Aerospace Engineering > GATE 2020 > Turbomachinery
The figure shows the T-S diagram for an axial turbine stage.
Assuming specific heat ratio of 1.33 for the hot gas, the isentropic efficiency of the turbine stage is _______ % (round off to two decimal places).

(Image of a T-S diagram is given)

Correct : 87 to 89

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Related Topics

T-S diagram turbine stage isentropic efficiency turbine specific heat ratio 1.33 aerospace engineering gate 2020 turbine stage efficiency calculation T-S diagram GATE aerospace engineering 2020 isentropic efficiency problems

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