A huge reservoir of air supplies a converging-diverging

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A huge reservoir of air supplies a converging-diverging nozzle with throat and exit areas of 10 cm^2 and 25 cm^2 respectively. The reservoir pressure and temperature are 150 kPa and 20C. Determine the range of back pressure over which
1. normal shocks appear in the nozzle
2. Oblique shocks form at the exit
3. Expansion waves form at the exit

Reference no: EM13294532

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