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The air entering a compressor with a pressure ratio of 10 at 100kPa at 27°C leaves at 600K. It enters the turbine at a temperature of 1300 K and exits at a temperature of 800 K. Since the power of the gas turbine is 10 MW, a) Draw the T-s diagram of the cycle  b) Find the amount of fluid circulating in the installation.  c) Find the adiabatic efficiencies of the gas turbine and the compressor.  d) Find net work  Note. Assume that the specific heat of heating of the air is constant. cp=1 kj/kgC  cv=07181 kj/kgC

The air entering a compressor with a pressure ratio of 10 at 100kPa at 27°C leaves at 600K. It enters the turbine at a temperature of 1300 K and exits at a temperature of 800 K. Since the power of the gas turbine is 10 MW, a) Draw the T-s diagram of the cycle  b) Find the amount of fluid circulating in the installation.  c) Find the adiabatic efficiencies of the gas turbine and the compressor.  d) Find net work  Note. Assume that the specific heat of heating of the air is constant. cp=1 kj/kgC  cv=07181 kj/kgC

Elements Of Electromagnetics
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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The air entering a compressor with a pressure ratio of 10 at 100kPa at 27°C leaves at 600K. It enters the turbine at a temperature of 1300 K and exits at a temperature of 800 K. Since the power of the gas turbine is 10 MW,

a) Draw the T-s diagram of the cycle 

b) Find the amount of fluid circulating in the installation. 

c) Find the adiabatic efficiencies of the gas turbine and the compressor. 

d) Find net work 

Note. Assume that the specific heat of heating of the air is constant.

cp=1 kj/kgC  cv=07181 kj/kgC

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