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 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

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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Question

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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