Question: A two dimensional oblique shock diffuser operates in a supersonic stream of air at an angle of attack 5o as shown in the figure below.

A two dimensional oblique shock diffuser operates in a supersonic stream of air at an angle of attack 5o as shown in the figure below. If P1=101.3 kPa and M1=2.3 determine the pressures, the Mach numbers, and the direction of flow in regions 3 and 5. 10 M, -23 P- 101.3 kPa Slip line

10 M, -23 P- 101.3 kPa Slip line

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