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wing_aerodynamic

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salmghlab58
salmghlab58
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geometries 2 Geometriesmeshes 2 Meshessimulations 1 Simulation setupruns 3 Results
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calculate lift coefficient and drag coefficient at variable AOA

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Project History

  • mabobajer

    mabobajer created this project

  • salmghlab58

    salmghlab58 copied this project