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Obtaining an absurd value for the lift coefficient |
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August 11, 2010, 02:31 |
Obtaining an absurd value for the lift coefficient
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Join Date: Nov 2009
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Hello every1,
I am trying to simulate a car model at some freestream velocity. Im using the realizable KE turb model for this. The problem comes when I'm calculating the lift coefficient. Although Im getting a correct value for Cd, Im getting an absurd value for Cl (arnd -77.56). If anyone has an experience on simulating flow over a car, kindly advise me on what changes should i make in order to get a correct Cl . Thanks a lot. Last edited by deeps; August 11, 2010 at 02:35. Reason: spelling mistake in the subject of the thread |
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