6 0.4650 1.40036 +FS_17 Duct5.Fl_O 396.42 6.324 527.27 126.01 0.0000 928.85 5.452 505.38 3824.3 0.4650 1.40036 +FS_19 Byp_Nozz.Fl_O 396.42 6.324 527.27 126.01 0.0000 928.85 3.339 439.19 2706.4 1.0000 1.40036 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1633.27 1.608 0.8924 3743.192 1.1630 0.8994 -11803.8 28.20 17.74 +LPC 174.28 2.331 0.8660 3470.910 1.3150 0.8810 -4225.9 28.89 22.18 +HPC 85.97 5.616 0.8640 6335.967 1.7125 0.8915 -12918.9 20.50 20.53 +HPT 27.41 2.696 0.9138 152.319 1.2381 0.9039 12918.9 +LPT 71.85 4.847 0.9279 82.511 1.4398 0.9125 16029.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3131.39 1.423 0.9220 0.949 2.1758 0.5215 1.4369 0.9679 3943.9586 +LPC 186.94 1.408 0.9021 0.948 1.7522 0.9323 3.2631 0.9600 3662.6571 +HPC 204.37 22.337 0.8524 0.997 2.0712 0.4206 0.2163 1.0137 6357.1603 +HPT 30.15 4.991 0.9322 99.482 4.9910 1.4085 0.4249 0.9803 1.5311 +LPT 149.29 6.366 0.9267 101.725 6.3662 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4776.14 12764.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 869.21 208.72 24.768 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 869.21 208.72 24.768 +Duct1 0.0025 0.4618 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 869.21 208.72 24.768 +Duct2 0.0025 0.4442 365.99 +Duct3 0.0050 0.2969 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.6165 1187.41 288.11 82.976 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 4.1116 1187.41 288.11 82.976 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 527.27 126.01 6.372 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.3028 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7325.8 9262.0 12918.9 +LP_Shaft 3499.6 24057.2 16029.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2313.12 0.9940 0.0550 1.22139 0.01795 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.686 0.9947 1.0000 0.9975 2706.36 1.000 1025.3 15296.4 +Core_Nozz 2.511 0.9976 1.0000 0.9999 862.88 1.000 1574.9 4409.9 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:58 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 423 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 5/ 15/ 1/ 3 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.900 43000.0 0.00 457.47 6170.5 0.6286 3879.03 5.5077 871.64 19.191 2223.9 2168.2 1725.2 + core size:20.19 Q: 192.43 Maximum Thrust: 7713.1 % Thrust: 80.0 Power code: 80.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 457.47 3.984 453.35 108.31 0.0000 1577.79 2.355 389.97 4637.1 0.9000 1.40131 +FS_2 Inlet.Fl_O 457.47 3.964 453.35 108.31 0.0000 1585.73 3.273 429.16 5943.4 0.5299 1.40131 +FS_21 Fan.Fl_O 457.47 6.190 521.73 124.69 0.0000 1089.22 5.351 500.44 4515.2 0.4608 1.40046 +FS_13 Splitter.Fl_O2 387.17 6.190 521.73 124.69 0.0000 921.85 5.337 500.07 3795.6 0.4650 1.40046 +FS_22 Splitter.Fl_O1 70.30 6.190 521.73 124.69 0.0000 167.38 5.421 502.30 719.5 0.4395 1.40046 +FS_23 Duct1.Fl_O 70.30 6.175 521.73 124.69 0.0000 167.80 5.407 502.30 721.3 0.4395 1.40046 +FS_24 LPC.Fl_O 70.30 13.933 679.65 162.65 0.0000 84.88 12.213 654.66 366.0 0.4383 1.39672 +FS_25 Duct2.Fl_O 70.30 13.898 679.65 162.65 0.0000 85.09 12.183 654.66 366.9 0.4383 1.39672 +FS_3 HPC.Fl_O 70.30 76.452 1157.50 280.52 0.0000 20.19 71.831 1138.12 119.9 0.3027 1.37082 +FS_36 Bld3.Fl_O 63.97 76.452 1157.50 280.52 0.0000 18.37 71.831 1138.12 109.1 0.3027 1.37082 +FS_4 Burner.Fl_O 65.05 72.247 2223.86 578.93 0.0168 27.40 71.781 2220.46 483.4 0.0994 1.30924 +FS_45 HPT.Fl_O 71.37 26.670 1725.16 436.39 0.0153 71.73 25.156 1700.39 439.1 0.2975 1.32847 +FS_48 Duct3.Fl_O 71.37 26.537 1725.16 436.39 0.0153 72.09 25.031 1700.39 441.4 0.2975 1.32847 +FS_5 LPT.Fl_O 71.37 5.480 1195.75 294.02 0.0153 290.62 5.014 1168.03 1477.4 0.3636 1.35787 +FS_7 Duct4.Fl_O 71.37 5.425 1195.75 294.02 0.0153 293.56 5.185 1181.56 2018.9 0.2589 1.35787 +FS_9 Core_Nozz.Fl_O 71.37 5.425 1195.75 294.02 0.0153 293.56 2.894 1011.03 862.9 1.0000 1.35787 +FS_15 BypBld.Fl_O 387.17 6.190 521.73 124.69 0.0000 921.85 5.337 500.07 3795.6 0.4650 1.40046 +FS_17 Duct5.Fl_O 387.17 6.144 521.73 124.69 0.0000 928.81 5.297 500.07 3824.3 0.4650 1.40046 +FS_19 Byp_Nozz.Fl_O 387.17 6.144 521.73 124.69 0.0000 928.81 3.244 434.56 2706.4 1.0000 1.40046 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1585.73 1.562 0.9023 3614.265 1.1508 0.9083 -10600.6 31.66 18.32 +LPC 167.80 2.256 0.8631 3369.106 1.3027 0.8778 -3776.1 28.06 20.50 +HPC 85.09 5.501 0.8648 6313.197 1.7031 0.8920 -11722.5 22.13 22.20 +HPT 27.40 2.709 0.9145 153.247 1.2420 0.9044 11722.4 +LPT 72.09 4.842 0.9258 81.354 1.4427 0.9100 14376.9 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 3040.45 1.391 0.9322 0.916 2.0969 0.5215 1.4369 0.9679 3943.9586 +LPC 179.98 1.385 0.8991 0.920 1.7165 0.9323 3.2631 0.9600 3662.6571 +HPC 202.29 21.806 0.8531 0.993 2.0972 0.4206 0.2163 1.0137 6357.1603 +HPT 30.14 5.022 0.9328 100.089 5.0221 1.4085 0.4249 0.9803 1.5311 +LPT 149.79 6.360 0.9246 100.299 6.3601 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4637.13 12393.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 849.55 203.90 23.062 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 849.55 203.90 23.062 +Duct1 0.0025 0.4395 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 849.55 203.90 23.062 +Duct2 0.0025 0.4383 365.99 +Duct3 0.0050 0.2975 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3636 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.4604 1157.50 280.52 76.452 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.8663 1157.50 280.52 76.452 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 521.73 124.69 6.190 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.5077 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7226.8 8519.3 11722.4 +LP_Shaft 3379.0 22346.3 14376.9 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2223.86 0.9940 0.0550 1.07751 0.01684 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.609 0.9953 1.0000 0.9975 2706.36 1.000 1019.8 14679.2 +Core_Nozz 2.304 0.9990 1.0000 0.9999 862.88 1.000 1541.5 3884.7 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:58 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 424 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.900 43000.0 0.00 427.92 4627.8 0.6331 2929.82 5.9851 871.64 15.992 2040.0 1990.4 1576.2 + core size:20.55 Q: 192.43 Maximum Thrust: 7713.1 % Thrust: 60.0 Power code: 60.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 427.92 3.984 453.35 108.31 0.0000 1475.88 2.355 389.97 4337.6 0.9000 1.40131 +FS_2 Inlet.Fl_O 427.92 3.964 453.35 108.31 0.0000 1483.31 3.380 433.14 5943.4 0.4822 1.40131 +FS_21 Fan.Fl_O 427.92 5.800 510.67 122.04 0.0000 1075.88 5.037 490.47 4515.2 0.4534 1.40065 +FS_13 Splitter.Fl_O2 366.66 5.800 510.67 122.04 0.0000 921.85 5.001 489.46 3795.6 0.4649 1.40065 +FS_22 Splitter.Fl_O1 61.26 5.800 510.67 122.04 0.0000 154.03 5.205 495.12 719.5 0.3960 1.40065 +FS_23 Duct1.Fl_O 61.26 5.785 510.67 122.04 0.0000 154.41 5.192 495.12 721.3 0.3960 1.40065 +FS_24 LPC.Fl_O 61.26 12.371 655.57 156.85 0.0000 81.82 10.970 633.51 366.0 0.4182 1.39762 +FS_25 Duct2.Fl_O 61.26 12.340 655.57 156.85 0.0000 82.02 10.942 633.51 366.9 0.4182 1.39762 +FS_3 HPC.Fl_O 61.26 63.707 1096.72 265.17 0.0000 20.55 59.706 1077.48 119.9 0.3084 1.37465 +FS_36 Bld3.Fl_O 55.75 63.707 1096.72 265.17 0.0000 18.70 59.706 1077.48 109.1 0.3084 1.37465 +FS_4 Burner.Fl_O 56.56 60.203 2039.98 524.59 0.0146 27.38 59.815 2036.82 483.4 0.0991 1.31637 +FS_45 HPT.Fl_O 62.08 22.096 1576.23 394.65 0.0133 71.97 20.834 1553.00 439.1 0.2976 1.33702 +FS_48 Duct3.Fl_O 62.08 21.986 1576.23 394.65 0.0133 72.33 20.730 1553.00 441.4 0.2976 1.33702 +FS_5 LPT.Fl_O 62.08 4.536 1087.56 265.66 0.0133 291.24 4.148 1061.81 1477.4 0.3634 1.36616 +FS_7 Duct4.Fl_O 62.08 4.490 1087.56 265.66 0.0133 294.19 4.291 1074.38 2018.9 0.2587 1.36616 +FS_9 Core_Nozz.Fl_O 62.08 4.490 1087.56 265.66 0.0133 294.19 2.390 916.54 862.9 1.0000 1.36616 +FS_15 BypBld.Fl_O 366.66 5.800 510.67 122.04 0.0000 921.85 5.001 489.46 3795.6 0.4649 1.40065 +FS_17 Duct5.Fl_O 366.66 5.756 510.67 122.04 0.0000 928.82 4.963 489.46 3824.3 0.4649 1.40065 +FS_19 Byp_Nozz.Fl_O 366.66 5.756 510.67 122.04 0.0000 928.82 3.039 425.34 2706.4 1.0000 1.40065 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1483.31 1.463 0.9105 3373.913 1.1264 0.9152 -8311.3 39.22 19.66 +LPC 154.41 2.138 0.8539 3178.924 1.2837 0.8686 -3017.2 24.91 16.43 +HPC 82.02 5.162 0.8659 6248.765 1.6729 0.8923 -9389.2 26.57 26.73 +HPT 27.38 2.725 0.9149 155.541 1.2487 0.9047 9389.3 +LPT 72.33 4.847 0.9207 79.450 1.4493 0.9037 11328.3 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2844.00 1.322 0.9406 0.855 2.0393 0.5215 1.4369 0.9679 3943.9586 +LPC 165.63 1.349 0.8894 0.868 1.6157 0.9323 3.2631 0.9600 3662.6571 +HPC 194.99 20.242 0.8542 0.983 2.1336 0.4206 0.2163 1.0137 6357.1603 +HPT 30.13 5.059 0.9332 101.587 5.0590 1.4085 0.4249 0.9803 1.5311 +LPT 150.30 6.367 0.9195 97.952 6.3668 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4337.60 11592.8 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 812.08 194.76 19.866 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 812.08 194.76 19.866 +Duct1 0.0025 0.3960 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 812.08 194.76 19.866 +Duct2 0.0025 0.4182 365.99 +Duct3 0.0050 0.2976 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3634 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 2.1442 1096.72 265.17 63.707 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 3.3694 1096.72 265.17 63.707 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 510.67 122.04 5.800 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 5.9851 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 7025.2 7019.6 9389.3 +LP_Shaft 3154.3 18862.3 11328.3 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 2039.98 0.9940 0.0550 0.81384 0.01460 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.445 0.9963 1.0000 0.9975 2706.36 1.000 1009.0 13351.0 +Core_Nozz 1.907 0.9999 1.0000 0.9999 862.88 1.000 1471.7 2869.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:58 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 425 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 8/ 18/ 1/ 6 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.900 43000.0 0.00 394.71 3085.2 0.6669 2057.42 6.6832 871.64 12.699 1834.7 1791.8 1410.2 + core size:20.99 Q: 192.43 Maximum Thrust: 7713.1 % Thrust: 40.0 Power code: 40.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 394.71 3.984 453.35 108.31 0.0000 1361.36 2.355 389.97 4001.1 0.9000 1.40131 +FS_2 Inlet.Fl_O 394.71 3.964 453.35 108.31 0.0000 1368.22 3.483 436.87 5943.4 0.4335 1.40131 +FS_21 Fan.Fl_O 394.71 5.365 498.44 119.10 0.0000 1059.82 4.684 479.44 4515.2 0.4446 1.40084 +FS_13 Splitter.Fl_O2 343.34 5.365 498.44 119.10 0.0000 921.88 4.626 477.73 3795.6 0.4649 1.40084 +FS_22 Splitter.Fl_O1 51.37 5.365 498.44 119.10 0.0000 137.94 4.936 486.68 719.5 0.3472 1.40084 +FS_23 Duct1.Fl_O 51.37 5.352 498.44 119.10 0.0000 138.29 4.924 486.68 721.3 0.3472 1.40084 +FS_24 LPC.Fl_O 51.37 10.569 625.42 149.59 0.0000 78.44 9.482 606.37 366.0 0.3969 1.39854 +FS_25 Duct2.Fl_O 51.37 10.543 625.42 149.59 0.0000 78.64 9.459 606.37 366.9 0.3969 1.39854 +FS_3 HPC.Fl_O 51.37 50.589 1025.87 247.43 0.0000 20.99 47.264 1006.86 119.9 0.3153 1.37910 +FS_36 Bld3.Fl_O 46.75 50.589 1025.87 247.43 0.0000 19.10 47.264 1006.86 109.1 0.3153 1.37910 +FS_4 Burner.Fl_O 47.32 47.806 1834.73 465.39 0.0122 27.36 47.499 1831.82 483.4 0.0986 1.32579 +FS_45 HPT.Fl_O 51.95 17.406 1410.19 349.23 0.0111 72.32 16.402 1388.72 439.1 0.2980 1.34745 +FS_48 Duct3.Fl_O 51.95 17.319 1410.19 349.23 0.0111 72.68 16.320 1388.72 441.4 0.2980 1.34745 +FS_5 LPT.Fl_O 51.95 3.698 976.33 237.05 0.0111 283.25 3.401 954.30 1477.4 0.3505 1.37472 +FS_7 Duct4.Fl_O 51.95 3.661 976.33 237.05 0.0111 286.11 3.507 964.99 2018.9 0.2502 1.37472 +FS_9 Core_Nozz.Fl_O 51.95 3.661 976.33 237.05 0.0111 286.11 2.355 865.05 862.9 0.8237 1.37472 +FS_15 BypBld.Fl_O 343.34 5.365 498.44 119.10 0.0000 921.88 4.626 477.73 3795.6 0.4649 1.40084 +FS_17 Duct5.Fl_O 343.34 5.325 498.44 119.10 0.0000 928.85 4.591 477.73 3824.3 0.4649 1.40084 +FS_19 Byp_Nozz.Fl_O 343.34 5.325 498.44 119.10 0.0000 928.85 2.812 415.14 2706.4 1.0000 1.40084 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1368.22 1.354 0.9105 3071.228 1.0994 0.9143 -6029.0 46.49 21.24 +LPC 138.29 1.975 0.8422 2929.037 1.2548 0.8565 -2215.7 21.92 12.65 +HPC 78.64 4.798 0.8647 6190.750 1.6403 0.8904 -7111.6 31.97 32.24 +HPT 27.36 2.747 0.9155 158.708 1.2577 0.9047 7111.6 +LPT 72.68 4.684 0.9147 76.462 1.4444 0.8965 8244.7 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2623.37 1.246 0.9407 0.779 2.0686 0.5215 1.4369 0.9679 3943.9586 +LPC 148.33 1.299 0.8773 0.800 1.5237 0.9323 3.2631 0.9600 3662.6571 +HPC 186.95 18.560 0.8531 0.974 2.1709 0.4206 0.2163 1.0137 6357.1603 +HPT 30.10 5.111 0.9338 103.655 5.1107 1.4085 0.4249 0.9803 1.5311 +LPT 151.02 6.139 0.9135 94.268 6.1387 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 4001.05 10693.3 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 767.16 183.83 16.409 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 767.16 183.83 16.409 +Duct1 0.0025 0.3472 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 767.16 183.83 16.409 +Duct2 0.0025 0.3969 365.99 +Duct3 0.0050 0.2980 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3505 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.7981 1025.87 247.43 50.589 +Duct5 0.0075 0.4649 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.8255 1025.87 247.43 50.589 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 498.44 119.10 5.365 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 6.6832 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6798.0 5494.4 7111.6 +LP_Shaft 2871.3 15080.7 8244.7 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1834.73 0.9940 0.0550 0.57151 0.01222 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.261 0.9971 1.0000 0.9975 2706.36 1.000 996.8 11874.1 +Core_Nozz 1.555 0.9999 1.0000 0.9999 862.88 0.824 1179.6 1904.5 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:58 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 426 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 6/ 16/ 1/ 4 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.900 43000.0 0.00 354.59 1542.6 0.7972 1229.82 7.8695 871.64 9.135 1572.6 1538.2 1200.1 + core size:21.64 Q: 192.43 Maximum Thrust: 7713.1 % Thrust: 20.0 Power code: 20.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 354.59 3.984 453.35 108.31 0.0000 1222.96 2.355 389.97 3594.3 0.9000 1.40131 +FS_2 Inlet.Fl_O 354.59 3.964 453.35 108.31 0.0000 1229.11 3.588 440.61 5943.4 0.3797 1.40131 +FS_21 Fan.Fl_O 354.59 4.841 483.30 115.48 0.0000 1039.11 4.254 465.76 4515.2 0.4334 1.40105 +FS_13 Splitter.Fl_O2 314.61 4.841 483.30 115.48 0.0000 921.95 4.174 463.21 3795.6 0.4650 1.40105 +FS_22 Splitter.Fl_O1 39.98 4.841 483.30 115.48 0.0000 117.16 4.569 475.37 719.5 0.2884 1.40105 +FS_23 Duct1.Fl_O 39.98 4.829 483.30 115.48 0.0000 117.45 4.558 475.37 721.3 0.2884 1.40105 +FS_24 LPC.Fl_O 39.98 8.429 584.14 139.66 0.0000 73.97 7.670 568.62 366.0 0.3697 1.39929 +FS_25 Duct2.Fl_O 39.98 8.407 584.14 139.66 0.0000 74.16 7.650 568.62 366.9 0.3697 1.39929 +FS_3 HPC.Fl_O 39.98 36.389 931.57 224.04 0.0000 21.64 33.835 912.90 119.9 0.3257 1.38493 +FS_36 Bld3.Fl_O 36.38 36.389 931.57 224.04 0.0000 19.69 33.835 912.90 109.1 0.3257 1.38493 +FS_4 Burner.Fl_O 36.72 34.387 1572.65 392.15 0.0094 27.33 34.167 1570.08 483.4 0.0980 1.33988 +FS_45 HPT.Fl_O 40.32 12.379 1200.13 293.49 0.0085 72.81 11.654 1181.02 439.1 0.2986 1.36214 +FS_48 Duct3.Fl_O 40.32 12.317 1200.13 293.49 0.0085 73.18 11.596 1181.02 441.4 0.2986 1.36214 +FS_5 LPT.Fl_O 40.32 3.058 855.12 206.44 0.0085 248.81 2.873 840.45 1477.4 0.3014 1.38379 +FS_7 Duct4.Fl_O 40.32 3.027 855.12 206.44 0.0085 251.32 2.930 847.45 2018.9 0.2171 1.38379 +FS_9 Core_Nozz.Fl_O 40.32 3.027 855.12 206.44 0.0085 251.32 2.355 797.41 862.9 0.6127 1.38379 +FS_15 BypBld.Fl_O 314.61 4.841 483.30 115.48 0.0000 921.95 4.174 463.21 3795.6 0.4650 1.40105 +FS_17 Duct5.Fl_O 314.61 4.805 483.30 115.48 0.0000 928.92 4.142 463.21 3824.3 0.4650 1.40105 +FS_19 Byp_Nozz.Fl_O 314.61 4.805 483.30 115.48 0.0000 928.92 2.537 402.54 2706.3 1.0000 1.40105 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1229.11 1.221 0.8916 2653.783 1.0661 0.8947 -3597.6 56.15 23.76 +LPC 117.45 1.745 0.8275 2570.236 1.2086 0.8405 -1367.9 20.78 9.05 +HPC 74.16 4.328 0.8622 6105.397 1.5948 0.8868 -4772.7 40.01 40.64 +HPT 27.33 2.778 0.9165 163.384 1.2707 0.9054 4772.8 +LPT 73.18 4.028 0.9115 71.618 1.4035 0.8943 4965.6 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2356.65 1.154 0.9211 0.673 2.2334 0.5215 1.4369 0.9679 3943.9586 +LPC 125.98 1.228 0.8620 0.702 1.4594 0.9323 3.2631 0.9600 3662.6571 +HPC 176.30 16.385 0.8506 0.960 2.2642 0.4206 0.2163 1.0137 6357.1603 +HPT 30.07 5.185 0.9349 106.709 5.1846 1.4085 0.4249 0.9803 1.5311 +LPT 152.06 5.224 0.9103 88.297 5.2239 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3594.27 9606.2 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 706.74 169.20 12.507 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 706.74 169.20 12.507 +Duct1 0.0025 0.2884 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 706.74 169.20 12.507 +Duct2 0.0025 0.3697 365.99 +Duct3 0.0050 0.2986 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.3014 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.3992 931.57 224.04 36.389 +Duct5 0.0075 0.4650 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 2.1988 931.57 224.04 36.389 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 483.30 115.48 4.841 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 7.8695 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6479.3 3868.8 4772.8 +LP_Shaft 2481.1 10511.6 4965.6 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1572.65 0.9940 0.0550 0.34162 0.00939 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 2.040 0.9976 1.0000 0.9975 2706.36 1.000 981.5 10091.2 +Core_Nozz 1.286 0.9999 1.0000 0.9999 862.88 0.613 844.0 1057.6 + + + + + + ************************************************************************************************************************************ +Date:08/27/13 Time:10:14:58 Model: Rough JT9D Turbofan Performance Model converge = 1 CASE: 427 +Version: NPSS_2.4 Gas Package: GasTbl iter/pass/Jacb/Broy= 10/ 30/ 2/ 7 Run by: tlavelle + + SUMMARY OUTPUT DATA + MN alt dTamb W Fn TSFC Wfuel BPR VTAS OPR T4 T41 T49 + 0.900 43000.0 0.00 317.00 385.7 1.6317 629.27 9.7788 871.64 6.076 1288.4 1263.2 976.0 + core size:22.55 Q: 192.43 Maximum Thrust: 7713.1 % Thrust: 5.0 Power code: 5.0 + + FLOW STATION DATA + W Pt Tt ht FAR Wc Ps Ts Aphy MN gamt +FS_1 Start.Fl_O 317.00 3.984 453.35 108.31 0.0000 1093.32 2.355 389.97 3213.3 0.9000 1.40131 +FS_2 Inlet.Fl_O 317.00 3.964 453.35 108.31 0.0000 1098.82 3.671 443.49 5943.4 0.3329 1.40131 +FS_21 Fan.Fl_O 317.00 4.362 469.26 112.12 0.0000 1015.74 3.861 453.14 4515.2 0.4210 1.40120 +FS_13 Splitter.Fl_O2 287.59 4.362 469.26 112.12 0.0000 921.50 3.762 449.77 3795.6 0.4646 1.40120 +FS_22 Splitter.Fl_O1 29.41 4.362 469.26 112.12 0.0000 94.24 4.208 464.42 719.5 0.2277 1.40120 +FS_23 Duct1.Fl_O 29.41 4.352 469.26 112.12 0.0000 94.47 4.197 464.42 721.3 0.2277 1.40120 +FS_24 LPC.Fl_O 29.41 6.470 538.59 128.73 0.0000 68.07 5.986 526.74 366.0 0.3353 1.40014 +FS_25 Duct2.Fl_O 29.41 6.454 538.59 128.73 0.0000 68.24 5.971 526.74 366.9 0.3353 1.40014 +FS_3 HPC.Fl_O 29.41 24.205 826.99 198.39 0.0000 22.55 22.347 808.62 119.9 0.3407 1.39066 +FS_36 Bld3.Fl_O 26.76 24.205 826.99 198.39 0.0000 20.52 22.347 808.62 109.1 0.3407 1.39066 +FS_4 Burner.Fl_O 26.94 22.874 1288.45 315.82 0.0065 27.28 22.728 1286.27 483.4 0.0972 1.35797 +FS_45 HPT.Fl_O 29.58 8.135 975.99 236.06 0.0059 73.31 7.653 959.73 439.1 0.2990 1.37816 +FS_48 Duct3.Fl_O 29.58 8.095 975.99 236.06 0.0059 73.68 7.614 959.73 441.4 0.2990 1.37816 +FS_5 LPT.Fl_O 29.58 2.693 743.62 178.75 0.0059 193.33 2.597 736.12 1477.4 0.2284 1.39088 +FS_7 Duct4.Fl_O 29.58 2.666 743.62 178.75 0.0059 195.29 2.615 739.62 2018.9 0.1664 1.39088 +FS_9 Core_Nozz.Fl_O 29.58 2.666 743.62 178.75 0.0059 195.29 2.355 718.13 862.9 0.4259 1.39088 +FS_15 BypBld.Fl_O 287.59 4.362 469.26 112.12 0.0000 921.50 3.762 449.77 3795.6 0.4646 1.40120 +FS_17 Duct5.Fl_O 287.59 4.330 469.26 112.12 0.0000 928.47 3.734 449.77 3824.3 0.4646 1.40120 +FS_19 Byp_Nozz.Fl_O 287.59 4.330 469.26 112.12 0.0000 928.47 2.355 394.14 2706.4 0.9746 1.40120 + +TURBOMACHINERY PERFORMANCE DATA + Wc PR eff Nc TR efPoly pwr SMN SMW +Fan 1098.82 1.101 0.7932 2146.115 1.0351 0.7961 -1707.5 78.43 26.39 +LPC 94.47 1.487 0.8134 2109.434 1.1477 0.8237 -691.3 23.29 7.11 +HPC 68.24 3.750 0.8508 5997.476 1.5355 0.8754 -2898.8 51.92 52.98 +HPT 27.28 2.812 0.9181 170.262 1.2865 0.9068 2898.8 +LPT 73.68 3.006 0.9033 64.225 1.3125 0.8888 2398.8 + +TURBOMACHINERY MAP DATA + WcMap PRmap effMap NcMap R/Parm s_WcDes s_PRdes s_effDes s_NcDes +Fan 2106.84 1.070 0.8195 0.544 2.6111 0.5215 1.4369 0.9679 3943.9586 +LPC 101.33 1.149 0.8473 0.576 1.4654 0.9323 3.2631 0.9600 3662.6571 +HPC 162.23 13.715 0.8394 0.943 2.3928 0.4206 0.2163 1.0137 6357.1603 +HPT 30.01 5.264 0.9365 111.201 5.2641 1.4085 0.4249 0.9803 1.5311 +LPT 153.10 3.798 0.9022 79.181 3.7985 0.7458 0.7169 1.0013 0.8111 + +===INLETS==== eRam Afs Fram +Inlet 0.9950 3213.26 8587.9 BLEEDS - interstg Wb/Win BldWk BldP W Tt ht Pt + CstmrBld HPC.C> 0.0000 0.3500 0.1465 0.0000 640.07 153.11 9.055 +====DUCTS==== dPnorm MN Aphy C_LPTexit HPC.C> 0.0000 0.3500 0.1465 0.0000 640.07 153.11 9.055 +Duct1 0.0025 0.2277 719.54 C_LPTinlt HPC.C> 0.0000 0.3500 0.1465 0.0000 640.07 153.11 9.055 +Duct2 0.0025 0.3353 365.99 +Duct3 0.0050 0.2990 439.14 BLEEDS - output Wb/Win hscale Pscale W Tt ht Pt +Duct4 0.0100 0.2284 1477.35 C_HPTexit Bld3.> 0.0350 1.0000 1.0000 1.0293 826.99 198.39 24.205 +Duct5 0.0075 0.4646 3795.63 C_HPTinlt Bld3.> 0.0550 1.0000 1.0000 1.6175 826.99 198.39 24.205 + Duct5Lk BypBl> 0.0000 1.0000 1.0000 0.0000 469.26 112.12 4.362 +==SPLITTERS== BPR dP/P 1 dP/P 2 +Splitter 9.7788 0.0000 0.0000 + +===SHAFTS==== Nmech trq in pwr in +HP_Shaft 6111.5 2491.2 2898.8 +LP_Shaft 2006.4 6279.2 2398.8 + + +===BURNERS=== TtOut eff dPnorm Wfuel FAR +Burner 1288.45 0.9940 0.0550 0.17480 0.00653 + + +===NOZZLES=== PR Cfg CdTh Cv Ath MNth Vact Fg +Byp_Nozz 1.839 0.9975 1.0000 0.9975 2706.36 0.975 946.5 8460.7 +Core_Nozz 1.132 0.9999 1.0000 0.9999 862.88 0.426 557.8 512.8 + + + + + diff --git a/Turbofan/Turbofan.mdl.py b/Turbofan/Turbofan.mdl.py new file mode 100644 index 0000000..8c549bb --- /dev/null +++ b/Turbofan/Turbofan.mdl.py @@ -0,0 +1,230 @@ +from openmdao.main.api import Assembly, Component +from openmdao.lib.drivers.api import DOEdriver +from openmdao.lib.doegenerators.api import FullFactorial +from openmdao.lib.casehandlers.api import DumpCaseRecorder +from openmdao.lib.datatypes.api import Float +from openmdao.lib.drivers.api import BroydenSolver + +from pycycle.api import (FlightConditions, Inlet, SplitterBPR, CompressorRline, Duct, + Burner, TurbinePRmap, NozzleConvergent, Shaft, Nmech, FlowStationVar) + +class Turbofan(Assembly): + + def configure(self): + + #component definition + fc = self.add('fc', FlightConditions()) + fc.alt = 34000 + fc.MN = .8 + fc.Wout = 674.2 + + inlet = self.add('inlet', Inlet() ) + inlet.ram_recovery = .995 + + fan = self.add('fan', CompressorRline()) + fan.eff = .867 + fan.PR = 1.645 + + split = self.add( 'split', SplitterBPR()) + split.BPR = 5.041 + + bypduct = self.add( 'bypduct', Duct()) + bypduct.dPqP = .01 + + bypnoz = self.add( 'bypnoz', NozzleConvergent()) + bypnoz.cfg = .9962 + self.connect('fc.Fl_O.Ps', 'bypnoz.PsExh') + + duct1 = self.add( 'duct1', Duct()) + duct1.dPqP = .0025 + + lpc = self.add( 'lpc', CompressorRline()) + lpc.eff = .868 + lpc.PR = 2.488 + + duct2 = self.add( 'duct2', Duct()) + duct2.dPqP = .0025 + + hpc = self.add( 'hpc', CompressorRline()) + hpc.eff = .865 + hpc.PR = 5.609 + hpc.Wfrac1=.055 + hpc.hfrac1=1 + hpc.Pfrac1=1 + hpc.Wfrac2=.035 + hpc.hfrac2=1 + hpc.Pfrac2=1 + + + burner = self.add( 'burner', Burner()) + burner.ID_fuel = 3 + burner.hFuel = -1200 + burner.Wfuel = 1.899 + burner.dPqP = .055 + + + hpt = self.add( 'hpt', TurbinePRmap()) + hpt.eff = .9133 + hpt.PR = 2.670 + + duct3 = self.add( 'duct3', Duct()) + duct3.dPqP = .005 + + lpt = self.add( 'lpt', TurbinePRmap()) + lpt.eff = .9323 + lpt.PR = 4.886 + + duct4 = self.add( 'duct4', Duct()) + duct4.dPqP = .01 + + prinoz = self.add( 'prinoz', NozzleConvergent()) + prinoz.cfg = .9978 + self.connect('fc.Fl_O.Ps', 'prinoz.PsExh') + + hpshaft = self.add( 'hpshaft', Shaft()) + hpspeed = self.add( 'hpspeed', Nmech()) + hpspeed.Nmech = 8000 + + lpshaft = self.add( 'lpshaft', Shaft() ) + lpspeed = self.add( 'lpspeed', Nmech()) + hpspeed.Nmech = 2000 + + #inter component connections + self.connect( 'fc.Fl_O', 'inlet.Fl_I' ) + self.connect( 'inlet.Fl_O', 'fan.Fl_I' ) + self.connect( 'fan.Fl_O', 'split.Fl_I' ) + self.connect( 'split.Fl_O2', 'bypduct.Fl_I' ) + self.connect( 'bypduct.Fl_O', 'bypnoz.Fl_I' ) + self.connect( 'split.Fl_O1', 'duct1.Fl_I' ) + self.connect( 'duct1.Fl_O', 'lpc.Fl_I' ) + self.connect( 'lpc.Fl_O', 'duct2.Fl_I' ) + self.connect( 'duct2.Fl_O', 'hpc.Fl_I' ) + self.connect( 'hpc.Fl_O', 'burner.Fl_I' ) + self.connect( 'burner.Fl_O', 'hpt.Fl_I') + self.connect( 'hpt.Fl_O', 'duct3.Fl_I' ) + self.connect( 'duct3.Fl_O', 'lpt.Fl_I' ) + self.connect( 'lpt.Fl_O', 'duct4.Fl_I' ) + self.connect( 'duct4.Fl_O', 'prinoz.Fl_I' ) + self.connect( 'hpc.Fl_bld1', 'hpt.Fl_bld1' ) + self.connect( 'hpc.Fl_bld2', 'hpt.Fl_bld2' ) + + self.connect( 'hpspeed.Nmech', ['hpshaft.Nmech','hpc.Nmech', 'hpt.Nmech'] ) + self.connect( 'lpspeed.Nmech', ['lpshaft.Nmech','fan.Nmech','lpc.Nmech', 'lpt.Nmech'] ) + self.connect( 'hpc.trq', 'hpshaft.trq1' ) + self.connect( 'hpt.trq', 'hpshaft.trq2' ) + self.connect( 'fan.trq', 'lpshaft.trq1' ) + self.connect( 'lpc.trq', 'lpshaft.trq2' ) + self.connect( 'lpt.trq', 'lpshaft.trq3' ) + + hpspeed.Nmech = 8000 + lpspeed.Nmech = 2000 + + driver = self.driver + comp_list = [ + 'inlet', + 'fan', + 'split', + 'bypduct', + 'bypnoz', + 'lpc', + 'hpc', + 'burner', + 'hpt', + 'lpt', + 'prinoz', + 'hpshaft', + 'lpshaft', + 'fc' + ] + + solver = self.add('solver',BroydenSolver()) + + solver.workflow.add( comp_list ) + driver.workflow.add('solver') + +from collections import OrderedDict +TF1 = Turbofan() + +TF1.run() + +#TF1.run() + +print 'high shaft torques' +print TF1.hpshaft.trqNet +print TF1.hpshaft.trq1 +print TF1.hpshaft.trq2 + +print 'Low shaft torques' +print TF1.lpshaft.trqNet +print TF1.lpshaft.trq1 +print TF1.lpshaft.trq2 +print TF1.lpshaft.trq3 + +print TF1.hpc.trq +print TF1.hpt.trq + + +print 'fc' +print TF1.fc.Fl_O.Pt +print TF1.fc.Fl_O.Ps +print TF1.fc.Fl_O.Tt +print TF1.fc.Fl_O.W + +print 'inlet' +print TF1.inlet.Fl_O.Pt +print TF1.inlet.Fl_O.Tt +print TF1.inlet.Fl_O.W + +print 'split' +print TF1.split.Fl_O1.Pt +print TF1.split.Fl_O1.Tt +print TF1.split.Fl_O1.W + +print 'split' +print TF1.split.Fl_O2.Pt +print TF1.split.Fl_O2.Tt +print TF1.split.Fl_O2.W + +print 'bypduct' +print TF1.bypduct.Fl_O.Pt +print TF1.bypduct.Fl_O.Tt +print TF1.bypduct.Fl_O.W + +print 'lpc' +print TF1.lpc.Fl_O.Pt +print TF1.lpc.Fl_O.Tt +print TF1.lpc.Fl_O.W + +print 'hpc' +print TF1.hpc.Fl_O.Pt +print TF1.hpc.Fl_O.Tt +print TF1.hpc.Fl_O.W + +print TF1.hpc.Fl_bld1.Pt +print TF1.hpc.Fl_bld1.Tt +print TF1.hpc.Fl_bld1.W + +print TF1.hpc.Fl_bld2.Pt +print TF1.hpc.Fl_bld2.Tt +print TF1.hpc.Fl_bld2.W + +print 'burner' +print TF1.burner.Fl_O.Pt +print TF1.burner.Fl_O.Tt +print TF1.burner.Fl_O.W + +print 'hpt' +print TF1.hpt.Fl_I.ht +print TF1.hpt.Fl_O.Pt +print TF1.hpt.Fl_O.Tt +print TF1.hpt.Fl_O.W + +print 'lpt' +print TF1.lpt.Fl_O.Pt +print TF1.lpt.Fl_O.Tt +print TF1.lpt.Fl_O.W + +print TF1.hpshaft.trqNet +print TF1.burner.Wfuel/(TF1.prinoz.Fg+TF1.bypnoz.Fg-TF1.fc.Fram)*3600. + + diff --git a/Turbofan/api.py b/Turbofan/api.py new file mode 100644 index 0000000..bca07a5 --- /dev/null +++ b/Turbofan/api.py @@ -0,0 +1,13 @@ +from splitterT import SplitterBPR +from start import FlowStart, FlowStartStatic +from inletT import Inlet +from nozzleT import Nozzle +from ductT import Duct +from compressor import Compressor +from heat_exchanger import HeatExchanger +from cycle_component import CycleComponent +from flowstation import FlowStation, FlowStationVar + +from flightconditions import FlightConditions +from burner import Burner +from turbine import Turbine \ No newline at end of file diff --git a/src/pycycle/api.py b/src/pycycle/api.py index 792e729..58af69e 100644 --- a/src/pycycle/api.py +++ b/src/pycycle/api.py @@ -1,9 +1,26 @@ -from splitter import SplitterBPR, SplitterW -from start import FlowStart, FlowStartStatic -from inlet import Inlet -from nozzle import Nozzle -from duct import Duct +#------------------------------------------------- +# load in flowstation/thermo info +#------------------------------------------------- +from flowstation import FlowStation, FlowStationVar + +#------------------------------------------------- +# load in component info +#------------------------------------------------- +from burner import Burner from compressor import Compressor +from compressor_rline import CompressorRline +from duct import Duct +from flightconditions import FlightConditions from heat_exchanger import HeatExchanger +from inlet import Inlet +from nozzle_convergent import NozzleConvergent +from nozzle import Nozzle +from shaft import Shaft, Nmech +from splitter_bpr import SplitterBPR +from start import FlowStart +from turbine_prmap import TurbinePRmap + from cycle_component import CycleComponent -from flowstation import FlowStation, FlowStationVar + + + diff --git a/src/pycycle/burner.py b/src/pycycle/burner.py new file mode 100644 index 0000000..6a1fccd --- /dev/null +++ b/src/pycycle/burner.py @@ -0,0 +1,43 @@ +from openmdao.main.api import Component +from openmdao.lib.datatypes.api import Float, VarTree, Int + +from pycycle.flowstation import FlowStation, FlowStationVar +from pycycle.cycle_component import CycleComponent + + +class Burner(CycleComponent): + """The burner takes mixes one cantera flow with another at cantera reactant + and user supplied enthalpy. If this cantera reactant is fuel, burning will + occur""" + + #IO Variables + ID_fuel = Int( 0, iotype="in", desc="reactant id number of the flow being mixed (fuel being burned)", units = "lbm/s" ) + dPqP = Float( 0.0, iotype="in", desc="pressure differential as a fraction of incomming pressure", units = "lbf/inch**2" ) + hFuel = Float( 0.0, iotype="in", desc="enthalpy of incoming fuel", units = "Btu/lbm" ) + Wfuel = Float( 0.0, iotype="in", desc="fuel weight flow", units = "lbm/s" ) + + #flow connections + Fl_I = FlowStationVar( iotype="in", desc="incoming flow stream to the burner", copy=None ) + Fl_O = FlowStationVar( iotype="out", desc="flow stream leaving the burner", copy=None ) + + + def execute(self): + Fl_I = self.Fl_I + Fl_O = self.Fl_O + + #set the exit station to the inlet as a starting point + Fl_O.copy_from( Fl_I ) + + #mix the new reactant with the flow + Fl_O.burn( self.ID_fuel, self.Wfuel, self.hFuel ) + + #apply the pressure drop + Fl_O.setTotal_hP( Fl_O.ht, Fl_O.Pt*(1-self.dPqP) ) + + +if __name__ == "__main__": + from openmdao.main.api import set_as_top + + c = set_as_top(Burner()) + c.run() + diff --git a/src/pycycle/compressor_rline.py b/src/pycycle/compressor_rline.py new file mode 100644 index 0000000..31848b5 --- /dev/null +++ b/src/pycycle/compressor_rline.py @@ -0,0 +1,92 @@ +import math + +from openmdao.main.api import Component +from openmdao.lib.datatypes.api import Float, VarTree, Event + +from pycycle.flowstation import FlowStation, FlowStationVar, GAS_CONSTANT +from pycycle.cycle_component import CycleComponent + + + +class CompressorRline(CycleComponent): + """Axial Compressor performance calculations""" + + + Fl_I = FlowStationVar(iotype="in", desc="incoming air stream to compressor", copy=None) + + PR = Float(iotype="out", desc="pressure ratio at operating conditions") + eff = Float(iotype="out", desc="adiabatic efficiency at the operating condition") + eff_poly = Float(iotype="out", desc="polytropic efficiency at the operating condition") + pwr = Float(iotype="out", units="hp", desc="power required to run the compressor at the operating condition") + tip_radius = Float(iotype="out", units="inch", desc="radius at the tip of the compressor") + hub_radius = Float(iotype="out", units="inch", desc="radius at the tip of the compressor") + Wfrac1 = Float(iotype="in", units="lbm/s", desc="Bleed 1 flow fraction") + hfrac1 = Float(iotype="in", units="Btu/lbm", desc="Bleed 1 enthalpy fraction") + Pfrac1 = Float(iotype="in", units="lbf/inch**2", desc="Bleed 1 pressure fraction") + Wfrac2 = Float(iotype="in", units="lbm/s", desc="Bleed 2 flow fraction") + hfrac2 = Float(iotype="in", units="Btu/lbm", desc="Bleed 2 enthalpy fraction") + Pfrac2 = Float(iotype="in", units="lbf/inch**2", desc="Bleed 2 pressure fraction") + + Nmech = Float( 1000., iotype="in", desc="Mechanical speed") + trq = Float( 0., iotype="out", desc="trq") + + Fl_O = FlowStationVar( iotype="out",desc="outgoing air stream from compressor", copy=None ) + Fl_bld1 = FlowStationVar(iotype="out", desc="first bleed port", copy=None ) + Fl_bld2 = FlowStationVar(iotype="out", desc="second bleed port", copy=None ) + + + def execute(self): + + Fl_I = self.Fl_I + Fl_O = self.Fl_O + Fl_O.copy_from( Fl_I ) + Fl_bld1 = self.Fl_bld1 + Fl_bld1.copy_from( Fl_I ) + Fl_bld2 = self.Fl_bld2 + Fl_bld2.copy_from( Fl_I ) + + FO_ideal = FlowStation() + FO_ideal.copy_from( Fl_I ) + + PtOut = Fl_I.Pt*self.PR + FO_ideal.setTotalSP( Fl_I.s,PtOut ) + + htOut = Fl_I.ht + ( FO_ideal.ht - Fl_I.ht )/self.eff + + # set the exit conditions to knowm enthalpy and pressure + Fl_O.setTotalTP( 518, 15 ) + Fl_O.setTotal_hP( htOut, PtOut ) + + # set the condtions for bleed 1 + Wbleed1 = self.Wfrac1*Fl_I.W + htBleed1 = Fl_I.ht+ self.hfrac1*( Fl_O.ht - Fl_I.ht ) + PtBleed1 = Fl_I.Pt + self.Pfrac1*( Fl_O.Pt - Fl_I.Pt ) + Fl_bld1.setTotal_hP( htBleed1,PtBleed1 ) + Fl_bld1.W = Wbleed1 + + + # set the conditions for bleed 2 + Wbleed2 = self.Wfrac2*Fl_I.W; + htBleed2 = Fl_I.ht+ self.hfrac2*( Fl_O.ht - Fl_I.ht) + PtBleed2 = Fl_I.Pt + self.Pfrac2*( Fl_O.Pt - Fl_I.Pt ) + Fl_bld2.setTotal_hP( htBleed2,PtBleed2 ) + Fl_bld2.W = Wbleed2 + + # subtract the bleed flow from the exit flow + Wout = Fl_I.W - Fl_bld1.W - Fl_bld2.W + Fl_O.W = Wout + + + # determine the power + self.pwr = Fl_I.W * ( Fl_I.ht - Fl_O.ht ) * 1.4148; + self.pwr = self.pwr - Fl_bld1.W*(Fl_bld1.ht-Fl_O.ht)*1.4148 - Fl_bld2.W*(Fl_bld2.ht-Fl_O.ht)*1.4148 + + self.trq = 550. * self.pwr / self.Nmech; + +if __name__ == "__main__": + from openmdao.main.api import set_as_top + + c = set_as_top(CompressorRline()) + c.run() + + diff --git a/src/pycycle/duct.py b/src/pycycle/duct.py index f2ddeb8..4be65cb 100644 --- a/src/pycycle/duct.py +++ b/src/pycycle/duct.py @@ -6,38 +6,31 @@ class Duct(CycleComponent): - """The inlet takes in air at a given flow rate and mach number, and diffuses it down - to a slower mach number and larger area""" + """The duct allows the user to apply a pressure drop to the stream""" - dPqP = Float(0.0, iotype="in", desc="pressure differential as a fraction of incomming pressure") - Q_dot = Float(0.0, iotype="in", units="Btu/s", desc="heat flow rate into (positive) or out of (negative) the air") - MNexit_des = Float(.6, iotype="in", desc="mach number at the exit of the inlet") + dPqP = Float( 0.0, iotype="in", desc="pressure differential as a fraction of incomming pressure" ) - Fl_I = FlowStationVar(iotype="in", desc="incoming air stream to compressor", copy=None) - Fl_O = FlowStationVar(iotype="out", desc="outgoing air stream from compressor", copy=None) + Fl_I = FlowStationVar( iotype="in", desc="incoming air stream to compressor", copy=None ) + Fl_O = FlowStationVar( iotype="out", desc="outgoing air stream from compressor", copy=None ) - def execute(self): + def execute( self ): Fl_I = self.Fl_I Fl_O = self.Fl_O + + # pass the flow information along + Fl_O.copy_from( Fl_I ) + + #determine the exit pressure + Pt_out = Fl_I.Pt*( 1 - self.dPqP ) - Pt_out = Fl_I.Pt*(1-self.dPqP) - q = self.Q_dot/Fl_I.W - Fl_O.setTotal_hP(Fl_I.ht+q, Pt_out) - Fl_O.W = Fl_I.W - - if self.run_design: - Fl_O.Mach = self.MNexit_des - self._exit_area_des = Fl_O.area - else: - Fl_O.area = self._exit_area_des - - + # set the exit conditions based on the new enthalpy and pressure + Fl_O.setTotal_hP( Fl_I.ht, Pt_out ) if __name__ == "__main__": from openmdao.main.api import set_as_top - c = set_as_top(Inlet()) + c = set_as_top(Duct()) c.run() diff --git a/src/pycycle/flightconditions.py b/src/pycycle/flightconditions.py new file mode 100644 index 0000000..aeadc93 --- /dev/null +++ b/src/pycycle/flightconditions.py @@ -0,0 +1,76 @@ +import math +from openmdao.main.api import Component +from openmdao.lib.datatypes.api import Float, VarTree + +from pycycle.flowstation import FlowStationVar, FlowStation +from pycycle.cycle_component import CycleComponent + + +class FlightConditions(CycleComponent): + """This element determines the flow conditions based on input altitude, Mach number, + and dTs""" + + alt = Float( 0., iotype="in", desc="input altitude", units="ft" ) + MN = Float( 0., iotype="in", desc="input Mach number" ) + dTs = Float( 0., iotype="in", desc="input ambient altitude delta", units="R" ) + WAR = Float( 0., iotype="in", desc="Water to air ratio" ) + Wout = Float( 0., iotype="in", desc="Weight flow", units="lbm/s" ) + Fram = Float( 0., iotype="in", desc="Ram drag", units="lbf" ) + + Fl_O = FlowStationVar(iotype="out", desc="outgoing air stream from compressor", copy=None) + + def execute(self): + + Fl_O = self.Fl_O; + + # data that describes the atmosphere + REARTH = 6369.0 + GMR = 34.163195 + htab = ( 0.0, 11.0, 20.0, 32.0, 47.0, 51.0, 71.0, 84.852 ) + ttab = [ 288.15, 216.65, 216.65, 228.65, 270.65, 270.65, 214.65, 186.946 ] + ptab = [ 1.0, 2.2336110E-1, 5.4032950E-2, 8.5666784E-3, 1.0945601E-3, 6.6063531E-4, 3.9046834E-5, 3.68501E-6 ] + gtab = [ -6.5, 0.0, 1.0, 2.8, 0, -2.8, -2.0, 0.0 ] + + Ts=0 + Ps=0 + + # calculate geopotential altitude + h = self.alt/3280.84*REARTH/(self.alt/3280.84+REARTH) + + # determine where in the h table we are + i = 0 + while ( h >= htab[i] ): + i = i + 1 + + # grab the values from the table + i = i - 1 + tbase = ttab[i]*9/5 + tgrad = gtab[i] + deltah=h-htab[i] + + # determine Ps and Ts + Ts=tbase+tgrad*deltah*9/5 + if (tgrad == 0. ): + Ps = ptab[i]*math.exp(-GMR*deltah/tbase*9./5.)*14.696 + else: + Ps = ptab[i]*((tbase/Ts)**(GMR/tgrad))*14.696 + Ts = self.dTs + Ts + + # set the exit conditions in the port + Fl_O.W = self.Wout + Fl_O.setWAR( self.WAR ) + if ( self.MN > 0 ): + Fl_O.setStaticTsPsMN( Ts, Ps, self.MN ) + else: + Fl_O.setTotalTP( Ts, Ps ) + Fl_O.Mach = 0. + + #determine the ram drag + self.Fram = Fl_O.Vflow*Fl_O.W/32.174 + +if __name__ == "__main__": + from openmdao.main.api import set_as_top + + c = set_as_top(FlightConditions()) + c.run() + diff --git a/src/pycycle/flowstation.py b/src/pycycle/flowstation.py index 77dfc34..cb4ddda 100644 --- a/src/pycycle/flowstation.py +++ b/src/pycycle/flowstation.py @@ -14,9 +14,9 @@ #secant solver with a limit on overall step size def secant(func, x0, TOL=1e-7, x_min=1e15, x_max=1e15, maxdx = 1e15 ): if x0 >= 0: - x1 = x0*(1 + 1e-2) + 1e-2 + x1 = x0*(1 + 1e-4) + 1e-4 else: - x1 = x0*(1 + 1e-2) - 1e-2 + x1 = x0*(1 + 1e-4) - 1e-4 f1, f = func(x1), func(x0) if (abs(f) > abs(f1)): x1, x0 = x0, x1 @@ -54,8 +54,8 @@ class FlowStation(VariableTree): numreacts = 0 ht=Float(0.0, desc='total enthalpy', units='Btu/lbm') - Tt=Float(0.0, desc='total temperature', units='degR') - Pt=Float(0.0, desc='total pressure', units='lbf/inch**2') + Tt=Float(518.67, desc='total temperature', units='degR') + Pt=Float(14.696, desc='total pressure', units='lbf/inch**2') rhot=Float(0.0, desc='total density', units='lbm/ft**3') gamt=Float(0.0, desc='total gamma') Cp = Float(0.0, desc='Specific heat at constant pressure', units='Btu/(lbm*degR)') @@ -65,8 +65,8 @@ class FlowStation(VariableTree): FAR =Float(0.0, desc='fuel to air ratio') WAR =Float(0.0, desc='water to air ratio') hs=Float(0.0, desc='static enthalpy', units='Btu/lbm') - Ts=Float(0.0, desc='static temperature', units='degR') - Ps=Float(0.0, desc='static pressure', units='lbf/inch**2') + Ts=Float(518.67, desc='static temperature', units='degR') + Ps=Float(14.696, desc='static pressure', units='lbf/inch**2') rhos=Float(0.0, desc='static density', units='lbm/ft**3') gams=Float(0.0, desc='static gamma') Vflow =Float(0.0, desc='Velocity', units='ft/s') @@ -123,11 +123,22 @@ def _W_changed(self): self._trigger=0 #trigger action on Mach - def _Mach_changed(self): + def _Mach_changed(self): if self._trigger == 0: self._trigger=1 self._mach_or_area=1 - self.setStatic() + if self.Mach == 0: + self.hs = self.ht + self.Ts = self.Tt + self.Ps = self.Pt + self.rhos = self.rhot + self.gams = self.gamt + self.Vflow = 0 + self.Vsonic = 0 + self.Mach = 0 + self.area = 0 + else: + self.setStatic() self._trigger=0 #trigger action on area @@ -240,7 +251,7 @@ def setTotal_hP(self, hin, Pin): self._trigger=1 self.ht=hin self.Pt=Pin - def f(Tt): + def f(Tt): self._flow.set(T=Tt*5./9., P=Pin*6894.75729) self._flow.equilibrate('TP') return hin - self._flow.enthalpy_mass()*0.0004302099943161011 @@ -330,14 +341,15 @@ def f(Ps): return self.Mach - mach_target Ps_guess = self.Pt*(1 + (self.gamt-1)/2*mach_target**2)**(self.gamt/(1-self.gamt))*.9 - secant(f, Ps_guess, x_min=0, x_max=self.Pt) - + secant(f, Ps_guess, x_min=0, x_max=self.Pt*.99) + #set the statics based on pressure def setStaticPs(self): def f(Ts): - self._setComp() + self._setComp() + self._flow.set(T=Ts*5./9., P=self.Ps*6894.75729 ) self._flow.equilibrate('TP') return self.s - self._flow.entropy_mass()*0.000238845896627 @@ -404,20 +416,36 @@ def setStatic(self): #set the statics based on Ts, Ps, and MN #UPDGRAEDE TO USE LOOPS def setStaticTsPsMN(self, Ts, Ps, MN): - self._trigger=1 + + self._setComp() + self._trigger=1 + self.Ts=Ts + self.Ps=Ps + self._flow.set(T=Ts*5./9., P=Ps*6894.75729) + self._flow.equilibrate('TP') + self.hs=self._flow.enthalpy_mass()*0.0004302099943161011 + self.s=self._flow.entropy_mass()*0.000238845896627 + self.rhos=self._flow.density()*.0624 + self.Ts=Ts + self.Cp = self._flow.cp_mass()*2.388459e-4 + self.Cv = self._flow.cv_mass()*2.388459e-4 + self.gams=self.Cp/self.Cv + MMW = self._flow.meanMolecularWeight() + Vson = math.sqrt( self.gams*self.Ts*1544/MMW*32.174 ) + Vflow = MN*Vson; + ht = self.hs + (Vflow)**2/( 778.169 * 32.1740 * 2 ); - self.Tt=Ts*(1+(self.gamt - 1) /2.* MN**2) - self.Pt=Ps*(1+(self.gamt - 1) /2.* MN**2)**(self.gamt /(self.gamt -1)) - self.setTotalTP(self.Tt, self.Pt) + Tt=Ts*(1+(self.gams - 1) /2.* MN**2) + Pt=Ps*(1+(self.gams - 1) /2.* MN**2)**(self.gams /(self.gams -1)) - #do this once more beacause gamt changed... very crude iteration - self.Tt=Ts*(1+(self.gamt - 1) /2.* MN**2) - self.Pt=Ps*(1+(self.gamt - 1) /2.* MN**2)**(self.gamt /(self.gamt -1)) - self.setTotalTP(self.Tt, self.Pt) + def f(Pti): + self.Pt = Pti + self.setTotalSP(self.s, Pti) + return ht - self.ht + secant(f, Pt, x_min=0, x_max=Pt*2 ) - self._trigger=1 + self.Mach=MN - self.setStaticMach() self.area= self.W / (self.rhos * self.Vflow)*144. self._trigger=0 diff --git a/src/pycycle/inlet.py b/src/pycycle/inlet.py index 8f8b15a..c03bd22 100644 --- a/src/pycycle/inlet.py +++ b/src/pycycle/inlet.py @@ -6,36 +6,25 @@ class Inlet(CycleComponent): - """The inlet takes in air at a given flow rate and mach number, and diffuses it down - to a slower mach number and larger area""" + """This simple inlet applies a ram recovery (pressure drop) to the flow""" - ram_recovery = Float(1.000, iotype="in", desc="fraction of the total pressure retained") - MNexit_des = Float(.6, iotype="in", desc="mach number at the exit of the inlet") - - A_capture = Float(iotype="in", desc="area at the entrance plane to the inlet", units="inch**2") - Fl_I = FlowStationVar(iotype="in", desc="incoming air stream to compressor", copy=None) - Fl_O = FlowStationVar(iotype="out", desc="outgoing air stream from compressor", copy=None) - F_ram = Float(iotype="out", desc="ram drag from the inlet", units="lbf") + ram_recovery = Float( 1.000, iotype="in", desc="fraction of the total pressure retained" ) + + Fl_I = FlowStationVar( iotype="in", desc="incoming air stream to compressor", copy=None ) + Fl_O = FlowStationVar( iotype="out", desc="outgoing air stream from compressor", copy=None ) + def execute(self): Fl_I = self.Fl_I Fl_O = self.Fl_O - + Fl_O.copy_from( Fl_I ) + + #determine the exit pressure Pt_out = Fl_I.Pt*self.ram_recovery - Fl_O.setTotalTP(Fl_I.Tt, Pt_out) - Fl_O.W = Fl_I.W - - self.F_ram = Fl_I.W*Fl_I.Vflow/32.174 #lbf - - if self.run_design: - Fl_O.Mach = self.MNexit_des - self._exit_area_des = Fl_O.area - self.A_capture = Fl_I.area - else: - Fl_O.area = self._exit_area_des - - + + #set the conditions in the exit port + Fl_O.setTotal_hP(Fl_I.ht, Pt_out) if __name__ == "__main__": from openmdao.main.api import set_as_top diff --git a/src/pycycle/nozzle_convergent.py b/src/pycycle/nozzle_convergent.py new file mode 100644 index 0000000..fb78f93 --- /dev/null +++ b/src/pycycle/nozzle_convergent.py @@ -0,0 +1,46 @@ +from openmdao.main.api import Component +from openmdao.lib.datatypes.api import Float, VarTree, Enum + +from pycycle.flowstation import FlowStationVar, FlowStation +from pycycle.cycle_component import CycleComponent + + + +class NozzleConvergent(CycleComponent): + + PsExh = Float( 0., iotype="in", desc="Exhaust static pressure", units="lbf/inch**2" ) + Ath = Float( 0., iotype="in", desc="Nozzle throat area", units="inch**2" ) + Cfg = Float( 1., iotype="in", desc="Coefficient on gross thrust" ) + Fg = Float( 0., iotype="in", desc="Gross Thrust", units="lbf" ) + + Fl_I = FlowStationVar( iotype="in", desc="incoming air stream to nozzle", copy=None ) + Fl_Th = FlowStationVar( iotype="in", desc="Nozzle throat conditions", copy=None ) + + def execute(self): + + # set the throat conditions based on MN + Fl_I= self.Fl_I + Fl_Th = self.Fl_Th + Fl_Th.copy_from( Fl_I ) + Fl_Th.Ps = self.PsExh; + + # determine is the exhaust pressure chokes the nozzle + if Fl_Th.Mach > 1.0: + # static pressur results in MN > 1 Nozzle is choked + # set MN to 1 + Fl_Th.MN = 1 + Ath = Fl_Th.W / ( Fl_Th.rhos * Fl_Th.Vflow)*144.; + else: + #nozzle not choked, run to static pressure + print self.PsExh + Ath = Fl_Th.W / ( Fl_Th.rhos * Fl_Th.Vflow )*144.; + + #calculate gross thrust + self.Fg = ( Fl_Th.W / 32.174 ) * Fl_Th.Vflow + ( Fl_Th.Ps - self.PsExh ) * Fl_Th.area*self.Cfg + + +if __name__ == "__main__": + from openmdao.main.api import set_as_top + + c = set_as_top(NozzleConvergent()) + c.run() diff --git a/src/pycycle/shaft.py b/src/pycycle/shaft.py new file mode 100644 index 0000000..3df7257 --- /dev/null +++ b/src/pycycle/shaft.py @@ -0,0 +1,36 @@ +from openmdao.main.api import Component +from openmdao.lib.datatypes.api import Float, VarTree + +from pycycle.flowstation import FlowStation, FlowStationVar +from pycycle.cycle_component import CycleComponent + + +class Shaft(CycleComponent): + """This componet serves as the torque balancing part of the shaft element""" + + Nmech = Float( 0.0, iotype="in", desc="pressure differential as a fraction of incomming pressure", units='rpm' ) + + trq1 = Float( 0.0, iotype="in", desc="pressure differential as a fraction of incomming pressure", units='ft*lbf' ) + trq2 = Float( 0.0, iotype="in", desc="pressure differential as a fraction of incomming pressure", units='ft*lbf' ) + trq3 = Float( 0.0, iotype="in", desc="pressure differential as a fraction of incomming pressure", units='ft*lbf' ) + trqNet = Float( 0.0, iotype="in", desc="pressure differential as a fraction of incomming pressure", units='ft*lbf' ) + + + def execute(self): + self.trqNet = self.trq1+self.trq2+self.trq3 + + + +class Nmech(CycleComponent): + """This component serves as the model hub for the speed (usually set from the sovler)""" + + Nmech = Float( 0.0, iotype="out", desc="pressure differential as a fraction of incomming pressure", units='rpm' ) + + def execute(self): + self.Nmech = self.Nmech + +if __name__ == "__main__": + from openmdao.main.api import set_as_top + + c = set_as_top(Shaft()) + c.run() diff --git a/src/pycycle/splitter_bpr.py b/src/pycycle/splitter_bpr.py new file mode 100644 index 0000000..d76dcce --- /dev/null +++ b/src/pycycle/splitter_bpr.py @@ -0,0 +1,29 @@ +from openmdao.main.api import Component +from openmdao.lib.datatypes.api import Float, VarTree + +from pycycle.flowstation import FlowStation, FlowStationVar +from pycycle.cycle_component import CycleComponent + + +class SplitterBPR(CycleComponent): + """Takes a single incoming air stream and splits it into two separate ones + based on a given bypass ratio""" + + BPR = Float( 2.0, iotype="in", desc="ratio of mass flow in Fl_O2 to Fl_O1" ) + + Fl_I = FlowStationVar( iotype="in", desc="incoming air stream to splitter", copy=None ) + Fl_O1 = FlowStationVar( iotype="out", desc="outgoing air stream 1", copy=None ) + Fl_O2 = FlowStationVar( iotype="out", desc="outgoing air stream 2", copy=None ) + + + def execute(self): + Fl_I = self.Fl_I + Fl_O1 = self.Fl_O1 + Fl_O2 = self.Fl_O2 + Fl_O1.copy_from( Fl_I ) + Fl_O2.copy_from( Fl_I ) + + # determine the flow splits + Fl_O1.W = Fl_I.W/( self.BPR + 1) + Fl_O2.W = Fl_O1.W*self.BPR + diff --git a/src/pycycle/start.py b/src/pycycle/start.py index a1413b8..f1e6127 100644 --- a/src/pycycle/start.py +++ b/src/pycycle/start.py @@ -6,43 +6,31 @@ class FlowStart(CycleComponent): - """Flow initialization""" + """Start a flow""" - W = Float(1, iotype="in", desc="mass flow rate", units="lbm/s") - Pt = Float(14.7, iotype="in", desc="total pressure", units="psi") - Tt = Float(518, iotype="in", desc="total temperature", units="degR") - Mach = Float(.1, iotype="in", desc="Mach Number") - - area_des = Float(iotype="out", desc="flow area at the design condition") - Fl_O = FlowStationVar(iotype="out", desc="outgoing flow at the specified conditions", copy=None) + W = Float( 0., iotype="in", desc="mass flow rate", units="lbm/s" ) + Pt = Float( 14.7, iotype="in", desc="total pressure", units="psi" ) + Tt = Float( 518, iotype="in", desc="total temperature", units="degR" ) + species1 = Float( 1., iotype="in", desc="relative amount of species 1 in the flow" ) + species2 = Float( 0., iotype="in", desc="relative amount of species 2 in the flow" ) + species3 = Float( 0., iotype="in", desc="relative amount of species 3 in the flow" ) + species4 = Float( 0., iotype="in", desc="relative amount of species 4 in the flow" ) + species5 = Float( 0., iotype="in", desc="relative amount of species 5 in the flow" ) + species6 = Float( 0., iotype="in", desc="relative amount of species 6 in the flow" ) + + Fl_O = FlowStationVar( iotype="out", desc="outgoing flow at the specified conditions", copy=None ) def execute(self): Fl_O = self.Fl_O - Fl_O.setTotalTP(self.Tt, self.Pt) + Fl_O._species = [ self.species1, self.species2, self.species3, self.species4, self.species5, self.species6 ] + Fl_O.setTotalTP( self.Tt, self.Pt ) Fl_O.W = self.W - Fl_O.Mach = self.Mach - - if self.run_design: - self.area_des = Fl_O.area - -class FlowStartStatic(CycleComponent): - - W = Float(1, iotype="in", desc="mass flow rate", units="lbm/s") - Ps = Float(14.7, iotype="in", desc="total pressure", units="psi") - Ts = Float(518, iotype="in", desc="total temperature", units="degR") - Mach = Float(.1, iotype="in", desc="Mach Number") - - Fl_O = FlowStationVar(iotype="out", desc="outgoing flow at the specified conditions", copy=None) - - - def execute(self): - self.Fl_O.setStaticTsPsMN(self.Ts, self.Ps, self.Mach) - self.Fl_O.W = self.W - self.Fl_O.Mach = self.Mach - - +if __name__ == "__main__": + from openmdao.main.api import set_as_top + c = set_as_top(FlowStart()) + c.run() diff --git a/src/pycycle/test/openmdao_log.txt b/src/pycycle/test/openmdao_log.txt index ad4e1dc..0b912d2 100644 --- a/src/pycycle/test/openmdao_log.txt +++ b/src/pycycle/test/openmdao_log.txt @@ -5227,3 +5227,539 @@ Sep 17 13:39:37 E root: Variable 'sub_or_super' must be in ('sub', 'super'), but *********** BEGIN NEW LOG ************** (2013-10-25 16:27:10.266000) PID=2308 + + +*********** BEGIN NEW LOG ************** (2013-12-20 18:22:07.464000) PID=5764 + + + +*********** BEGIN NEW LOG ************** (2013-12-20 18:22:56.980000) PID=6692 + + + +*********** BEGIN NEW LOG ************** (2013-12-20 18:23:14.222000) PID=1168 + + + +*********** BEGIN NEW LOG ************** (2013-12-20 18:26:37.343000) PID=7504 + + + +*********** BEGIN NEW LOG ************** (2013-12-20 18:27:34.460000) PID=4396 + + + +*********** BEGIN NEW LOG ************** (2013-12-20 18:37:40.250000) PID=7228 + + + +*********** BEGIN NEW LOG ************** (2013-12-20 18:37:48.731000) PID=6836 + + + +*********** BEGIN NEW LOG ************** (2013-12-20 18:39:50.124000) PID=8144 + + + +*********** BEGIN NEW LOG ************** 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b/src/pycycle/test/test_burner.py @@ -0,0 +1,46 @@ + +import unittest + +from openmdao.main.api import set_as_top +from openmdao.util.testutil import assert_rel_error + +from pycycle.api import Burner, FlowStation + + + +class BurnerTestCase(unittest.TestCase): + + + + def tearDown(self): + comp = None + + def test_burner(self): + + # initial test case based on JT9D 34000 .8 operation + self.burner = set_as_top(Burner()) + self.fs = FlowStation() + self.fs.W = 101.57 + self.fs.setDryAir() + self.fs.setTotalTP( 1209.83, 125.611 ) + + burner = self.burner + burner.ID_fuel = 3 + burner.hFuel = -1200 + burner.Wfuel = 1.899 + burner.dPqP = .055 + + burner.Fl_I = self.fs + burner.run() + + TOL = .001 + + # check the flow and mechanical values + assert_rel_error( self, burner.Fl_O.W, 103.47, TOL ) + assert_rel_error( self, burner.Fl_O.Pt, 118.702, TOL ) + assert_rel_error( self, burner.Fl_O.Tt, 2370.00, TOL ) + + +if __name__ == "__main__": + unittest.main() + \ No newline at end of file diff --git a/src/pycycle/test/test_compressorrline.py b/src/pycycle/test/test_compressorrline.py new file mode 100644 index 0000000..8b31098 --- /dev/null +++ b/src/pycycle/test/test_compressorrline.py @@ -0,0 +1,70 @@ + +import unittest + +from openmdao.main.api import set_as_top +from openmdao.util.testutil import assert_rel_error + +from pycycle.api import CompressorRline, FlowStation + + + +class CompressorRlineTestCase(unittest.TestCase): + + + + def tearDown(self): + comp = None + + def test_compressor(self): + + # initial test case based on JT9D 34000 .8 operation + self.comp = set_as_top(CompressorRline()) + self.fs = FlowStation() + self.fs.W = 111.61 + self.fs.setDryAir() + self.fs.setTotalTP( 707.81, 22.395 ) + comp = self.comp + comp.PR = 5.609 + comp.eff = .8651 + comp.Wfrac1=.055 + comp.hfrac1=1 + comp.Pfrac1=1 + comp.Wfrac2=.035 + comp.hfrac2=1 + comp.Pfrac2=1 + comp.Nmech=8000 + + comp.Fl_I = self.fs + comp.run() + + TOL = .001 + + # check the flow and mechanical values + assert_rel_error( self,comp.Fl_O.W, 101.57, TOL ) + assert_rel_error( self,comp.Fl_O.Pt, 125.611, TOL ) + assert_rel_error( self,comp.Fl_O.Tt, 1209.83, TOL ) + + assert_rel_error( self,comp.Fl_bld1.W, 6.1386, TOL ) + assert_rel_error( self,comp.Fl_bld1.Pt, 125.611, TOL ) + assert_rel_error( self,comp.Fl_bld1.Tt, 1209.83, TOL ) + + assert_rel_error( self,comp.Fl_bld2.W, 3.9064, TOL ) + assert_rel_error( self,comp.Fl_bld2.Pt, 125.611, TOL ) + assert_rel_error( self,comp.Fl_bld2.Tt, 1209.83, TOL ) + + + assert_rel_error( self,comp.pwr, -19639.2, TOL ) + assert_rel_error( self,comp.trq, -1350.435, TOL ) + + assert_rel_error( self,comp.eff, .8651, TOL ) + + # adjust the bleed fraction to ensure the temperature is about half + # way between input and output + comp.hfrac1 = .5 + comp.run() + + assert_rel_error( self,comp.Fl_bld1.Tt, 961.654, TOL ) + +if __name__ == "__main__": + unittest.main() + \ No newline at end of file diff --git a/src/pycycle/test/test_duct.py b/src/pycycle/test/test_duct.py index 7ae437a..d150dc2 100644 --- a/src/pycycle/test/test_duct.py +++ b/src/pycycle/test/test_duct.py @@ -4,55 +4,37 @@ from openmdao.main.api import set_as_top from openmdao.util.testutil import assert_rel_error -from pycycle import duct, flowstation +from pycycle.api import Duct, FlowStation -class DuctTestCase(unittest.TestCase): - def test_start(self): - comp = set_as_top(duct.Duct()) - comp.dPqP = 0 - comp.Q_dot = -237.8 - comp.MNexit_des = .4 +class DuctTestCase(unittest.TestCase): - fs = flowstation.FlowStation() - fs.W = 1.080 - fs.setTotalTP(1424.01, .34) - fs.Mach = .4 + - comp.Fl_I = fs + def tearDown(self): + comp = None - comp.design = True - comp.run() - - assert_rel_error(self,comp.Fl_O.W, 1.080, .005) - assert_rel_error(self,comp.Fl_O.Pt, .34, .005) - assert_rel_error(self,comp.Fl_O.Tt, 540.00, .005) - assert_rel_error(self,comp.Fl_O.rhos, .001566, .005) - assert_rel_error(self,comp.Fl_O.Mach, 0.4, .005) - assert_rel_error(self,comp.Fl_O.area, 221.4, .005) - - #check off design - comp.run() + def test_duct(self): + + # initial test case based on JT9D 34000 .8 operation + self.duct = set_as_top(Duct()) + self.fs = FlowStation() + self.fs.W = 100. + self.fs.setTotalTP( 1000, 100 ); - assert_rel_error(self,comp.Fl_O.W, 1.080, .005) - assert_rel_error(self,comp.Fl_O.Pt, .34, .005) - assert_rel_error(self,comp.Fl_O.Tt, 540.00, .005) - assert_rel_error(self,comp.Fl_O.rhos, .001566, .005) - assert_rel_error(self,comp.Fl_O.Mach, 0.4, .005) - assert_rel_error(self,comp.Fl_O.area, 221.4, .005) - - #vary something - comp.dPqP = .1 - comp.run() - - assert_rel_error(self,comp.Fl_O.W, 1.080, .005) - assert_rel_error(self,comp.Fl_O.Pt, .306, .005) - assert_rel_error(self,comp.Fl_O.Tt, 540.00, .005) - assert_rel_error(self,comp.Fl_O.rhos, .0013783, .005) - assert_rel_error(self,comp.Fl_O.Mach, 0.4572, .005) - assert_rel_error(self,comp.Fl_O.area, 221.4, .005) + duct = self.duct + duct.Fl_I = self.fs + duct.dPqP = .1 + duct.run() + + TOL = .001 + # check the flow and mechanical values + assert_rel_error( self, duct.Fl_O.W, 100., TOL ) + assert_rel_error( self, duct.Fl_O.Pt, 90., TOL ) + assert_rel_error( self, duct.Fl_O.Tt, 1000., TOL ) + if __name__ == "__main__": unittest.main() \ No newline at end of file diff --git a/src/pycycle/test/test_flightconditions.py b/src/pycycle/test/test_flightconditions.py new file mode 100644 index 0000000..2aa9bc2 --- /dev/null +++ b/src/pycycle/test/test_flightconditions.py @@ -0,0 +1,44 @@ + +import unittest + +from openmdao.main.api import set_as_top +from openmdao.util.testutil import assert_rel_error + +from pycycle import flightconditions, flowstation + +class FlightConditionsTestCase(unittest.TestCase): + + def test_start(self): + comp = set_as_top(flightconditions.FlightConditions()) + + comp.alt = 35000. + comp.MN = .8 + comp.dTs = 2. + comp.WAR = .0; + comp.Wout = 100; + + comp.run() + + assert_rel_error(self,comp.Fl_O.W, 100., .005) + assert_rel_error(self,comp.Fl_O.Mach, .8, .005) + assert_rel_error(self,comp.Fl_O.Ps, 3.471, .005) + assert_rel_error(self,comp.Fl_O.Pt, 5.2968, .005) + assert_rel_error(self,comp.Fl_O.Tt, 447.847, .005) + + comp.alt = 0. + comp.MN = .0 + comp.dTs = 0. + comp.WAR = .0; + comp.Wout = 100; + + comp.run() + + assert_rel_error(self,comp.Fl_O.W, 100., .005) + assert_rel_error(self,comp.Fl_O.Mach, .0, .005) + assert_rel_error(self,comp.Fl_O.Pt, 14.696, .005) + assert_rel_error(self,comp.Fl_O.Tt, 518.67, .005) + + +if __name__ == "__main__": + unittest.main() + \ No newline at end of file diff --git a/src/pycycle/test/test_inlet.py b/src/pycycle/test/test_inlet.py index 9ccc0c6..c728328 100644 --- a/src/pycycle/test/test_inlet.py +++ b/src/pycycle/test/test_inlet.py @@ -4,53 +4,37 @@ from openmdao.main.api import set_as_top from openmdao.util.testutil import assert_rel_error -from pycycle import inlet, flowstation +from pycycle.api import Inlet, FlowStation -class StartTestCase(unittest.TestCase): - def test_start(self): - comp = set_as_top(inlet.Inlet()) - comp.ram_recovery = 1.0 - comp.MNexit_des = .6 +class InletTestCase(unittest.TestCase): - fs = flowstation.FlowStation() - fs.W = 1.080 - fs.setTotalTP(630.75, 0.0272) - fs.Mach = 1.0 + - comp.Fl_I = fs + def tearDown(self): + comp = None - comp.design = True - comp.run() - - assert_rel_error(self,comp.Fl_O.W, 1.080, .005) - assert_rel_error(self,comp.Fl_O.Pt, .0272, .005) - assert_rel_error(self,comp.Fl_O.Tt, 630.75, .005) - assert_rel_error(self,comp.Fl_O.rhos, .000098, .005) - assert_rel_error(self,comp.Fl_O.Mach, 0.6, .005) - assert_rel_error(self,comp.Fl_O.area, 2230.8, .005) - - #check off design - comp.run() - - assert_rel_error(self,comp.Fl_O.W, 1.080, .005) - assert_rel_error(self,comp.Fl_O.Pt, .0272, .005) - assert_rel_error(self,comp.Fl_O.Tt, 630.75, .005) - assert_rel_error(self,comp.Fl_O.rhos, .000098, .005) - assert_rel_error(self,comp.Fl_O.Mach, 0.6, .005) - assert_rel_error(self,comp.Fl_O.area, 2230.8, .005) - - #vary something - comp.Fl_I.W = .9 - comp.run() + def test_duct(self): + + # initial test case based on JT9D 34000 .8 operation + self.inlet = set_as_top(Inlet()) + self.fs = FlowStation() + self.fs.W = 100. + self.fs.setTotalTP( 1000, 100 ); + + inlet = self.inlet + inlet.Fl_I = self.fs + inlet.ram_recovery = .9 + inlet.run() - assert_rel_error(self,comp.Fl_O.W, .9, .005) - assert_rel_error(self,comp.Fl_O.Pt, .0272, .005) - assert_rel_error(self,comp.Fl_O.Tt, 630.75, .005) - assert_rel_error(self,comp.Fl_O.Mach, 0.45955, .005) - assert_rel_error(self,comp.Fl_O.area, 2230.8, .005) + TOL = .001 + # check the flow and mechanical values + assert_rel_error( self, inlet.Fl_O.W, 100., TOL ) + assert_rel_error( self, inlet.Fl_O.Pt, 90., TOL ) + assert_rel_error( self, inlet.Fl_O.Tt, 1000., TOL ) + if __name__ == "__main__": unittest.main() \ No newline at end of file diff --git a/src/pycycle/test/test_nozzleconvergent.py b/src/pycycle/test/test_nozzleconvergent.py new file mode 100644 index 0000000..e5e9f36 --- /dev/null +++ b/src/pycycle/test/test_nozzleconvergent.py @@ -0,0 +1,58 @@ + +import unittest + +from openmdao.main.api import set_as_top +from openmdao.util.testutil import assert_rel_error + +from pycycle.api import NozzleConvergent, FlowStation + + + +class NozzleConvergentCase(unittest.TestCase): + + + + def tearDown(self): + comp = None + + def test_nozzleconvergent(self): + + # initial test case based on JT9D 34000 .8 operation + # choked + self.nozz = set_as_top(NozzleConvergent()) + self.fs = FlowStation() + self.fs.W = 562.61 + self.fs.setTotalTP( 527.55, 8.978 ); + + nozz = self.nozz + nozz.Fl_I = self.fs + nozz.Cfg = .9962 + nozz.PsExh = 3.626 + nozz.run() + + TOL = .001 + + # check the flow and mechanical values + assert_rel_error( self, nozz.Fg, 21033.3, TOL ) + + # initial test case based on JT9D 0. 0. operation + # unchoked + self.nozz = set_as_top(NozzleConvergent()) + self.fs = FlowStation() + self.fs.W = 1293.91 + self.fs.setTotalTP( 632.71, 23.195 ); + + nozz = self.nozz + nozz.Fl_I = self.fs + nozz.Cfg = .9975 + nozz.PsExh = 14.696 + nozz.run() + + TOL = .001 + + # check the flow and mechanical values + assert_rel_error( self, nozz.Fg, 38786, TOL ) + +if __name__ == "__main__": + unittest.main() + \ No newline at end of file diff --git a/src/pycycle/test/test_shaft.py b/src/pycycle/test/test_shaft.py new file mode 100644 index 0000000..f463ea7 --- /dev/null +++ b/src/pycycle/test/test_shaft.py @@ -0,0 +1,27 @@ + +import unittest + +from openmdao.main.api import set_as_top +from openmdao.util.testutil import assert_rel_error + +from pycycle.api import Shaft + +class TurbineTestCase(unittest.TestCase): + + + def test_shaft(self): + + self.shaft = set_as_top(Shaft()) + + shaft = self.shaft + shaft.trq1 = -10000 + shaft.trq2 = 9000 + + shaft.run() + TOL = .001 + + assert_rel_error( self,shaft.trqNet, -1000., TOL ) + +if __name__ == "__main__": + unittest.main() + \ No newline at end of file diff --git a/src/pycycle/test/test_splitter.py b/src/pycycle/test/test_splitter.py index 3c9d304..7cd22f8 100644 --- a/src/pycycle/test/test_splitter.py +++ b/src/pycycle/test/test_splitter.py @@ -4,106 +4,38 @@ from openmdao.main.api import set_as_top from openmdao.util.testutil import assert_rel_error -from pycycle import splitter, flowstation - -class SplitterTestCase(unittest.TestCase): +from pycycle import splitter_bpr, flowstation + +class SplitterBPRTestCase(unittest.TestCase): def setUp(self): - self.comp = set_as_top(splitter.SplitterBPR()) + self.comp = set_as_top(splitter_bpr.SplitterBPR()) self.fs = flowstation.FlowStation() - self.fs.W = 3.48771299 - self.fs.setTotalTP(630.74523, 0.0271945) - self.fs.Mach = 1 - - def tearDown(self): - comp = None - - def test_splitter(self): - comp = self.comp - - comp.BPR = 2.2285 - comp.MNexit1_des = 1.00 - comp.MNexit2_des = 1.00 - comp.design = True - - comp.Fl_I = self.fs - - comp.run() - - def check(self, comp): - - - TOL = .001 - assert_rel_error(self,comp.Fl_O1.W, 1.08 ,TOL) - assert_rel_error(self,comp.Fl_O1.Pt, 0.0271945 , TOL) - assert_rel_error(self,comp.Fl_O1.Tt, 630.75, TOL) - assert_rel_error(self,comp.Fl_O1.rhos, 0.0000737216 , TOL) - assert_rel_error(self,comp.Fl_O1.Mach, 1.0 ,TOL) - assert_rel_error(self,comp.Fl_O1.area, 1877.2, TOL) - - assert_rel_error(self,comp.Fl_O2.W, 2.407 ,TOL) - assert_rel_error(self,comp.Fl_O2.Pt, 0.0271945 , TOL) - assert_rel_error(self,comp.Fl_O2.Tt, 630.75, TOL) - assert_rel_error(self,comp.Fl_O2.rhos, 0.0000737216 , TOL) - assert_rel_error(self,comp.Fl_O2.Mach, 1.0 ,TOL) - assert_rel_error(self,comp.Fl_O2.area, 4183.4, TOL) + self.fs.W = 10 + self.fs.setTotalTP(630.74523, 10) def test_splitterBPR(self): comp = self.comp - comp.BPR = 2.2285 - comp.MNexit1_des = 1.00 - comp.MNexit2_des = 1.00 - comp.design = True - - comp.Fl_I = self.fs - - comp.run() - - self.check(comp) - - #run off design - comp.run() - - self.check(comp) - - #try changing something - - TOL = 0.001 - comp.Fl_I.W *= .95 - comp.run() - assert_rel_error(self,comp.Fl_O1.Mach, .76922 ,TOL) - assert_rel_error(self,comp.Fl_O2.Mach, .76922 ,TOL) - - def test_splitterW(self): - comp = self.comp = set_as_top(splitter.SplitterW()) + comp.BPR = 9 - comp.W1_des = 1.08 - comp.MNexit1_des = 1.00 - comp.MNexit2_des = 1.00 - comp.design = True comp.Fl_I = self.fs comp.run() + TOL = .001 + assert_rel_error(self,comp.Fl_O1.W, 1. ,TOL) + assert_rel_error(self,comp.Fl_O1.Pt, 10. , TOL) + assert_rel_error(self,comp.Fl_O1.Tt, 630.75, TOL) - self.check(comp) - - #run off design - comp.run() - - self.check(comp) - - #try changing something - TOL = 0.001 - comp.Fl_I.W *= .95 - comp.run() - assert_rel_error(self,comp.Fl_O1.Mach, .76922 ,TOL) - assert_rel_error(self,comp.Fl_O2.Mach, .76922 ,TOL) + assert_rel_error(self,comp.Fl_O2.W, 9. ,TOL) + assert_rel_error(self,comp.Fl_O2.Pt, 10., TOL) + assert_rel_error(self,comp.Fl_O2.Tt, 630.75, TOL) + if __name__ == "__main__": unittest.main() diff --git a/src/pycycle/test/test_splitterBPR.py b/src/pycycle/test/test_splitterBPR.py new file mode 100644 index 0000000..2751bac --- /dev/null +++ b/src/pycycle/test/test_splitterBPR.py @@ -0,0 +1,110 @@ + +import unittest + +from openmdao.main.api import set_as_top +from openmdao.util.testutil import assert_rel_error + +from pycycle.api import splitter, flowstation + +class SplitterTestCase(unittest.TestCase): + + def setUp(self): + self.comp = set_as_top(splitter.SplitterBPR()) + + self.fs = flowstation.FlowStation() + self.fs.W = 3.48771299 + self.fs.setTotalTP(630.74523, 0.0271945) + self.fs.Mach = 1 + + def tearDown(self): + comp = None + + def test_splitter(self): + comp = self.comp + + comp.BPR = 2.2285 + comp.MNexit1_des = 1.00 + comp.MNexit2_des = 1.00 + comp.design = True + + comp.Fl_I = self.fs + + comp.run() + + def check(self, comp): + + + TOL = .001 + assert_rel_error(self,comp.Fl_O1.W, 1.08 ,TOL) + assert_rel_error(self,comp.Fl_O1.Pt, 0.0271945 , TOL) + assert_rel_error(self,comp.Fl_O1.Tt, 630.75, TOL) + assert_rel_error(self,comp.Fl_O1.rhos, 0.0000737216 , TOL) + assert_rel_error(self,comp.Fl_O1.Mach, 1.0 ,TOL) + assert_rel_error(self,comp.Fl_O1.area, 1877.2, TOL) + + assert_rel_error(self,comp.Fl_O2.W, 2.407 ,TOL) + assert_rel_error(self,comp.Fl_O2.Pt, 0.0271945 , TOL) + assert_rel_error(self,comp.Fl_O2.Tt, 630.75, TOL) + assert_rel_error(self,comp.Fl_O2.rhos, 0.0000737216 , TOL) + assert_rel_error(self,comp.Fl_O2.Mach, 1.0 ,TOL) + assert_rel_error(self,comp.Fl_O2.area, 4183.4, TOL) + + def test_splitterBPR(self): + comp = self.comp + + comp.BPR = 2.2285 + comp.MNexit1_des = 1.00 + comp.MNexit2_des = 1.00 + comp.design = True + + comp.Fl_I = self.fs + + comp.run() + + self.check(comp) + + #run off design + comp.run() + + self.check(comp) + + #try changing something + + TOL = 0.001 + comp.Fl_I.W *= .95 + comp.run() + assert_rel_error(self,comp.Fl_O1.Mach, .76922 ,TOL) + assert_rel_error(self,comp.Fl_O2.Mach, .76922 ,TOL) + + def test_splitterW(self): + comp = self.comp = set_as_top(splitter.SplitterW()) + + comp.W1_des = 1.08 + comp.MNexit1_des = 1.00 + comp.MNexit2_des = 1.00 + comp.design = True + + comp.Fl_I = self.fs + + comp.run() + + self.check(comp) + + #run off design + comp.run() + + self.check(comp) + + #try changing something + + TOL = 0.001 + comp.Fl_I.W *= .95 + comp.run() + assert_rel_error(self,comp.Fl_O1.Mach, .76922 ,TOL) + assert_rel_error(self,comp.Fl_O2.Mach, .76922 ,TOL) + + + +if __name__ == "__main__": + unittest.main() + \ No newline at end of file diff --git a/src/pycycle/test/test_turbineprmap.py b/src/pycycle/test/test_turbineprmap.py new file mode 100644 index 0000000..5b83e00 --- /dev/null +++ b/src/pycycle/test/test_turbineprmap.py @@ -0,0 +1,52 @@ + +import unittest + +from openmdao.main.api import set_as_top +from openmdao.util.testutil import assert_rel_error + +from pycycle import turbine_prmap, flowstation + +class TurbineTestCase(unittest.TestCase): + + + + + def test_turbine(self): + + self.turbine = set_as_top(turbine_prmap.TurbinePRmap()) + + self.fs = flowstation.FlowStation() + self.fs._species=[.9816,0,.018355,0,0,0,0] + self.fs.W = 103.47 + self.fs.setTotalTP( 2371.94, 119.086 ) + + self.b1 = flowstation.FlowStation() + self.b1.W = 6.1386 + self.b1.setTotalTP( 1211.05, 126.017 ) + + self.b2 = flowstation.FlowStation() + self.b2.W = 3.9064 + self.b2.setTotalTP( 1211.05, 126.017 ) + + turbine = self.turbine + turbine.eff = .9133 + turbine.PR = 2.670 + turbine.Nmech = 8000. + + turbine.Fl_I = self.fs + turbine.Fl_bld1 = self.b1 + turbine.Fl_bld2 = self.b2 + turbine.run() + TOL = .001 + + assert_rel_error( self,turbine.Fl_O.W, 113.51, TOL ) + assert_rel_error( self,turbine.Fl_O.Pt, 44.60, TOL ) + assert_rel_error( self,turbine.Fl_O.Tt, 1850.6, TOL ) + + + assert_rel_error( self,turbine.pwr, 19684, TOL ) + assert_rel_error( self,turbine.trq, 1353.2, TOL ) + +if __name__ == "__main__": + unittest.main() + \ No newline at end of file diff --git a/src/pycycle/turbine_prmap.py b/src/pycycle/turbine_prmap.py new file mode 100644 index 0000000..2e55019 --- /dev/null +++ b/src/pycycle/turbine_prmap.py @@ -0,0 +1,71 @@ +import math + +from openmdao.main.api import Component +from openmdao.lib.datatypes.api import Float, VarTree, Event + +from pycycle.flowstation import FlowStation, FlowStationVar, GAS_CONSTANT +from pycycle.cycle_component import CycleComponent + + + +class TurbinePRmap(CycleComponent): + """Axial Compressor performance calculations""" + + PR = Float( 0., iotype="in", desc="Pressure ratio at design conditions") + MNexit_des = Float( 0., iotype="in", desc="mach number at the compressor exit at design conditions") + eff_des = Float( 0., iotype="in", desc="adiabatic efficiency at the design condition") + + Fl_I = FlowStationVar(iotype="in", desc="incoming air stream to compressor", copy=None) + Fl_bld1 = FlowStationVar(iotype="in", desc="bleed entering the front of the turbine", copy=None) + Fl_bld2 = FlowStationVar(iotype="in", desc="bleed entering the exit of the turbine", copy=None) + + PR = Float(iotype="out", desc="pressure ratio at operating conditions") + eff = Float(iotype="out", desc="adiabatic efficiency at the operating condition") + eff_poly = Float(iotype="out", desc="polytropic efficiency at the operating condition") + pwr = Float(iotype="out", units="hp", desc="power required to run the compressor at the operating condition") + + Nmech = Float( 10000., iotype="in", desc="Mechanical speed") + trq = Float( 0., iotype="out", desc="trq") + + Fl_O = FlowStationVar(iotype="out", desc="outgoing air stream from compressor", copy=None) + + + def execute(self): + + Fl_I = self.Fl_I + Fl_O = self.Fl_O + Fl_bld1 = self.Fl_bld1 + Fl_bld2 = self.Fl_bld2 + + F41 = FlowStation() + F48 = FlowStation() + fs_ideal = FlowStation() + + F41.copy_from( Fl_I ) + F41.add( Fl_bld1 ) + fs_ideal.copy_from( F41 ) + F48.copy_from( F41 ) + + #Design Calculations + #fs_ideal.copy_from( Fl_O ) + Pt_out = self.Fl_I.Pt/self.PR + fs_ideal.setTotalSP(F41.s, Pt_out) + ht_out = F41.ht - ( F41.ht - fs_ideal.ht )*self.eff; + F48.setTotal_hP(ht_out, Pt_out) + + C = GAS_CONSTANT*math.log(self.PR) + delta_s = Fl_O.s - Fl_I.s + self.eff_poly = C/(C+delta_s) + self.pwr = (F41.W)*(F41.ht - F48.ht) * 1.4148532 #btu/s to hp + self.trq = 550. * self.pwr / self.Nmech; + + Fl_O.copy_from( F48 ) + Fl_O.add( Fl_bld2 ) + +if __name__ == "__main__": + from openmdao.main.api import set_as_top + + c = set_as_top(Turbine()) + c.run() + +