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2D airfoil Simulation Kwsst boundary conditions

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Old   July 7, 2018, 16:19
Default 2D airfoil Simulation Kwsst boundary conditions
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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 03:52.
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Old   July 21, 2018, 16:10
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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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Old   August 11, 2018, 08:54
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Thank you very much
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