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in an air-standard gas turbine cycle the air enters the compressor at 0.12 mpa at 25 c and leaving at a pressure 1.0 mpa. the maximum temperature is 1200 c. assume a compressor efficiency of 90%, a turbine
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in an air-standard gas turbine cycle the air enters the compressor at 0.12 mpa at 25 c and leaving at a pressure 1.0 mpa. the maximum temperature is 1200 c. assume a compressor efficiency of 90%, a turbine efficiency of 92%, and a regenerator effectiveness of 85%. (a) determine the compressor work, turbine work, heat addition in combustion chamber, and cycle efficiency. if net power output is 5mw, what are the ratings (total energy transfer) of each of components. (b) what is the exergy of the exhaust at the outlet of the regenerator?

User Khushneet
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Answer:

can be found in the service manual for the specific vehicle being serviced.

User Cbr
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