The flow is turned using a compression ramp and an expansion corner. if the approach flow mach number is, m=3, approach flow static pressure is, p1=1 atm, and the ramp angle is 10 degrees, a) (10 pts) calculate the mach number after the compression ramp. b) (10 pts) calculate the flow turning angle, t, required to achieve m=3 after the expansion corner. c) (10 pts) calculate the total pressure after the compression corner. d) (10 pts) calculate the static pressure after the expansion corner.