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July 14, 2002, 10:49 |
Flow Over an Airfoil
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#1 |
Guest
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Hi all,I want investigate flow over an airfoil(for example NACA 0012)at angle of attack.I like use O grid type.What i should use B.C for this problem?What kind of B.C should be used? Thanks.
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July 14, 2002, 16:57 |
Re: Flow Over an Airfoil
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#2 |
Guest
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Pressure far field B.C.
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July 18, 2002, 21:34 |
Re: Flow Over an Airfoil
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#3 |
Guest
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airfoil ---- Wall etc ------- Only Pressure far field
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