Compressible flows by Joel Guerrero3
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- contributor: Joel Guerrero
- affiliation: Universita degli Studi di Genova, Wolf Dynamics
- contact: click here for email address
- OpenFOAM version: 7
- published under: CC BY-SA license (creative commons licenses)
Supersonic flow past a wedge - Shock waves
In this tutorial, we simulate a supersonic flow past a wedge. The inlet Mach number is 3, and the wedge angle is 20 degrees. You will learn about,
- Running compressible flow simulations.
- Running supersonic flow simulations.
- Setting the thermophysical properties for the working fluid.
- Setting a robust numeric for compressible-supersonic flow simulations.
- How to use pseudo-transient solvers.
- Computing the Mach number.
- Capturing shock waves.
- Sampling and plotting
You can download the case files in this link.
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