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.
Note: Please manually create two folders named "input" and "output" in the directory where the .gsv file resides. The "input" and "output" folders will be automatically generated only when initiating a new project in GASVIEW.
