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Moment Calculation for a simple wing geometry

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November 11, 2022, 13:56	Moment Calculation for a simple wing geometry	#1
shariq12 New Member shariq Join Date: Jul 2022 Posts: 7 Rep Power: 4	Hello everyone, I'm Simulating a simple wing in Ansys and trying to validate the results obtained using XFLR, I'm able to get a good agreement on Cl however I'm not able to match my Cm, What could be the reason?. Also is there a way to find out where my net lift is acting on the wing so that I can manually compute moment

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lift and drag calculation, moment coefficient, wing simulation

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