An Open-Cycle gas turbine installation consists of two isentropic compressor stages with intercooling and two isentropic turbine stages with reheating. The ambient air at 100 kPa and 300 K is drawn into the first compressor stage and compressed to the intercooler pressure of 380 kPa. The air is cooled back to 300 K in the intercooler and is compressed to 1000 kPa in the second compressor stage. The compressed air is then heated to 1400 K in the combustion chamber and sent to the first turbine stage. The air leaves the first turbine stage at 380 kPa and enters the reheater, where the air is reheated back to 1400 K before entering the second turbine stage. The air is finally exhausted at 100 kPa by the second turbine stage to the ambient. It is given that the air behaves as an ideal gas with Ca = 1.005 kJ/kg.K and c = 0.72 kJ/kg.K.

An Open-Cycle gas turbine installation consists of two isentropic compressor stages with intercooling and two isentropic turbine stages with reheating. The ambient air at 100 kPa and 300 K is drawn into the first compressor stage and compressed to the intercooler pressure of 380 kPa. The air is cooled back to 300 K in the intercooler and is compressed to 1000 kPa in the second compressor stage. The compressed air is then heated to 1400 K in the combustion chamber and sent to the first turbine stage. The air leaves the first turbine stage at 380 kPa and enters the reheater, where the air is reheated back to 1400 K before entering the second turbine stage. The air is finally exhausted at 100 kPa by the second turbine stage to the ambient. It is given that the air behaves as an ideal gas with Ca = 1.005 kJ/kg.K and c = 0.72 kJ/kg.K.

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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Answer the question.
Temperature after the heat addition process = K Thermal efficiency =% Mean effective pressure = kpa