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NACA 0012 Airfoil Validation
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385
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0Statistics
2 Geometries
2 Meshes
2 Simulation setups
3 Results
2 Geometries 2 Meshes 2 Simulation setups 3 ResultsAbout this project
This is NACA 0012 airfoil validation case, using NASA wind tunel test results at mach 0.15.
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Project History
UllWarg created this project