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NACA4418 CONTROL SURFACE - LIFT, DRAG, MOMENT STUDY

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jmepley
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geometries 6 Geometriesmeshes 4 Meshessimulations 3 Simulation setupsruns 2 Results
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Evaluate the effects of varying control surface deflection on lift drag and moment coefficients of the NACA4418 airfoil.

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  • jmepley

    jmepley created this project