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How to set initial field for supersonic flows |
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March 4, 2006, 08:57 |
How to set initial field for supersonic flows
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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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