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NACA 63212 AIRFOIL

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arthurherring
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geometries 21 Geometriesmeshes 8 Meshessimulations 9 Simulation setupsruns 9 Results
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NACA 63212 Airfoil at varying angle of attack (zero to stall) laminar flow in seawater

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Project History

  • arthurherring

    arthurherring created this project