The stagnation temperature in an airflow is (149^{circ} mathrm{C}) upstream and downstream from a normal shock wave.

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The stagnation temperature in an airflow is \(149^{\circ} \mathrm{C}\) upstream and downstream from a normal shock wave. The absolute stagnation pressure downstream from the shock wave is \(229.5 \mathrm{kPa}\). Through the wave the absolute pressure rises from 103.4 to \(138 \mathrm{kPa}\). Determine the velocities upstream and downstream from the wave.

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