Difference between revisions of "Compressible flows by Joel Guerrero"
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| − | You can download the case files in this [http://www.wolfdynamics.com/ | + | You can download the case files in this [http://www.wolfdynamics.com/validations/supersonic_wedge/case.tar.gz link]. |
Go back to the [https://wiki.openfoam.com/Collection_by_authors#Joel_Guerrero contributions page]. | Go back to the [https://wiki.openfoam.com/Collection_by_authors#Joel_Guerrero contributions page]. | ||
Revision as of 02:56, 19 August 2019
- 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.
Go back to the contributions page.
