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May 3, 2013, 03:25
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run time post processing of pressure distribution over airfoil
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#1 |
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New Member
Zifei Yin
Join Date: Sep 2012
Posts: 25
Rep Power: 2  |
I have used forceCoeffs to output Cl Cd and Cm by run time for airfoil calculate.
Now, I'd like to outpot pressure distribution over airfoil by run time post processing. Is there a way to achieve this? |
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| Tags |
| postprocessing; openfoam; |
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