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July 28, 2014, 01:53 |
Lift hysteresis trouble
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#1 |
New Member
Pras
Join Date: Apr 2014
Posts: 13
Rep Power: 12 |
Hi all,
I am running a case of oscillating airfoil and I get lift coefficients such that as the angle of attack increases the lift coefficient decreases and vice versa. Basically, the hysteresis loop is rotated 90 degrees. When I try to get static lift coefficients I get correct behaviour and good converged solution. Anybody has any suggestions? |
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July 28, 2014, 16:47 |
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#2 |
New Member
Pras
Join Date: Apr 2014
Posts: 13
Rep Power: 12 |
Looks like not many people around willing to help
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August 18, 2015, 10:04 |
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#3 |
Senior Member
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Hey Pras,
Did you solve the problem? I seem to have the same problem. Any suggestions? Regards, Awais |
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