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NACA 63012 AIRFOIL

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arthurherring
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geometries 21 Geometriesmeshes 14 Meshessimulations 13 Simulation setupsruns 13 Results
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NACA 63012 Airfoil at varying angle of attack (zero to stall) laminar flow in seawater

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Project History

  • arthurherring

    arthurherring created this project