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Old   October 18, 2007, 13:04
Default lift and drag coefficient
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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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Old   October 18, 2007, 15:28
Default Re: lift and drag coefficient
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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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Old   October 18, 2007, 16:36
Default Re: lift and drag coefficient
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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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