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Aerofoil-Simulation

A series of files for calculating and drawing airflow around an aerofoil. Written for an Aerodynamics course. All flows are subsonic and mostly laminar. The simulation could only find a steady state solution. The repository also includes several files for normalizing and adjusting aerofoil models, and a file for easy construction of several basic shapes.

Below are some images depicting what this code can achieve. Calculating lift coefficient at each vertex of a convex aerofoil Calculating airflow around a circle (N=36) with a vortex present Calculating flow around an aerofoil and comparing results with experimental data

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A series of files for calculating and drawing airflow around an aerofoil. Written for an Aerodynamics course at the University of Nevada, Reno.

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