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NACA63415_CFD
Statistics
3Â Geometries
2Â Meshes
3Â Simulation setups
7Â Results
3Â Geometries 2Â Meshes 3Â Simulation setups 7Â 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
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