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Outline:Supersonic flow over a wedge using OpenFOAM Problem specification Boundary conditions BlockMeshDict file of wedge Mesh parameters of wedge Compressible solver Paraview visualization Calculating Mach number Contour of U (velocity) and T (Temperature) Validation
Supersonic flow over a wedge using OpenFOAM Problem specification Boundary conditions BlockMeshDict file of wedge Mesh parameters of wedge Compressible solver Paraview visualization Calculating Mach number Contour of U (velocity) and T (Temperature) Validation
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