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Supersonic flow past a wedge
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Statistics
2 Geometries
2 Meshes
1 Simulation setup
2 Results
2 Geometries 2 Meshes 1 Simulation setup 2 ResultsAbout this project
The inlet Mach number is 3, and the wedge angle is 20 degrees. In this validation case, we also compare the dependence of the solution on the mesh resolution. We also show two methods to capture the shock wave, namely, numerical Schlieren (gradient of density), and numerical shadowgraph (Laplacian of the gradient).
