Air approaches a normal shock at (M_{1}=2.5), with (T_{0_{1}}=1250^{circ} mathrm{R}) and (p_{1}=20) psia. Determine the speed and

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Air approaches a normal shock at \(M_{1}=2.5\), with \(T_{0_{1}}=1250^{\circ} \mathrm{R}\) and \(p_{1}=20\) psia. Determine the speed and temperature of the air leaving the shock and the entropy change across the shock.

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Ali Khawaja

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