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 inlettemperature is 1480 K. Determine:P2Pi82CompressorP₁=98 kPaT₁=320 KHeat exchangerHeat exchangerCourT3 = 1480 KTurbinea. The mass flow rateb. The backwards ratioc. The rate of Heat addition to the systemd. Thermal efficiencycycleTT3=1480 KP= 784 kPaP=98 kPaT₁= 320 KS

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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: Pi 8 2 gin Heat exchanger 3 T3= 1480 K Fal T T3=1480 K kPa

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: Pi 8 2 gin Heat exchanger 3 T3= 1480 K Fal T T3=1480 K kPa

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

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:
P2
Pi
8
2
Compressor
P₁=98 kPa
T₁=320 K
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

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