An airplane is in trimmed flight and has a weight of 4500 lb. the distance between the aerodynamic center of the wing to the aerodynamic center of the tail is 20 ft. assume that there is no pitching moment at the aerodynamic center of the wing or at the aerodynamic center of the tail. also, neglect any drag influence on the pitching moment of the aircraft.1. calculate the location of the center of gravity of the trimmed aircraft when the wing produces 90% of the needed lift and the tail produces 10% of the needed lift. measure the location of the center of gravity as a distance aft of the wing aerodynamic center