2.6. Supersonic Flow over a Forward-facing Step
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This tutorial illustrates the setup and solution of a two-dimensional compressible flow supersonic problem. This tutorial demonstrates how to do the following:
Generate the mesh using the built-in tool.
Set numerical control parameters.
Enable the second-order discretization scheme for improved predictions.
Set gas properties, initial conditions and boundary conditions.
Set physical model for a supersonic problem.
Set output parameters for a 2D compressible flow supersonic problem.
Generate and check the GASFLOW input file, ingf.
Plot the calculation results by ParaView.
1) GASFLOW input file
2) Comparison to the numerical solutions
[ED-FD 5] Transient Supersonic Flow at Mach 3 over a Forward-facing Step
