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June 27, 2013, 21:18 |
cd and cl parameters
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#1 |
New Member
Ricardo
Join Date: Jun 2013
Location: u.k.
Posts: 4
Rep Power: 12 |
I am simulating Naca 0012 airfoil in 2D with with 10 degrees of angle of attack. I donīt know where I have to check the values obtained for cl and cd. In the picture attached I show where I am checking the results. Are those the correct values for cd and cl?? Or I have to go to: Reports-Forces.
Thank you very much. |
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June 28, 2013, 16:06 |
Answer
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#2 |
Member
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Hi mate,
Those two methods are giving same results, but with Results > Forces you can get accurate number. And as seen, changes in Cd is of order of 1e-7, which is negligible.
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ICEM, CFX and Fluent expert |
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