Aerospace Engineering > GATE 2017 > Propulsion
For a turbine stage, which one of the following losses occurs due to the turning of the wall boundary layer through an angle due to curved surface?
A
Profile loss
B
Annulus loss
C
Tip clearance loss
D
Secondary flow loss

Correct : d

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Related Topics

turbine stage losses profile loss GATE Aerospace Engineering 2017 aerospace engineering gate annulus loss secondary flow loss curved surface boundary layer GATE 2017 Q18

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