In a jet engine, the emitter, compressor, turbine and Lule are isanthropic, while the combustion chamber operates at constant pressure.At the emitter Inlet, the air temperature is 230 K, the pressure is 25 kPa, the flow is 30 kg/s and the speed is 200 m/s.According to the pressure of the air at the compressor outlet is 500 kPa, the temperature of the air at the turbine inlet is 1000 K and the pressure of the air at the Lule outlet is 25 kPa, a) schematically draw the flow diagram of the cycle. b) find the speed of gases at the exit of the Lule. c) find the amount of heat supplied to the combustion chamber. d) find the Response Force, Response power and response efficiency.

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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In a jet engine, the emitter, compressor, turbine and Lule are isanthropic, while the combustion chamber operates at constant pressure.At the emitter Inlet, the air temperature is 230 K, the pressure is 25 kPa, the flow is 30 kg/s and the speed is 200 m/s.According to the pressure of the air at the compressor outlet is 500 kPa, the temperature of the air at the turbine inlet is 1000 K and the pressure of the air at the Lule outlet is 25 kPa, a) schematically draw the flow diagram of the cycle. b) find the speed of gases at the exit of the Lule. c) find the amount of heat supplied to the combustion chamber. d) find the Response Force, Response power and response efficiency.
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