Aerospace Engineering > GATE 2017 > Fluid Mechanics
Which one of the following statements is NOT true
A
Compared to a laminar boundary layer, a turbulent boundary layer is more desirable on a wing operating at large angle of attack
B
The skin friction drag for a turbulent boundary layer is larger than that for a laminar boundary layer
C
The location of transition from laminar to turbulent boundary layer depends only on the operating Reynolds number
D
A separated flow does not necessarily lead to a turbulent boundary layer

Correct : c

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Related Topics

boundary layer transition turbulent boundary layer laminar boundary layer skin friction drag separated flow GATE aerospace engineering 2017 Reynolds number boundary layer separation

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