The rate of change of moment coefficient with respect to the angle of attack, dCm/dα , at half chord point of a thin airfoil, as per approximations from t...

For a thin flat plate at 2 degrees angle of attack, the pitching moment coefficient about the trailing edge is

Consider a NACA 0012 aerofoil of chord c in a freestream with velocity V∞ at a non-zero positive angle of attack α. The average time-of-flight for a...