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Airfoil computation

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April 9, 2008, 23:32	Airfoil computation	#1
shan Guest Posts: n/a	Sponsored Links I have done simulation on 2D airfoil. coefficient of lift and drag are known.Is it possible to compute Torque generated from cl & cd or is there any other option in fluent which calculates torque generated.Also will the same method will be used if we compute for 3D airfoil.

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April 10, 2008, 07:50	Re: Airfoil computation	#2
Greg Guest Posts: n/a	In report-force, you have "moments", it is the torque from lift+drag around the point you imput the coordinate.

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