I need the answer as soon as possible A gas turbine power plant operating on Brayton cycle shown in figure.The air enters the compressor at 300 K and exits at 700 KThe pressure ratio for compressor is 7.The gas enters the turbine at 1600K, 600 kPaand exits at 1050 K, 100 kPa.FuelT₁ = 700K√₂=7 commuor=45T₁= 300k Fresh airCombustion Chamber T₁ = 1600 kP₂=600kPa1 and(TarbingExt ges-1050 KP = 100 kBelow 30%Between 30% and 40%Between 40% and 50%Between 50% and 60%Above 60%(2* The adiabatic efficiency of turbine is:Below 50%Between 50% and 55%Between 55% and 60%Between 60% and 65%Above 65%* Input work to compressor in (kJ/ kg); isBelow 400Between 400 and 410Between 410 and 420Between 420 and 430 OAbove 430*: The turbine work in (kJ/kg) isBelow 200Between 200 and 400Between 400 and 600Between 600 and 800Above 800 O

For the Brayton cycle, r = compression ratio of the compressor = 7 T1 = 300 oCT2 = 700 oC P3 = 600…

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 T₁ Fook- 7 commer Ti= 300k Fresh air (2. Combustion Chamber T31600 k Py =600 kPa Torbing hat -1050 K P = 100 kP Below 30% O Exhaust gas Between 30% and 40% Between 40% and 50% O Between 50% and 60% Above 60% * The adiabatic efficiency of turbine is : Below 50% O Between 50% and 55% Between 55% and 60% O Between 60% and 65% Above 65% *Input work to compressor in (kJ/kg) ; is Below 400 Between 400 and 410 Between 410 and 420 O Between 420 and 430 O Above 430 *: The turbine work in (kJ/kg) is Below 200 Between 200 and 400 O Between 400 and 600 Between 600 and 800 Above 800 O

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 T₁ Fook- 7 commer Ti= 300k Fresh air (2. Combustion Chamber T31600 k Py =600 kPa Torbing hat -1050 K P = 100 kP Below 30% O Exhaust gas Between 30% and 40% Between 40% and 50% O Between 50% and 60% Above 60% * The adiabatic efficiency of turbine is : Below 50% O Between 50% and 55% Between 55% and 60% O Between 60% and 65% Above 65% Input work to compressor in (kJ/kg) ; is Below 400 Between 400 and 410 Between 410 and 420 O Between 420 and 430 O Above 430 : The turbine work in (kJ/kg) is Below 200 Between 200 and 400 O Between 400 and 600 Between 600 and 800 Above 800 O

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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