Compressors, Gas Turbines and Jet Engines
Gas turbine cycle with regenerator

Allows high compression ratio
Increases thermal efficiency
Decreases heat loss is exhaust
Allows operation at very high altitudes

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Compressors, Gas Turbines and Jet Engines
The overall isothermal efficiency of compressor is defined as the ratio of

Power to drive compressor to isothermal h.p.
Work to compress air isothermally to work for actual compression
Isothermal h.p. to adiabatic h.p.
Isothermal h.p. to the BHP of motor

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