Engineering
Engineering, 11.07.2019 04:30, brandistrothma

Air enters a convergence-divergence nozzle with 1.5 mpa pressure, 700 k temperature and very low velocity. there is a normal shock wave stands at the exit of the nozzle with mach 2.6. 3.a determine the pressure, temperature and density before and after the nsw 3.b quantify the entropy change across the nsw. 3.c determine the velocities before and after the nsw

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