A 10,000 lb airplane flying at sea level has a lift-drag relation given by Cp = 0.02 +0.05 CL2. It is equipped with a jet engine delivering 3000 lbs of thrust independent of flight speed. If the wing planform area is 200 ft, a) Determine the maximum and minimum speeds by an analytical method. b) Does the minimum speed seem theoretically possible? c) Why or why not? Hint: Assume L = W and T = D and set up a quadratic equation for q.