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How to compute Cm of the wing at 25% of the airfoil.

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Old   April 3, 2021, 04:37
Default How to compute Cm of the wing at 25% of the airfoil.
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I have already run the calculation at ANSYS Fluent and I have found the Cl and Cd.
As about the moment coefficient, idk what to insert as inputs for the moment at the force report window, because of the sweep angle of 30 deg.

I would appreciate it if somebody could help me!

P.S I have attached 2 pictures as about the problem.
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File Type: jpg force report.JPG (32.5 KB, 8 views)
File Type: jpg Capture.JPG (30.0 KB, 4 views)
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ansys, cfd, fluent, moment coefficient

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