Consider the flow over a cone of 20 half cone angle, at zero angle of attack. a. For a free stream Mach number of M = 2.5 (assume standard see level conditions), evaluate the shock wave angle, p, T, p, and M immediately behind the shock wave and on the cone surface. b. Evaluate the minimum free stream Mach number for the flow to remain attached. C. Evaluate the drag coefficient for the Mach number range of 1.5