B) Write a program in MATLAB that would answer all the questions below Drag can be calculated with the drag equation, = 22 Where, Cd = drag coefficient, which is determined experimentally, usually in a wind tunnel, = air density, V= velocity of the aircraft, A= reference area (the surface area over which the air flows) Although the drag coefficient is not a constant, it can be taken to be constant at low speeds (less than 200 mph). Suppose the following data were measured in a wind tunnel: drag = 20,000 N = 110-6 kg / m3 V = 100 mph (HINT: convert this to meters per second) A = 1 m2 1) Calculate the drag coefficient. 2) Use the drag coefficient to predict how much drag will be exerted on the aircraft at velocities from 0 mph to 200 mph. 3) Create a table of your results obtained in the previous problem (2)