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simpleFoam kOmegaSST k, w and nut initial and boundary values |
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#1 |
New Member
Ezel Bayraktar
Join Date: Jul 2020
Posts: 4
Rep Power: 6 ![]() |
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 http://ichrome.com/blogs/archives/342 and http://www.wolfdynamics.com/tools.html?id=110. 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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#2 |
New Member
Ali Can
Join Date: Apr 2021
Posts: 28
Rep Power: 5 ![]() |
Hi Ezel, if you are sure that the turbulence coefficients you use are correct, you can try to reduce the relaxation factors to get stable results.
Eyşan Tezcan Atay |
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#3 |
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Eren
Join Date: Aug 2018
Posts: 86
Rep Power: 8 ![]() |
You need to share your log so people can see/understand whats happening. A simulation can diverge from hundreds of reasons.
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#4 |
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Ezel Bayraktar
Join Date: Jul 2020
Posts: 4
Rep Power: 6 ![]() |
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Tags |
komega sst model, komegacoeffs, simplefoam convergence |
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Thread | Thread Starter | Forum | Replies | Last Post |
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