An ideal Brayton or gas turbine cycle with air as the working medium operates between pressures of 15 psia and 90 lb. The compressor inlet temperatures is 70°F and the turbine inlet temperature is 1240°F. Determine the thermal efficiency. a. 0.39 b. 0.49 c. 0.59 d. 0.69 An ideal Brayton or gas turbine cycle with air as the working medium operates between pressures of 15

Elements Of Electromagnetics
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An ideal Brayton or gas turbine cycle with air as the working medium operates between pressures of 15
psia and 90 lb. The compressor inlet temperatures is 70°F and the turbine inlet temperature is 1240°F.
Determine the thermal efficiency.
a. 0.39
b. 0.49
c. 0.59
d. 0.69
An ideal Brayton or gas turbine cycle with air as the working medium operates between pressures of 15
psia and 90 lb. The compressor inlet temperatures is 70°F and the turbine inlet temperature is 1240°F.
Determine the internal work-ratio.
a. 0.21
b. 0.31
c. 0.41
d. 0.51
An ideal Brayton or gas turbine cycle with air as the working medium operates between pressures of 15
psia and 90 lb. The compressor inlet temperatures is 70°F and the turbine inlet temperature is 1240°F.
The efficiency of the turbine and compressor is both 80%. Determine the thermal efficiency.
a. 0.344
b. 0.244
c. 0.144
d. 0.044
Transcribed Image Text:An ideal Brayton or gas turbine cycle with air as the working medium operates between pressures of 15 psia and 90 lb. The compressor inlet temperatures is 70°F and the turbine inlet temperature is 1240°F. Determine the thermal efficiency. a. 0.39 b. 0.49 c. 0.59 d. 0.69 An ideal Brayton or gas turbine cycle with air as the working medium operates between pressures of 15 psia and 90 lb. The compressor inlet temperatures is 70°F and the turbine inlet temperature is 1240°F. Determine the internal work-ratio. a. 0.21 b. 0.31 c. 0.41 d. 0.51 An ideal Brayton or gas turbine cycle with air as the working medium operates between pressures of 15 psia and 90 lb. The compressor inlet temperatures is 70°F and the turbine inlet temperature is 1240°F. The efficiency of the turbine and compressor is both 80%. Determine the thermal efficiency. a. 0.344 b. 0.244 c. 0.144 d. 0.044
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