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What is the Basic Calculation of Lift Coef In Modelling 2D??

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October 14, 2009, 05:52	What is the Basic Calculation of FLUENT on Computing Lift Coef In Modelling 2D??	#1
teguhtf Senior Member teguh hady Join Date: Aug 2009 Location: Saga, Japan Posts: 222 Rep Power: 19	Hello All!!! I wanna find Lift coefficient of an airfoil. My drawing is 2D. Do you know the basic calculation of FLUENT in computing Lift coefficient in 2D?? Because the equation of CL = L/(qA). where L is the lift force, q is dynamic pressure, and A is planform area. If A is zero then CL is infinite. (2D has no planform area(A)) Can you tell me?? What is the Basic Calculation of FLUENT on Computing Lift Coef In Modelling 2D?? thanks teguhtf Last edited by teguhtf; October 14, 2009 at 14:19. Reason: completing

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