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mechanical engineering compressors gas dynamics and gas turbines
1. 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 stage
(B): rotor to static enthalpy rise in the stator
(C): stator to static enthalpy rise in the rotor
(D): stator to static enthalpy rise in the stage
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