Aerospace Engineering > GATE 2024 > Turbines
Which of the following statements is/are TRUE for an axial turbine?
A
For a fixed rotational speed, the mass flow rate increases with an increase in the flow coefficient
B
The absolute stagnation enthalpy of the flow decreases across the nozzle row
C
The relative stagnation enthalpy remains unchanged through the rotor
D
For a fixed rotational speed, the mass flow rate remains unchanged with a change in the flow coefficient

Correct : a

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Related Topics

axial turbine aerospace engineering GATE GATE AE 2024 Q48 flow coefficient turbine mass flow rate axial turbine stagnation enthalpy turbine turbine nozzle rotor

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