Compressors, Gas Turbines and Jet Engines
Inter-cooling in multistage compressors is done

To enable compression in two stages
To cool the air at delivery
To minimize the work of compression
To cool the air during compression

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Compressors, Gas Turbines and Jet Engines
The following is true for an open cycle gas turbine having exhaust heat exchanger. Atmospheric air before entering the compressor is

Bled gas from turbine is heated and readmitted for complete expansion
Compressed air before entering the combustion chamber is heated
Exhaust gases drive the compressor
Heated

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