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1 Geometry
1 Mesh
4 Simulation setups
4 ResultsCFD simulation of NACA 0012 airfoil at different angles of attack. Analysis of Cl, Cd and Cl/Cd for AoA = 0°, 5° and 10°
by slilbaekslilbaek
tcarvalhal created this project
about 1 month ago
1 Geometry 1 Mesh 4 Simulation setups 4 ResultsCFD simulation of NACA 0012 airfoil at different angles of attack. Analysis of Cl, Cd and Cl/Cd for AoA = 0°, 5° and 10°
