Question: Consider an oblique shock wave generated by a compression corner with a 1 0 0 deflection angle. The Mach number of the flow ahead of

Consider an oblique shock wave generated by a compression corner with a

10^{0}

deflection angle. The Mach number of the flow ahead of the corner is

3.6 .

The flow pressure and temperature are

10^{5} \frac{N}{m^{2}}, 300^{0} K .

The oblique shock wave subsequently impinges on a straight wall opposite the compression corner. Calculate the angle of the reflected shock wave relative to the straight wall. Also, obtain the pressure, temperature, and Mach number behind the reflected wave.

10

Consider an oblique shock wave generated by a

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