Mechanics of Fluids Mid - II, November - 2014
1.The boundary layer separation exists on the surface when
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du/dy = 0 and dp/du = 0
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du/dy = 0 and dp/dx > 0
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du/dy = 0 and dp/dx < 0
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None
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Answer: B
2.The drag provided by end effect due to finite length of an aerofoil is
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Form drag
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Profile drag
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Induced drag
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Boundary drag
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Answer: C
3.The head loss in a sudden expansion from 6 cm diameter pipe to 12 cm diameter pipe in terms of velocity V1 is the smaller diameter pipe is
Answer: D
4.The Prandtl mixing length is
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Independent of shear stress
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zero at the pipe wall
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Independent of distance from the fixed surface
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Constant for all fluids
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Answer: B
5.Which of the following bend will cause maximum head loss
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300 bend
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600 bend
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900 bend
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U bend
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Answer: C
6.Co-efficient of velocity contraction and discharge arranged in increasing order of
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Cv Cc Cd
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Cd Cc Cv
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Cv Cd Cc
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Cc Cd Cv
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Answer: B
7.Ratio of inertia force to viscous force is known as
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Renold’s number
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Froude number
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Mach number
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Euler number
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Answer: A
8.Model analysis of a pipe flow is based on
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Renold’s number
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Froude number
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Mach number
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Euler number
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Answer: A
9.Buckingham theorem stipulate that the number of dimensional groups
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n-m
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m-n
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n+m
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n/m
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Answer: A
10.The loss of head due to sudden contraction of a pipe
Answer: A
11.The co-efficient of drag for turbulent flow over the cylinder is _______ than that for laminar flow because separation is delayed.
Answer: Less
12.Flow around sphere at very low Reynold’s number is governed by the _________________
Answer: Stoke’s law
13.Momentum transfer is on molecular level in flow.
Answer: Laminar
14.The velocity distribution in turbulent flow is given approximately by Prandtl’s _______________
Answer: One seventh power law
15.If the Reynold’s number is used for model and prototype using the same liquid then the discharge ratio is __________
Answer: 1
16.Froude number is used in the study of ________________ flow
Answer: Fee surface
17.Boundary layer thickness ___________________ along with the flow direction.
Answer: Increases
18.At the separation point of boundary layer the velocity gradient will be __________________
Answer: Zero
19.Flow in a pipe is laminar when Reynold’s number is __________________
Answer: Less than 2000
20.Frictional resistance of a pipe varies approximately with the ___________________ of the liquid
Answer: Square of velocity