Air enters the compressor of an ideal air-standard Brayton cycle at P1-98 kPa and T1-320 K, with a volumetric flow rate of 15 m3/s. The compressor pressure ratio is 8. The turbine inlet temperature is 1480 K. Determine: Compressor P₁=98 kPa T₁=320 K lin Heat exchanger Heat exchanger Cour T3= 1480 K Turbine a. The mass flow rate b. The backwards ratio c. The rate of Heat addition to the system d. Thermal efficiency cycle T T3=1480 K P= 784 kPa P=98 kPa T₁= 320 K S

Air enters the compressor of an ideal air-standard Brayton cycle at P1-98 kPa and T1-320 K, with a volumetric flow rate of 15 m3/s. The compressor pressure ratio is 8. The turbine inlet temperature is 1480 K. Determine: Compressor P₁=98 kPa T₁=320 K lin Heat exchanger Heat exchanger Cour T3= 1480 K Turbine a. The mass flow rate b. The backwards ratio c. The rate of Heat addition to the system d. Thermal efficiency cycle T T3=1480 K P= 784 kPa P=98 kPa T₁= 320 K S

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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