Difference between revisions of "Compressible flows by Joel Guerrero"
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=[http://www.wolfdynamics.com/validations/supersonic_wedge/tut_2D_supersonic_wedge.pdf Supersonic flow past a wedge - Shock waves]= | =[http://www.wolfdynamics.com/validations/supersonic_wedge/tut_2D_supersonic_wedge.pdf Supersonic flow past a wedge - Shock waves]= | ||
− | [[File: | + | [[File:sup_wedge.png|800px|right|Supersonic wedge]] |
In this [http://www.wolfdynamics.com/validations/supersonic_wedge/tut_2D_supersonic_wedge.pdf 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, | In this [http://www.wolfdynamics.com/validations/supersonic_wedge/tut_2D_supersonic_wedge.pdf 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, | ||
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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. | ||
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− | You can download the case files | + | You can download the case files at 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]. |
Latest revision as of 09:55, 6 January 2020
- 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 at this link.
Go back to the contributions page.