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2d laminar supersonic flow with boundary layer modeling
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0Statistics
2 Geometries
6 Meshes
3 Simulation setups
14 Results
2 Geometries 6 Meshes 3 Simulation setups 14 ResultsAbout this project
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 created this project
e0625598 copied this project