Point of lift / drag in a 3D wing simulate.
I've done a 3D simulation of a wing with simpleFoam.
Now I will know how to find the point there the lift is centered.
I have used patchIntegrate to know how much the lift is,
but I also need to know where.
I don't find any thing about that here in cfd-online.
Does any one know how to treat this problem ? I will be thank full for answer!
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