Engineering, 14.09.2019 02:30, ravensenpai423

Air enters an isentropic nozzle at 360 kpa, 8 m/sec and 540 k. the nozzle exit pressure is 90 kpa. calculate the temperature and velocity of the airflow at the nozzle exit using a) exact analysis (variable specific heats) b) approximate analysis (constant specific heats; assume that specific heat ratio (k) for air is 141

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Air enters an isentropic nozzle at 360 kpa, 8 m/sec and 540 k. the nozzle exit pressure is 90 kpa. c...