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This project aims to study the dynamic behavior of a simplified model of an aircraft when rolling (steady state) when it is circulating stationary on the runway. The roughness of the track is the main exciting agent that will be considered in this project.
Landing Gear Analysis for Airbus A320 and IL76 including Equivalent Stress, Equivalent Strain, total deformation, safety factor, equivalent alternating stress, iso corrosion curves, life and damage analysis