2) A gas turbine cycle has two stages of compression with an intercooler between the stages. Air enters the first stage at 27 °C, each stage has an isentropic efficiency of 80 %. Air exits the intercooler at 55 °C. The cycle has a single turbine stage with a pressure ratio of 26 and has an isentropic efficiency of 88 %. Find the exit temperature of the second stage of the compressor. a. 298 °C. b. 249 °C. c. 686 °C. d. 160 °C

Elements Of Electromagnetics
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е. 74
2) A gas turbine cycle has two stages of compression with an intercooler between the stages. Air enters
the first stage at 27 °C, each stage has an isentropic efficiency of 80 %. Air exits the intercooler at 55 °C.
The cycle has a single turbine stage with a pressure ratio of 26 and has an isentropic efficiency of 88 %.
Find the exit temperature of the second stage of the compressor.
а. 298 °С.
b. 249 °С.
c. 686 °C.
d. 160 °C
Transcribed Image Text:е. 74 2) A gas turbine cycle has two stages of compression with an intercooler between the stages. Air enters the first stage at 27 °C, each stage has an isentropic efficiency of 80 %. Air exits the intercooler at 55 °C. The cycle has a single turbine stage with a pressure ratio of 26 and has an isentropic efficiency of 88 %. Find the exit temperature of the second stage of the compressor. а. 298 °С. b. 249 °С. c. 686 °C. d. 160 °C
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