SOLVED: A cambered airfoil has a pitching moment coefficient about the aerodynamic center of -0.025. Estimate the position of the center of pressure when the airfoil is at 3 degrees angle of attack and the lift coefficient is 0.325. The dynamic pressure is 90 N/m^2.A. At 47% of the chordB. At 38% of the chordC. None of the aboveD. At 42.5% of the chordE. At 35% of the chordF. At 27% of the chord

Which Airfoil Should I Use?

Consider an airfoil with a circular arc camber line (maximum ca... | Filo