What is the Basic Calculation of FLUENT on Computing Lift Coef In Modelling 2D??
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
Can you tell me?? What is the Basic Calculation of FLUENT on Computing Lift Coef In Modelling 2D?? thanks teguhtf |
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