An incident shock wave with wave angle (=30^{circ}) impinges on a straight wall. If the upstream flow

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An incident shock wave with wave angle \(=30^{\circ}\) impinges on a straight wall. If the upstream flow properties are \(M_{1}=2.8, p_{1}=1 \mathrm{~atm}\), and \(T_{1}=300 \mathrm{~K}\), calculate the pressure, temperature, Mach number, and total pressure downstream of the reflected wave.

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