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Unsteady Flow over an Airfoil

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Old   October 1, 2015, 00:56
Default Unsteady Flow over an Airfoil
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Siavash
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Hi everybody
I'm trying to simulate NACA0015 airfoil separation in unsteady flow situations.
M=0.22. mesh is C-Type.AOA=15 deg.
I have tried Pressure far-field BC all around.Divergence in Temp and Press occurred.
for next try, used velocity inlet and 3-pressure farfield. Divergence!
Can anybody help me?
regards
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