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May 27, 2009, 09:28 |
lift coefficient
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#1 |
New Member
sahar
Join Date: May 2009
Posts: 1
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well i was simulating a simple cone cylinder , i gave the angle of attack also,flow was supersonic but while it was running on fluent my solution was converged but lift cofficient(Cl) residuals comes zero during all simulations which is not possible i cant get my mistake,,so plz guide me
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