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

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

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Compressors, Gas Turbines and Jet Engines
The assumption made in two stage compression with inter-cooler is that

The compression in both the cylinders is polytropic
There is no pressure drop in the inter-cooler
All of the listed here
The suction and delivery of air takes place at constant pressure

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