Compressors, Gas Turbines and Jet Engines
The degree of reaction of an axial flow turbine is the ratio of isentropic temperature drop in a blade row to the

Total adiabatic temperature drop
Total temperature drop in the stage
Adiabatic temperature drop in the stage
Total temperature drop

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Compressors, Gas Turbines and Jet Engines
Intercooling in gas turbines

Decreases net output and thermal efficiency both
Decreases net output but increases thermal efficiency
Increases net output and thermal efficiency both
Increases net output but decreases thermal efficiency

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