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May 6, 2010, 14:11	Fluent results	#1
arjit New Member Arjit Arora Join Date: Mar 2010 Posts: 11 Rep Power: 16	Hi! On analyzing a 3D wing in fluent, it gave me the following results for force 1. Upward for on the top surface of the wing : 111N 2. Upward force on the bottom surface of the wing : -51N Net result: 60 N lifts! Why am i getting a negative lift for the lower surface?? Conditions: Angle of attack = 8degress Boundary conditions: Velocity inlet at 15m/s, outflow.. wing=wall. other walls = symmetry

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