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Determine a the mass flow rate through the nozzle b the

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Reference no: EM13643110

Air enters an adiabatic nozzle steadily at 300 kPa, 200 degree Cesius, and 30 m/s and leaves at 100 kPa and 180 m/s. The inlet area of the 80 cm^2. Determine (a) the mass flow rate through the nozzle, (b) the exit temperature exit temperature of the air, and (c) the exit area of the nozzle. Note: can you include the page for the table used to get values.

Reference no: EM13643110

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