lift and drag coefficient
 

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!!!

Re: lift and drag coefficient
 

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

Re: lift and drag coefficient
 

Ok sorry I hadn't seen that I could search for my answer in the archives...No comment... :) Thanks!