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How to set initial field for supersonic flows

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Old   March 4, 2006, 08:57
Default How to set initial field for supersonic flows
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Qu Kun
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When I simulate a supersonic inviscid flow arround a airfoil, if I set the inital field according to the free stream, there will be negative pressure at tail edge after some steps. This problem also occurs at the back of a cylind.

Then how to set a good initial field? Or there some other reason?

Thanks
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