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2d laminar supersonic flow with boundary layer modeling
521
8
Statistics
2Â Geometries
6Â Meshes
3Â Simulation setups
14Â Results
2Â Geometries 6Â Meshes 3Â Simulation setups 14Â 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.
