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

Similar Questions

If → denotes increasing order of intensity, then the meaning of the words dry → arid → parched is analogous to diet → fast → ______. Which one of the given opt...
#10 MCQ
If two positive non-zero real variables x and y are such that (x+y) is proportional to x/y, then x+y:
#11 MCQ
Consider the following sample of numbers: 9, 18, 11, 14, 15, 17, 10, 69, 11, 13. The median of the sample is
#12 MCQ

Related Topics

No tags found

Unique Visitor Count

Total Unique Visitors

Loading......

Question Options

Contributed by: