A Brayton cycle inlet is at 300 K. Inlet and exit temperatures of the turbine is measured as 1800 K and 710 K, respectively. The compressor pressure ratio is 13. Use cold air-standard approach to calculate the thermal efficiency of the cycle.

Elements Of Electromagnetics
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Author:Sadiku, Matthew N. O.
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Can you help me with this one please. Temperatures are in Kelvin unit.

A Brayton cycle inlet is at 300 K. Inlet and exit temperatures of the turbine is measured as
1800 K and 710 K, respectively. The compressor pressure ratio is 13. Use cold air-standard
approach to calculate the thermal efficiency of the cycle.
BURNER-
COMPR.
TURBINE
a. 0.35
O b. 0.40
C. 0.45
d. 0.50
e. 0.55
f. 0.60
g. 0.65
Seçimimi temizle
Transcribed Image Text:A Brayton cycle inlet is at 300 K. Inlet and exit temperatures of the turbine is measured as 1800 K and 710 K, respectively. The compressor pressure ratio is 13. Use cold air-standard approach to calculate the thermal efficiency of the cycle. BURNER- COMPR. TURBINE a. 0.35 O b. 0.40 C. 0.45 d. 0.50 e. 0.55 f. 0.60 g. 0.65 Seçimimi temizle
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