A wing with a trapezoidal planform is shown below. If the velocity is 132 ft/s, the density of air is 1.88 X10-3 slug ft3 , and the weight of the airplane using this wing is 1,060 lb, determine the amount of drag generated by the wing. Assume the airplane is undergoing steady flight. The span efficiency factor is 1. Cbase =4.1 ft Ctip = 3.3 ft b = 11.9 ft Provide your answer in pounds. 2.0 1.5 1.0 Sectional Lift Coefficient [-] 0.5 0.0