Answer to Question #304419 in Engineering for BALAJI A

Question

Design a fixed area internal compression inlet that will start at M0 = 2.9 for an aircraft that will cruise at Mach number of 2.4, Determine the

following Capture to throat area ratio AC / A t . Determine efficiency of the inlet after starting at M0 = 2.9 and the shock located at the throat.

Determine efficiency of the inlet after starting at M0 = 2.4 and the shock located at the throat. Determine the Mach number at which the inlet will

un-start.