Compressors, Gas Turbines and Jet Engines
The pressure and temperature conditions of air at the suction of compressor are

Slightly more than atmospheric
Slightly less than atmospheric
Atmospheric
Pressure slightly less than atmospheric and temperature slightly more than atmospheric

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Compressors, Gas Turbines and Jet Engines
The degree of reaction in an axial flow compressor is defined as the ratio of static enthalpy rise in the

Rotor to static enthalpy rise in the stator
Rotor to static enthalpy rise in the stage
Stator to static enthalpy rise in the rotor
Stator to static enthalpy rise in the stage

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