Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 45 m/s and leaves at 100 kPa and 180 m/s. The inlet area of the nozzle is 110 cm.. Determine (a) the mass flow rate through the nozzle, (b) the exit temperature of the air, and (c) the exit area of the nozzle. The gas constant of air is 0.287 kPa.m/kg.K. The specific heat of air is c,= 1.02 kJ/kg."C. P = 300 kPa T = 200°C P2= 100 kPa V, = 180 m/s Air V = 45 m/s A, = 110 cm? FIGURE P5-39

Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 45 m/s and leaves at 100 kPa and 180 m/s. The inlet area of the nozzle is 110 cm.. Determine (a) the mass flow rate through the nozzle, (b) the exit temperature of the air, and (c) the exit area of the nozzle. The gas constant of air is 0.287 kPa.m/kg.K. The specific heat of air is c,= 1.02 kJ/kg."C. P = 300 kPa T = 200°C P2= 100 kPa V, = 180 m/s Air V = 45 m/s A, = 110 cm? FIGURE P5-39

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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