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Examine the following open gas turbine process. The temperature of the inlet air is 292 K and pressure is 100 kPa. The polytropic efficiency of the compressor is 85.0 % and pressure ratio is 8. The heat flow rate (fuel power) into process is 1.25 MW. The maximum temperature of the process (after combustion chamber) is 1560 K and the polytropic efficiency of the turbine is 86.0 %. The mass flow rate of air is 1.063 kg/s. A constant specific heat cp = 1.15 kJ/kgk can be used for the working fluid. Combustion chamber can be considered as adiabatic. Fuel Air in Calculate: C 21 CH 3 1) Temperature after compressor T2 2) Compressor power Pc 3) Temperature after turbine T4 4) Turbine power Pt 5) Thermal efficiency of the system t T Flue gas K (with zero decimal accuracy) MW (with three decimal accuracy) K (with zero decimal accuracy) MW (with three decimal accuracy) % (with one decimal accuracy)

Examine the following open gas turbine process. The temperature of the inlet air is 292 K and pressure is 100 kPa. The polytropic efficiency of the compressor is 85.0 % and pressure ratio is 8. The heat flow rate (fuel power) into process is 1.25 MW. The maximum temperature of the process (after combustion chamber) is 1560 K and the polytropic efficiency of the turbine is 86.0 %. The mass flow rate of air is 1.063 kg/s. A constant specific heat cp = 1.15 kJ/kgk can be used for the working fluid. Combustion chamber can be considered as adiabatic. Fuel Air in Calculate: C 21 CH 3 1) Temperature after compressor T2 2) Compressor power Pc 3) Temperature after turbine T4 4) Turbine power Pt 5) Thermal efficiency of the system t T Flue gas K (with zero decimal accuracy) MW (with three decimal accuracy) K (with zero decimal accuracy) MW (with three decimal accuracy) % (with one decimal accuracy)

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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Please do not rely too much on chatgpt, because its answer may be wrong. Please consider it carefully and give your own answer. You can borrow ideas from gpt, but please do not believe its answer.
Very very grateful!

Examine the following open gas turbine process. The temperature of the inlet air is 292 K and pressure is 100 kPa. The polytropic efficiency of the compressor is 85.0 % and pressure ratio is 8. The heat flow rate (fuel power) into process is 1.25 MW. The maximum temperature of the process (after combustion chamber) is 1560 K and the polytropic efficiency of the turbine is 86.0 %. The mass flow rate of air is 1.063 kg/s. A constant specific heat Cp 1.15 kJ/kgk can be used for the working fluid. Combustion chamber can be considered as adiabatic. = Air in Calculate: 2 Fuel CH 3 1) Temperature after compressor T₂ 2) Compressor power Pc 3) Temperature after turbine T4 4) Turbine power Pt 5) Thermal efficiency of the system nt Flue gas K (with zero decimal accuracy) MW (with three decimal accuracy) K (with zero decimal accuracy) MW (with three decimal accuracy) % (with one decimal accuracy)
Transcribed Image Text:Examine the following open gas turbine process. The temperature of the inlet air is 292 K and pressure is 100 kPa. The polytropic efficiency of the compressor is 85.0 % and pressure ratio is 8. The heat flow rate (fuel power) into process is 1.25 MW. The maximum temperature of the process (after combustion chamber) is 1560 K and the polytropic efficiency of the turbine is 86.0 %. The mass flow rate of air is 1.063 kg/s. A constant specific heat Cp 1.15 kJ/kgk can be used for the working fluid. Combustion chamber can be considered as adiabatic. = Air in Calculate: 2 Fuel CH 3 1) Temperature after compressor T₂ 2) Compressor power Pc 3) Temperature after turbine T4 4) Turbine power Pt 5) Thermal efficiency of the system nt Flue gas K (with zero decimal accuracy) MW (with three decimal accuracy) K (with zero decimal accuracy) MW (with three decimal accuracy) % (with one decimal accuracy)
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