How to compute Cm of the wing at 25% of the airfoil. -- CFD Online Discussion Forums

April 3, 2021, 04:37

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

Student_mary

New Member

mariyaaah123

Join Date: Mar 2021

Posts: 3

Rep Power: 5

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.

Attached Images

	force report.JPG (32.5 KB, 8 views)
	Capture.JPG (30.0 KB, 4 views)

Tags

ansys, cfd, fluent, moment coefficient

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