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Analyze a Gas turbine engine at a design speed under the following data employing a ...

Analyze a Gas turbine engine at a design speed under the following data employing a  separate power turbine, heat exchanger, reheater and intercooler between two-stage  compression.  Efficiency of compression in each stage: 85%  Isentropic efficiency of compressor turbine: 90%  Isentropic efficiency of power turbine: 85%  Transmission efficiency: 98%  Pressure ratio in each stage of compression: 2:1  Pressure loss in intercooler: 0.07 bar  Temperature after intercooling: 300 K  Thermal ratio of heat exchanger: 0.75  Pressure loss in combustion chamber: 0.15bar  Combustion efficiency of reheater: 98%  Maximum cycle temperature: 1000 K  Temperature after reheating: 1000 K  Air mass flow: 25 kg/s  Ambient air temperature: 15 °C  Ambient air pressure: 1 barTake the calorific value of fuel as 42 MJ/kg and pressure loss in each side of heat  exchanger as 0.1 bar. Find the net power output overall thermal efficiency, specific  fuel consumption. Neglect the kinetic energy of the gases leaving the system

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