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Consider a normal shock wave in air. The upstream conditions are given by M1=3, p1 = 1 atm, and r1 = 1.23 kg/m3. Calculate the downstream values of p2, T2, r2, M2, u2, p02 and T02. (Anderson 3.4)
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Consider a normal shock wave in air. The upstream conditions are given by M1=3, p1 = 1 atm, and r1 = 1.23 kg/m3. Calculate the downstream values of p2, T2, r2, M2, u2, p02 and T02. (Anderson 3.4)

User Simmy
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Consider a normal shock wave in air. The upstream conditions are given by M1=3, p-example-1
Consider a normal shock wave in air. The upstream conditions are given by M1=3, p-example-2
Consider a normal shock wave in air. The upstream conditions are given by M1=3, p-example-3
User Pablo Grisafi
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