Q. In case of gas turbines and compressors, degree of reaction is (Solved)
1. Static pressure drop in rotor/ static pressure drop in stage
2. Static pressure drop in stage/ static pressure drop in rotor
3. Isentropic enthalpy drop in rotor/ isentropic enthalpy drop in stage
4. Static temperature drop in stage/ static temperature drop in rotor
- c. Isentropic enthalpy drop in rotor/ isentropic enthalpy drop in stage