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 1600 K, 600 kPaand exits at 1050 K, 100 kPa.FuelT₁ Fook-=(6₂=7 commuor45T₁= 300k Fresh airTJCombustion Chamber Ts = 1600 kP₂=600kPa1 andTarbingExt ges-1050 KP=100 kBelow 30%Between 30% and 40%Between 40% and 50%Between 50% and 60%Above 60%12* 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 200 OBetween 200 and 400Between 400 and 600Between 600 and 800Above 800 O

given; inlet compressor temperature(T1)=300kexit compressor temperature(T2)=700kturbine inlet…

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 Toe Zook ( 6=7 commur T₁= 300k + fresh air Combustion Chamber Tj = 1600 K Py = 600kPa Tarbing Tut T-1050 K Exhaust ges P = 100 kP Below 30% O Between 30% and 40% O Between 40% and 50% Between 50% and 60% O Above 60% O 12** The adiabatic efficiency of turbine is Below 50% O Between 50% and 55% O Between 55% and 60% O Between 60% and 65% O Above 65% O Input work to compressor in (kJ/kg) ; is Below 400 O Between 400 and 410 Between 410 and 420 O Between 420 and 430 Above 430 O *: The turbine work in (kJ/kg) is Below 200 O Between 200 and 400 O Between 400 and 600 Between 600 and 800 Above 800

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 Toe Zook ( 6=7 commur T₁= 300k + fresh air Combustion Chamber Tj = 1600 K Py = 600kPa Tarbing Tut T-1050 K Exhaust ges P = 100 kP Below 30% O Between 30% and 40% O Between 40% and 50% Between 50% and 60% O Above 60% O 12** The adiabatic efficiency of turbine is Below 50% O Between 50% and 55% O Between 55% and 60% O Between 60% and 65% O Above 65% O Input work to compressor in (kJ/kg) ; is Below 400 O Between 400 and 410 Between 410 and 420 O Between 420 and 430 Above 430 O *: The turbine work in (kJ/kg) is Below 200 O Between 200 and 400 O Between 400 and 600 Between 600 and 800 Above 800

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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