Question 49

AENAT2 marksNeeds review
The figure shows the T-S diagram for an axial turbine stage.
Diagram for Aerospace Engineering question 49

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).

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2020AE

GATE AE 2020 · Paper 1

Aerospace Engineering · Original paper archive

Section
Aerospace Engineering
Question type
Numerical answer (NAT)
Marks
2 marks

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