Oblique shock wave – 2D Model
You can download a free step format of a 2D triangular object with a fluid domain to use in a supersonic CFD simulation. The model is not copyrighted and permission for reuse is granted.
I created a step by step CFD ANSYS Fluent tutorial about 2D oblique shock waves in supersonic flow. You can find the video tutorial on my Youtube Channel. The tutorial demonstrates how to use an online calculator tool to determine the shock wave line angle and the downstream Mach number. To check and use this tool please click here. For the purpose of completing this CFD simulation, I used the density based solve and the K-Omega SST turbulent model. The simulation is a steady-state case.