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Control Wing Test

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SayanS
SayanS
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geometries 2 Geometriesmeshes 1 Meshsimulations 1 Simulation setupruns 1 Result
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cfd simulation of a NACA 0012 airfoil with span 0.1m and chord 0.1m

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Project History

  • SayanS

    SayanS created this project