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NACA 63012 AIRFOIL
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Statistics
21Â Geometries
14Â Meshes
13Â Simulation setups
13Â Results
21Â Geometries 14Â Meshes 13Â Simulation setups 13Â ResultsAbout this project
NACA 63012 Airfoil at varying angle of attack (zero to stall) laminar flow in seawater
