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A total-pressure probe is placed in a supersonic wind tunnel where T = 530°R and M = 2.0. A normal shock stands in front of the probe. Behind the shock, M2 = 0.577 and p2 = 5.76 psia. Find (a) the downstream stagnation pressure and stagnation temperature and (b) all fluid properties upstream from the shock. Show static and stagnation state points and the process path on a Ts diagram.
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Chapter 12 Solutions
Fox and McDonald's Introduction to Fluid Mechanics
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