A gas turbine that has a 0.75 efficiency compressor that compresses up to 0.5 MPa, a combustion chamber where fuel of 45 MJ/kg is burned that gives a temperature output of 900 K, a 0.85 efficiency turbine that is responsible for moving the compressor, and another 0.8 efficiency turbine that generates the necessary net power, which can be varied from 0 to 200 kW with a throttle valve between the turbines. Calculate: 1. Compressor outlet temperature 2. Pressure and outlet temperature of the first turbine.
A gas turbine that has a 0.75 efficiency compressor that compresses up to 0.5 MPa, a combustion chamber where fuel of 45 MJ/kg is burned that gives a temperature output of 900 K, a 0.85 efficiency turbine that is responsible for moving the compressor, and another 0.8 efficiency turbine that generates the necessary net power, which can be varied from 0 to 200 kW with a throttle valve between the turbines. Calculate: 1. Compressor outlet temperature 2. Pressure and outlet temperature of the first turbine.
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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A gas turbine that has a 0.75 efficiency compressor that compresses up to 0.5 MPa, a combustion chamber where fuel of 45 MJ/kg is burned that gives a temperature output of 900 K, a 0.85 efficiency turbine that is responsible for moving the compressor, and another 0.8 efficiency turbine that generates the necessary net power, which can be varied from 0 to 200 kW with a throttle valve between the turbines. Calculate:
1. Compressor outlet temperature
2. Pressure and outlet temperature of the first turbine.
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