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NACA63415_CFD
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3 Geometries
2 Meshes
3 Simulation setups
0 Results
3 Geometries 2 Meshes 3 Simulation setups 0 ResultsAbout this project
Modelling incompressible viscous flow over a NACA 632-415 airfoil at Re=1.3e6 and M=0.25 for UCK 305E Aerodynamics course project
