An aircraft wing has an aerodynamic load q;(x)-q0 (1-(x/L)2), that acts upward in a distributed manner as shown. Under very specific conditions, the load function is parabolic. The wing mass results in 200 Ibs, at 7 feet from the edge of the fuselage and will act downward. Lis the wing length and is 24 feet. At the fuselage, the max value of the parabola is qo=200 lbs./ft. Based on the given parameters, what reactions on the wing must the fuselage provide for equilibrium? Enter your answer below. Keep your scratch work for submission to the appropriate assignment in Canvas. 9:(x) 200 Ibs./ft Fuselago Wing L 24 ft ft 200 lbs.