Difference between revisions of "Compressible flows by Joel Guerrero"
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* Setting the thermophysical properties for the working fluid. | * Setting the thermophysical properties for the working fluid. | ||
* Setting a robust numeric for compressible-supersonic flow simulations. | * Setting a robust numeric for compressible-supersonic flow simulations. | ||
| − | * | + | * How to use pseudo-transient solvers. |
* Computing the Mach number. | * Computing the Mach number. | ||
* Capturing shock waves. | * Capturing shock waves. | ||
Revision as of 00:56, 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.
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