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Airfoil for Volos Wing analysis

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Volos1
Volos1
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geometries 5 Geometriesmeshes 5 Meshessimulations 11 Simulation setupsruns 75 Results
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Testing NACA 63-615 vs NACA 65-410 vs EPPLER 1210. Chord length is 0.3 m Testing EPPLER 1210 with 0, 10, 20 deg of chord flex

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Project History

  • Volos1

    Volos1 created this project