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Completely solve and provide the diagram. Box the final answers. Use 4 decimals in all instances. Problem: A 25 MW Gas Turbine power plant operating on a simple open cycle system gives the following data: Air inlet temperature = 300 K Air inlet pressure = 101.325 kPa Pressure ratio = 4 Temperature after combustion = 1150 K Compressor adiabatic efficiency = 92% %3D Compressor mechanical efficiency = 87% Turbine mechanical efficiency = 80% Generator efficiency = 96% Heating value = 41,680 kJ/kg Combustion losses = 10% For air and gas mixture, Cp = 1.005 kJ/kg-K ; R = 282 J/kg-K %3D Determine: a. The actual temperature entering the combustor in K b. Fuel air ratio c. Fuel consumption in kg/s d. The volume of air supplied in CFM

Completely solve and provide the diagram. Box the final answers. Use 4 decimals in all instances. Problem: A 25 MW Gas Turbine power plant operating on a simple open cycle system gives the following data: Air inlet temperature = 300 K Air inlet pressure = 101.325 kPa Pressure ratio = 4 Temperature after combustion = 1150 K Compressor adiabatic efficiency = 92% %3D Compressor mechanical efficiency = 87% Turbine mechanical efficiency = 80% Generator efficiency = 96% Heating value = 41,680 kJ/kg Combustion losses = 10% For air and gas mixture, Cp = 1.005 kJ/kg-K ; R = 282 J/kg-K %3D Determine: a. The actual temperature entering the combustor in K b. Fuel air ratio c. Fuel consumption in kg/s d. The volume of air supplied in CFM

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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Completely solve and provide the diagram. Box the final answers. Use 4 decimals in all instances. PLEASE WRITE LEGIBLY OR TYPEWRITE THE SOLUTIONS.

 

Completely solve and provide the diagram. Box the final answers. Use 4 decimals in all instances. Problem: A 25 MW Gas Turbine power plant operating on a simple open cycle system gives the following data: Air inlet temperature = 300 K Air inlet pressure = 101.325 kPa Pressure ratio = 4 Temperature after combustion = 1150 K Compressor adiabatic efficiency = 92% Compressor mechanical efficiency = 87% Turbine mechanical efficiency = 80% Generator efficiency = 96% Heating value = 41,680 kJ/kg Combustion losses = 10% For air and gas mixture, Cp = 1.005 kJ/kg-K ; R = 282 J/kg-K Determine: a. The actual temperature entering the combustor in K b. Fuel air ratio c. Fuel consumption in kg/s d. The volume of air supplied in CFM
Transcribed Image Text:Completely solve and provide the diagram. Box the final answers. Use 4 decimals in all instances. Problem: A 25 MW Gas Turbine power plant operating on a simple open cycle system gives the following data: Air inlet temperature = 300 K Air inlet pressure = 101.325 kPa Pressure ratio = 4 Temperature after combustion = 1150 K Compressor adiabatic efficiency = 92% Compressor mechanical efficiency = 87% Turbine mechanical efficiency = 80% Generator efficiency = 96% Heating value = 41,680 kJ/kg Combustion losses = 10% For air and gas mixture, Cp = 1.005 kJ/kg-K ; R = 282 J/kg-K Determine: a. The actual temperature entering the combustor in K b. Fuel air ratio c. Fuel consumption in kg/s d. The volume of air supplied in CFM
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