Engineering, 07.03.2020 02:57 Itasouu
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 =...
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