CFD-Post v12.1 & wing pressure coefficients
I've modelled the flow around a 3-D wing and want to see the pressure coefficient distributions around aerofoil sections at different span-wise positions.
How can this be done in CFD-Post v12.1? I guess I need to make a line around the wing at a specified span-wise location and obtain the Cp data on the line. But I cannot get this to work?
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