Compressors, Gas Turbines and Jet Engines
Inter-cooling in gas turbine results in

Decrease in both thermal efficiency and net output
Increase in thermal efficiency but decrease in net output
Increase in both thermal efficiency and net output
Increase in net output but decrease in thermal efficiency

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Compressors, Gas Turbines and Jet Engines
For minimum work in multistage compression, assuming same index of compression in all stages

Work done in subsequent stages should decrease
Work done in subsequent stages should increase
Work done in all stages should be equal
Work done in first stage should be more

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