Hello,
I have a question regarding drag on a moving airfoil, as in a wind turbine. In the simplest form, say an airfoil is moving forward at zero angle of attack at a speed V with a tail wind of U. Is the drag:
a.) D = Cd*1/2*rho*A*(U^2-V^2)
b.) D= Cd*1/2*rho*A*(U-V)^2
Difference of the...