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when,Ma=0.95,problems of airfoil compution in cfx |
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May 24, 2005, 11:04
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when,Ma=0.95,problems of airfoil compution in cfx
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hi all
when Ma=0.95, I am computing an airfoil with a gap , Phiscal time scale=0.005, farfield rule=30 meters , the normal pressure force result is not converging , the transonic computing is so hard in cfx ,and how do I deal with it, my friends, help me!!! |
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