Air flows through a convergent-divergent nozzle from a


Question: Air flows through a convergent-divergent nozzle from a large reservoir in which the pressure is 300 kPa and the temperature is 100°C. The nozzle has a throat area of 1 cm2 and an exit area of 4 cm2. The nozzle discharges into another large reservoir in which the pressure can be varied. For what range of back-pressures will the mass flow rate through the nozzle be constant and what will the mass flow rate be under these circumstances?

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Mechanical Engineering: Air flows through a convergent-divergent nozzle from a
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