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NACA2408 - Copy
3
0
Statistics
4 Geometries
3 Meshes
3 Simulation setups
1 Result
4 Geometries 3 Meshes 3 Simulation setups 1 ResultAbout this project
Our goal is to model the lift and drag coefficients of this airfoil as a function of angle of attack, airspeed, and size. - Copy
