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NACA2412 Wing CFD Analysis
1
0
Statistics
2 Geometries
2 Meshes
5 Simulation setups
7 Results
2 Geometries 2 Meshes 5 Simulation setups 7 ResultsAbout this project
CFD analysis of NACA 2412 tapered wing to determine lift, drag and pressure distribution at various angles of attack. Part of aerospace engineering portfolio.
