Obtaining section data in fluent
I have simulated 3D flow around a blade in fluent and I would like to obtain the Cp values at the mid-section of the blade. I created a plane at that location but I do not know how to obtain the pressure coefficient on the resulting 2D airfoil section (where the plane cuts the blade) alone. I know that we can get the contours in the entire plane but how can I restrict them to a particular surface in that plane?
Some help is greatly appreciated
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