A gas-turbine power plant operating on an ideal Brayton cycle has a pressure ratio of 8. The gas temperature is 300 K at the compressor inlet and 1300 K at the turbine inlet. Utilizing the air-standard assumptions, determine (a) the gas temperature at the exits of the compressor and the turbine, (b) the back-work ratio, and (c) the thermal efficiency.

Elements Of Electromagnetics
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Author:Sadiku, Matthew N. O.
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A gas-turbine power plant operating on an ideal Brayton cycle has a pressure ratio of 8. The gas temperature is 300 K at the compressor inlet and 1300 K at the turbine inlet. Utilizing the air-standard assumptions, determine (a) the gas temperature at the exits of the compressor and the turbine, (b) the back-work ratio, and (c) the thermal efficiency.
1. A gas-turbine power plant operating on an ideal Brayton cycle has a pressure
ratio of 8. The gas temperature is 300 K at the compressor inlet and 1300 K at
the turbine inlet. Utilizing the air-standard assumptions, determine (a) the gas
temperature at the exits of the compressor and the turbine, (b) the back-work
ratio, and (c) the thermal efficiency.
T, K†
1300
W.
turb
din
P = const.
4
'p = 8
2
Tout
comp
300
P= const.
1
Transcribed Image Text:1. A gas-turbine power plant operating on an ideal Brayton cycle has a pressure ratio of 8. The gas temperature is 300 K at the compressor inlet and 1300 K at the turbine inlet. Utilizing the air-standard assumptions, determine (a) the gas temperature at the exits of the compressor and the turbine, (b) the back-work ratio, and (c) the thermal efficiency. T, K† 1300 W. turb din P = const. 4 'p = 8 2 Tout comp 300 P= const. 1
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