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:sup_wedge.png|800px|right|tut1]]
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[[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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You can download the case files in this [http://www.wolfdynamics.com/validations/supersonic_wedge/case.tar.gz link].
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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


Supersonic flow past a wedge - Shock waves

Supersonic wedge

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.