Compare the thermal efficiency of a two-stage gas turbine with regeneration, reheating and intercooling to that of
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All components operate ideally
Air enters the first compressor at 100 kPa and 208C
The total pressure ratio across all stages of compression is 16, and
The maximum cycle temperature is 8008C.
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Related Book For 
Thermodynamics An Engineering Approach
ISBN: 978-0073398174
8th edition
Authors: Yunus A. Cengel, Michael A. Boles
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