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NACA 0012 Airfoil Validation
417 2
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2 Geometries 2 Meshes 2 Simulation setups 3 Results
About this project
This is NACA 0012 airfoil validation case, using NASA wind tunel test results at mach 0.15.
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by Ali_ArafatAli_Arafat
Project History
UllWarg created this project