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simpleFoam kOmegaSST k, w and nut initial and boundary values

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Old   December 3, 2021, 09:27
Default simpleFoam kOmegaSST k, w and nut initial and boundary values
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Ezel Bayraktar
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Hello Everyone,

I am trying to simulate flow over an airfoil using simpleFoam and turbulence model kOmegaSST. I have taken k, w and nut values from and But after several iterations, soltion diverges. After changing these values many times, I have obtained a stable solution. My question is; how could we select values of these turbulence parameters.

with all respect...
Ezel Bayraktar
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