pinkplum596 pinkplum596

06-03-2020
Engineering

contestada

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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mirianmoses mirianmoses

08-03-2020

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