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NACA Airfoil 2421
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2 Geometries
1 Mesh
1 Simulation setup
1 Result
2 Geometries 1 Mesh 1 Simulation setup 1 ResultAbout this project
Study aerodynamic behaviour (CL, CD, CP) of NACA 2412 from 0° to 18° AoA Capture flow separation, stall onset, and shock wave formation at Mach 0.7–0.8
