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2D airfoil Simulation Kwsst boundary conditions |
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July 7, 2018, 17:19 |
2D airfoil Simulation Kwsst boundary conditions
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#1 |
Member
Os
Join Date: Jun 2017
Posts: 80
Rep Power: 9 |
hey guys
i am trying to make a 2d airfoil simulation in openfoam using the simpleFoam solver,and i am using the Komegasst turbulence modele and at the moment i know how to set th U and p boundary conditions but i have now idea about how to set them for K omega and nut. my 2d airfoil in in freestream and ive set my domain as follows inlet outlet top bottom airfoil frontandback.........>empty would you please help me how should i set the BC in the 0 directory for , K Omega and nut Thank you Last edited by losiola; July 16, 2018 at 04:52. |
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July 21, 2018, 17:10 |
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#2 |
Senior Member
Join Date: Aug 2015
Posts: 494
Rep Power: 15 |
Check out this tutorial : https://github.com/OpenFOAM/OpenFOAM...rofoilNACA0012. It's for rhoSimpleFoam, but a brief glance at the bc's for k,omega,nut looked to be fine for simpleFoam.
Caelan |
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August 11, 2018, 09:54 |
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#3 |
Member
Os
Join Date: Jun 2017
Posts: 80
Rep Power: 9 |
Thank you very much
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