Air enters a turbojet engine at 254 K, 57 kPa and 293 m/s. The pressure ratio across the compressor is 14.5 and the work developed by the turbine equals the compressor work input. If 700 kJ/kg of heat is transferred to air in the combustion chamber, calculate the velocity of air at the exit of the engine, in m/s. Properties of air: Cy=0.718 kJ/(kgK), Cp=1.005 kJ/(kgK), R=0.287 kJ/(kgK), k=1.4
Air enters a turbojet engine at 254 K, 57 kPa and 293 m/s. The pressure ratio across the compressor is 14.5 and the work developed by the turbine equals the compressor work input. If 700 kJ/kg of heat is transferred to air in the combustion chamber, calculate the velocity of air at the exit of the engine, in m/s. Properties of air: Cy=0.718 kJ/(kgK), Cp=1.005 kJ/(kgK), R=0.287 kJ/(kgK), k=1.4
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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![Air enters a turbojet engine at 254 K, 57 kPa and 293 m/s. The pressure ratio across
the compressor is 14.5 and the work developed by the turbine equals the compressor
work input. If 700 kJ/kg of heat is transferred to air in the combustion chamber,
calculate the velocity of air at the exit of the engine, in m/s.
Properties of air: Cv=0.718 kJ/(kgK), C,=1.005 kJ/(kgK), R=0.287 kJ/(kgK), k=1.4](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Ff99ef7b5-45a2-4d46-a89f-b0f5a771704a%2Ff5a2ef99-12d8-4c78-ac3b-c99e75b29d00%2Fpo9tv6_processed.png&w=3840&q=75)
Transcribed Image Text:Air enters a turbojet engine at 254 K, 57 kPa and 293 m/s. The pressure ratio across
the compressor is 14.5 and the work developed by the turbine equals the compressor
work input. If 700 kJ/kg of heat is transferred to air in the combustion chamber,
calculate the velocity of air at the exit of the engine, in m/s.
Properties of air: Cv=0.718 kJ/(kgK), C,=1.005 kJ/(kgK), R=0.287 kJ/(kgK), k=1.4
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