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New Member
Cagri Metin
Join Date: Jul 2013
Location: İzmir/Turkey
Posts: 14
Rep Power: 13 ![]() |
I am new user for fluent, I am interesting in airfoil ,which is NACA 0021, I get independing of mesh number in my solution but when I've started 16 angle of attack, I show a diverge problem for omega on residual window. please help me
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diverged, sst k-omega |
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