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NACA 63212 AIRFOIL
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Statistics
21Â Geometries
8Â Meshes
9Â Simulation setups
9Â Results
21Â Geometries 8Â Meshes 9Â Simulation setups 9Â ResultsAbout this project
NACA 63212 Airfoil at varying angle of attack (zero to stall) laminar flow in seawater
