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Engineering, 02.11.2019 05:31 cowerdwhisper23

Air enters an adiabatic nozzle steadily at 500 kpa, 100°c and 30 m/s and leaves at 100 kpa and 240 m/s. the inlet area of the nozzle is 50 cm2 . determine (a) the mass flow rate through the nozzle, (b) the exit temperature of the air, and (c) the exit area of the nozzle. to save time use constant specific heats evaluated at 300 °k.

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