2. What is the difference between an ideal and a real fluid?

3. Distinguish between path lines, stream lines and streak lines.

4. To what type of flow is the concept of velocity potential and stream function

applicable?

5. What are the assumptions made in the derivation of Euler's equation?

6. Sketch the velocity and shear stress distribution for laminar flow of an

incompressible fluid through a circular pipe.

7. Give four examples in every day life where formation of boundary layer is

important.

8. What are the characteristics of laminar flow?

9. What are the applications of model testing?

10. Enumerate the applications of dimensional homogeneity.

certain point the gauge pressure is 0.31 atmosphere. At what height

above the given point is the liquid level? (8)

(ii) Define Viscosity. Explain the effect of temperature and pressure on

viscosity of liquids and gases. (8)

Or

(b) (i) Explain the characteristics of non- Newtonian fluids in detail. (8)

(ii) The velocity distribution for flow over a plate is given by

2

u =2y − y

where u is the velocity in m/s at a distance y meters above the

plate. Determine the velocity gradient and shear stress at the

boundary and 0.15 m from it. (8)

12. (a) Derive an expression for the depth of centre of pressure from free surface

of liquid of an inclined plane surface submerged in the liquid. (16)

Or

(b) (i) Derive the differential equation of continuity. (8)

(ii) In a two dimensional incompressible flow, the fluid velocity

components are given by u = x −4y and v = −y −4x . Show that

velocity potential exists and determine its form as well as stream

function. (8)

13. (a) A drainage pump has tapered suction pipe. The pipe is running full of

water. The pipe diameter at the inlet and at the upper end is 1 m and

0.5 m respectively. The free water surface is 2 m above the centre of the

inlet and centre of upper end is 3 m above the top of free water surface.

The pressure at the top end of the pipe is 25 cm of Hg and it is known

that loss of head by friction between top and bottom section is one tenth

of the velocity head at the top section. Compute the discharge in litre/sec.

Neglect loss of head at the entrance of the tapered pipe. (16)

Or

(b) Show that the momentum correction factor and kinetic energy correction

factor for laminar flow through a circular pipe are 4/3 and 2 respectively.

(16)

14. (a) Explain what you understand by boundary layer thickness and

displacement thickness. Determine the relationship between the two for

a boundary layer which is

(i) laminar throughout and

(ii) turbulent throughout.

Assume :

(1) in the laminar boundary layer, the flow obeys the law, shear

stress

dy

du

τ = where is the viscosity, which leads to

velocity profile

2

(U −u) = k(δ − y) where U is the free stream

velocity, u is the velocity at a distance y above the plate and

k is a constant.

(2) the velocity distribution in the turbulent boundary layer is

given by

. (16)

Or

(b) Derive an expression for the calculation of loss of head due to

(i) sudden enlargement

(ii) sudden contraction. (16)

15. (a) Describe Buckingham’s π – theorem to formulate a dimensionally

homogeneous equation between the various physical quantities effecting

a certain phenomenon. (16)

Or

(b) By dimensional analysis, show that the power P developed by a hydraulic

turbine is given by

=

gH

N D

P N D f

2 2

3 5

ρ where ρ – mass density of

liquid, N – rotational speed, D – diameter of runner, H – working head

and g – acceleration due to gravity. (16)

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