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Old   July 3, 2005, 13:07
Default asymmetry
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Anmol
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Hi,

I am solving flow around an airfoil with triagular mesh at a Reynold's # ~1,000,000. The pressure distribution is not exactly symmetrical. I tried grid refinement and reducing residuals but it helps little. If anyone can suggest a reason, I would be really thankful.

Regards, Anmol
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