Q.

In case of gas turbines and compressors, degree of reaction is                

A. Static pressure drop in rotor/ static pressure drop in stage
B. Static pressure drop in stage/ static pressure drop in rotor
C. Isentropic enthalpy drop in rotor/ isentropic enthalpy drop in stage
D. Static temperature drop in stage/ static temperature drop in rotor
Answer» C. Isentropic enthalpy drop in rotor/ isentropic enthalpy drop in stage
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