Q(2-3)A gas-turbine power plant operates on Brayton cycle. The air pressure inside the combustion chamber is 1100 kPa. The pressure at the turbine exist is 1.10 bar. Using local thermometers on site, the maximum temperature reached in the system is 1311 K while the minimum temperature in the system is 22C. The working fluid is air, which enters the compressor at a rate of 120 m3/min and leaves the turbine at 460°C. Assume the compressor has no deviation. Determine: The compression ratio Turbine isentropic efficiency % Actual temperature inter the combustion chamber in K The not nower cutput in M/day

Q(2-3)A gas-turbine power plant operates on Brayton cycle. The air pressure inside the combustion chamber is 1100 kPa. The pressure at the turbine exist is 1.10 bar. Using local thermometers on site, the maximum temperature reached in the system is 1311 K while the minimum temperature in the system is 22C. The working fluid is air, which enters the compressor at a rate of 120 m3/min and leaves the turbine at 460°C. Assume the compressor has no deviation. Determine: The compression ratio Turbine isentropic efficiency % Actual temperature inter the combustion chamber in K The not nower cutput in M/day

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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