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A gas turbine power plant operating on Brayton cycle shown in figure. The air enters the compressor at 300 K and exits at 700 K. The pressure ratio for compressor is 7. The gas enters the turbine at 1600 K, 600 kPa and exits at 1050 K, 100 kPa. Fuel Find Work In put work efficiency To - 1600 k

A gas turbine power plant operating on Brayton cycle shown in figure. The air enters the compressor at 300 K and exits at 700 K. The pressure ratio for compressor is 7. The gas enters the turbine at 1600 K, 600 kPa and exits at 1050 K, 100 kPa. Fuel Find Work In put work efficiency To - 1600 k

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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A gas turbine power plant operating on Brayton cycle shown in figure. The air enters the compressor at 300 K and exits at 700 K. The pressure ratio for compressor is 7. The gas enters the turbine at 1600 K, 600 kPa and exits at 1050 K, 100 kPa. Fuel T₂ = 700k. p=7 Compressor T₁ = 300k Fresh air Combustion Chamber Turbine Find Work T3 = 1600 K P3=600 кра Exhaust gas In put work efficiency we net =1050 K P4=100 kPa
Transcribed Image Text:A gas turbine power plant operating on Brayton cycle shown in figure. The air enters the compressor at 300 K and exits at 700 K. The pressure ratio for compressor is 7. The gas enters the turbine at 1600 K, 600 kPa and exits at 1050 K, 100 kPa. Fuel T₂ = 700k. p=7 Compressor T₁ = 300k Fresh air Combustion Chamber Turbine Find Work T3 = 1600 K P3=600 кра Exhaust gas In put work efficiency we net =1050 K P4=100 kPa
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