Difference between revisions of "Compressible flows by Joel Guerrero2"
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(Created page with "category:basic tutorial category:laminar * '''contributor''': Joel Guerrero * '''affiliation''': Universita degli Studi di Genova, Wolf Dynamics * '''contact''': <mail...") |
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| − | =[http://www.wolfdynamics.com/validations/expansion_fan/tut_expansion_fan.pdf Supersonic flow past an expansion corner | + | =[http://www.wolfdynamics.com/validations/expansion_fan/tut_expansion_fan.pdf Supersonic flow past an expansion corner - Expansion fan]= |
[[File:sup_wedge.png|800px|right|tut1]] | [[File:sup_wedge.png|800px|right|tut1]] | ||
| − | In this [http://www.wolfdynamics.com/validations/ | + | In this [http://www.wolfdynamics.com/validations/expansion_fan/tut_expansion_fan.pdf tutorial], we simulate the flow past an expansion corner. The inlet Mach number is 2.5, and the expansion corner angle is 15 degrees. You will learn about, |
* Running compressible flow simulations. | * Running compressible flow simulations. | ||
| Line 18: | Line 18: | ||
* 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 | + | * How to use steady solvers with high-speed compressible flow. |
* Computing the Mach number. | * Computing the Mach number. | ||
| − | |||
* Sampling and plotting | * Sampling and plotting | ||
| − | You can download the case files in this [http://www.wolfdynamics.com/validations/ | + | You can download the case files in this [http://www.wolfdynamics.com/validations/expansion_fan/expansion_fan.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 11:33, 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 an expansion corner - Expansion fan
In this tutorial, we simulate the flow past an expansion corner. The inlet Mach number is 2.5, and the expansion corner angle is 15 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 steady solvers with high-speed compressible flow.
- Computing the Mach number.
- Sampling and plotting
You can download the case files in this link.
Go back to the contributions page.
