Compressors Gas Dynamics and Gas Turbines - Engineering

Q1:

The degree of reaction in an axial flow compressor is defined as the ratio of static enthalpy rise in the

A rotor to static enthalpy rise in the stator

B stator to static enthalpy rise in the rotor

C rotor to static enthalpy rise in the stage

D stator to static enthalpy rise in the stage

ANS:C - rotor to static enthalpy rise in the stage

Explanation: No answer description is available.