50% Reaction Axial Flow Compressor (Symmetrical Blading) - GATE 2023 Aerospace Engineering Q21

Aerospace Engineering > GATE 2023 > Axial Compressors

For a stage of a 50% reaction ideal axial flow compressor (symmetrical blading), select the correct statement from the options given.

The stagnation enthalpy rise across the rotor is 50% of the rise across the stage.

The static enthalpy rise across the rotor is 50% of the rise across the stage.

Axial velocity component of the flow at the rotor exit is 50% of that at the rotor entry.

The static pressure rise across the rotor is 50% of the rise across the stator.

Correct : a

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