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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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](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F882dd77d-3d57-44ea-a5c8-2fa33ce787a8%2F09a3358e-5340-46f3-9918-274b94b9e6ce%2Fekmzu5_processed.png&w=3840&q=75)
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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