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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
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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Please use the air standerd analysis instead of the cold air standerd analysis

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: PA 8 2 Compressor P₁=98 kPa T₁=320 K lin Heat exchanger Heat exchanger Lout 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
Transcribed Image Text: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: PA 8 2 Compressor P₁=98 kPa T₁=320 K lin Heat exchanger Heat exchanger Lout 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
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