I am currently working on a final year project which involves the aerodynamics around an airfoil.
while I am familiar with the post processing activities with CFD software, I am not entirely sure how I can attain the Lift Coefficient (Cl) data from the CFD pressure and velocity data.
I know the mathematical relationship between Cl and Cp (pressure coefficient) but surely there must be a way to directly extract Cl from the Cp calculated by the software.
Thanks.