Question: For flow of air through a normal shock, the upstream conditions are V1 = 600 m/s, To1 = 500 K, and po1 = 700 kPa.

For flow of air through a normal shock, the upstream conditions are V1 = 600 m/s, To1 = 500 K, and po1 = 700 kPa. Compute the downstream conditions Ma2, V2, T2, p2, and po2.

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