Question: A two - dimensional oblique shock diffuser operates in a supersonic stream of air as shown in below figure. If P 1 = 1 0

A two-dimensional oblique shock diffuser operates in a supersonic stream of air as shown in below figure. If P1=101,3kPa and M1=2.3, Determine the pressure, the Mach number, and the deflection of (angle ) in regions 3 and 5. Assume that the flow in the various regions downstream of the oblique shockwaves is supersonic.
A two - dimensional oblique shock diffuser

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