Determine mass flow rate of air through the nozzle

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Reference no: EM13704048

Air enters an adiabatic nozzle steadily at 300 kPa, 200oC, and 30 m/s and leaves at 100 kPa and 180 m/s. The inlet area of the nozzle is 80 cm2. Determine:

(a) Mass flow rate of air through the nozzle

(b) The exit temperature of the air

(c) The exit area of the nozzle

Reference no: EM13704048

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