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October 18, 2007, 14:04
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lift and drag coefficient
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#1 |
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Guest
Posts: n/a
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hello!
I am studying the airfoil NACA 23012 in ANSYS CFX 11.0, and I would like to see the lift and drag coefficient (or force) in CFX-post. Does anybody know how I can see them? Many thanks in advance!!! |
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October 18, 2007, 16:28
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Re: lift and drag coefficient
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#2 |
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Guest
Posts: n/a
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Hello Marion,
This has been discussed in this forum many times. Please see the archives. Any ways, in simple words: Force you can get directly from the post. See the functions. Normalize it with dynamic head. Small expression will do. You have the coefficients ready. Regards Anantha |
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October 18, 2007, 17:36
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Re: lift and drag coefficient
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#3 |
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Guest
Posts: n/a
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Ok sorry I hadn't seen that I could search for my answer in the archives...No comment...
 Thanks!
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