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2d laminar supersonic flow with boundary layer modeling

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2d laminar supersonic flow with boundary layer modeling image
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geometries 2 Geometriesmeshes 6 Meshessimulations 3 Simulation setupsruns 14 Results

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at first a test model with a coarse mesh is used to find the right boundary conditions for all patches. the second model should capture the correct shockwave boundary layer interaction.

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  • wulliamp

    wulliamp created this project

  • e0625598

    e0625598 copied this project