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Reg. No.
Question Paper Code : 31560
B.E./B.Tech. DEGREE EXAMINATION, NOVEMBER/DECEMBER 2013-
Third Semester
Mechanical Engineering
ME zzo4rcu 3213rA{E 34tCE t20BnO122 ME 305/080180007/IE 41 - FLUID
MECHANICS AND MACHINERY
(Common to Aeronautical Engineering, Automobile Engineering, Production
Engineering,. Mechatronics Engineering, Mechanical and Automation Engineering
and Fourth Semester Manufacturing Engineering; Industrial Engineering and
Industrial Engineering uld Management)
(Regulation 2008/20 10)
(Common to PTCtr 3213 - Fluid Mechanics and Machinery for B.E. (Part-Time)
Third Semester - Manufacturing Engineering Regulation 2009)
Time: Three hours Maximum : 100 marks
y missin! data can be suitably assumed with justification.
Answer ALL questions.
PART A
-
(10 x 2 -- 20 marks)
1. What is cavitation? What causes it?
2. Differentiate between kinematic viscosity of liquids and gases with respect to
pressure.
3. How does surface roughness affect the pressure drop in a pipe if the flow is
turbulent?
4. A piping system involves two pipes of different diameters (but of identical
length, material, and roughness) connected in parallel. How would you
compare the flow rates and pressure drops in these two pipes?
5. The excess pressure Ap inside a bubble is known to be a function of the
surface tension and the radius. By dimensional reasoning determine how the
excess pressure will vary if we double the surface tension and the radius.
6. Determine the d.ynamic pressure exerted by a flowing fncompressible fluid on
an immersed object, assuming the pressure is a function of the density and the
velocity.
2 I I 1 t 2 I t, o q 5
7.
8.
9.
What is meant by hydraulic efficiency of turbine?
Define - r.nanometric head:and, write its mathematical equation-
Draw the relationship between discharge and crank angle for a single acting
pump:
Mention the significance of 'back leakage'.10.
11. (a) (r)
PARTB-(5x 16=80marks)
Water enters the bottom of the cone in Fig. 1. at a uniformly
increasing average velocity v = Lt . It d is very small, derive an
analytic formula for the water surface rise h(t), assuming h = 0 at
t =0. (8)
Fig. 1
(D According to Torricelli's theorem, the velocity of a fluid draining
from a hole in a tank is V
=
(2gh)''', where h is the depth of water
above the hole. Let'the hole haye ,r"u A. and the cylindrical tank
have bottom area Au. Derive a formula for the time to drain the
I
I
I
I
tank from an initial depth h".
Or
A simple turbomachine is constructed from a disk with two internal
ducts which exit tangentially through square holes, as in the Fig. 2.
water at 20"c enters the disk at the center, as shown. The disk
must drivb, at 250 rev/min, a smaLl device whose retarding torque is
1.5 Nm. What is the proper mass flow of water, in kg/s?
2cm
(B)
1l*r-[-]*:2 cm
-t{
Fig.2.
2
(8)
(1)(b)
I
32 ct
I
cm
Itjt,
O,,
tlt!7
31560
t
(ii) A two-dimensional sheet of water, 10 cm thick and moving at'7 mls,
strikes a fixed wall inclined at 20' with respect to the jet direction.
Assuming frictionless flow, find the normal force on the wall per
. meter of depth, and the widths of the sheet deflected upstream and
downstream along the wall. (8)
t2. (a) (1) Consider turbulent flow (f = 0.184 Re{ 2) of a fluid through a square
' channel with smooth surfaces. Now the mean velocity of the fluid is
doubled. Determine the change in the head loss of the fluid. Assume
the flow regime remains unchanged. What will be the head loss for
fully turbulent flow in a rough pipe?
(1i) Discuss on vari.ous minor losses in pipe flow.
Or
(b) (I) Two tanks of fluid (p = 998 kg/m3 and p= 0.001 kg/ms.) at 20oC
are connected by a capillary tube 4 mm in diameter and 3'5 m long.
The surface of tank 1 is 30 cm higher than the surface of tank 2.
Estimate the flow rate in m3/h. Is the flow Laminar? For what tube
diameter will Reynolds number be 500? (10)
(i1) Explain the concept of boundary layer in pipes for both laminar and
turbulent flows with neat sketches. (6)
13. (a) (r) Derive an expression for the shear stress at the pipe waII when an
incompressible fluid flows through a pipe under pressure. IJse
dimensional analysis with the following significant parameters:
pipe diameter D, flow velocity V, and viscosity p and density p of
the fluid.. (10)
(u) Use dimensional analysis and the MLT system to arrange the
following into a dimensionless number: L, p, p and o - (6)
Or
G) (, Consider viscous flow ever a very small object. Analysis of the
' equations of motion shows that the inertial terms are much smaller
than viscous and pressure terms. Fluid density drops out, and these
are called. creeping flows. The only irnportant parameters are
velocity IJ, viscosityp, and body length scale d. For three-
dimensional bodies, like spheres, creeping flow analysis yields very
good results. It is uncertain, however, if creeping flow applies to
two-dimensional bodies, such as cylinders, since even though the
diameter may be very small, the length of the cylinder is infinite.
Let us see if d.imensional analysis can help. (1) Apply the Pi
theorem to two-d.imensional drag force Fr-oas a function of the
other parameters. Be careful: two-dimensional drag has dimensions
of force per unit length, not simply force, (2) Is your atalysis in part
(1) physicaily plausible? If not, explain why not. (3) It turns out that
fluid density p cannot be negldcted in analysis of creeping flow
over two dimensional bodies. Repeat the dimensional analysis, this
time including p as a variable, and find the resulting non-
dimensional relation between the parameters in this problem. (10)
(10)
(6)
31560
14. (a)
a
(i0 When fluid in a pipe is accelerated. linearly from rest, it begins as
laminar flow and then undergoes transition to turbulence at a time
f,, which depends upon the pipe diameter D, flui.d acceleration a,
density p and viscosityp. Arrange this into a dimensionless
relation between fr. and D. (6)
(r) A Kaplan turbine delivers 10 MW under a head of 25 m. The hub
and tip diameters are 1.2 m and 3 m. Hydraulic and overall
efficiencies are 0.90 and 0.85. If both velocity triangles are right
angled triangles, determine the speed, guide blade outlet angle and
(10)blade outlet angle.
(ir) Discuss - characteristics of centrifugal pump at constant speed. (6)
Or
(1) A centrifugal pump with an impeller diameter of 0.4 m runs at
1450 rpm. The angle at outlet of the backward curved vane is 25o
with tangent. The flow velocity remains constant at 3 m/s. If the
manometric efficiency is 84% determine the fraction of the kinetic
energ:y at outlet recovered as static head. (10;
characteristics of hydraulic turbines
&)
(i, Explain the load efficiency
with a diagram.
15. (a) Discuss on the following: Working of double acting
diagram, acceleration head, friction head.
. (6)
pump, inficator
(16)
Or
(b) With neat sketches, discuss about the rotary positive displacement pump-'
(16)
31560

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Fluid Mechanics & Machinery QP NOV-2013

  • 1. Reg. No. Question Paper Code : 31560 B.E./B.Tech. DEGREE EXAMINATION, NOVEMBER/DECEMBER 2013- Third Semester Mechanical Engineering ME zzo4rcu 3213rA{E 34tCE t20BnO122 ME 305/080180007/IE 41 - FLUID MECHANICS AND MACHINERY (Common to Aeronautical Engineering, Automobile Engineering, Production Engineering,. Mechatronics Engineering, Mechanical and Automation Engineering and Fourth Semester Manufacturing Engineering; Industrial Engineering and Industrial Engineering uld Management) (Regulation 2008/20 10) (Common to PTCtr 3213 - Fluid Mechanics and Machinery for B.E. (Part-Time) Third Semester - Manufacturing Engineering Regulation 2009) Time: Three hours Maximum : 100 marks y missin! data can be suitably assumed with justification. Answer ALL questions. PART A - (10 x 2 -- 20 marks) 1. What is cavitation? What causes it? 2. Differentiate between kinematic viscosity of liquids and gases with respect to pressure. 3. How does surface roughness affect the pressure drop in a pipe if the flow is turbulent? 4. A piping system involves two pipes of different diameters (but of identical length, material, and roughness) connected in parallel. How would you compare the flow rates and pressure drops in these two pipes? 5. The excess pressure Ap inside a bubble is known to be a function of the surface tension and the radius. By dimensional reasoning determine how the excess pressure will vary if we double the surface tension and the radius. 6. Determine the d.ynamic pressure exerted by a flowing fncompressible fluid on an immersed object, assuming the pressure is a function of the density and the velocity. 2 I I 1 t 2 I t, o q 5
  • 2. 7. 8. 9. What is meant by hydraulic efficiency of turbine? Define - r.nanometric head:and, write its mathematical equation- Draw the relationship between discharge and crank angle for a single acting pump: Mention the significance of 'back leakage'.10. 11. (a) (r) PARTB-(5x 16=80marks) Water enters the bottom of the cone in Fig. 1. at a uniformly increasing average velocity v = Lt . It d is very small, derive an analytic formula for the water surface rise h(t), assuming h = 0 at t =0. (8) Fig. 1 (D According to Torricelli's theorem, the velocity of a fluid draining from a hole in a tank is V = (2gh)''', where h is the depth of water above the hole. Let'the hole haye ,r"u A. and the cylindrical tank have bottom area Au. Derive a formula for the time to drain the I I I I tank from an initial depth h". Or A simple turbomachine is constructed from a disk with two internal ducts which exit tangentially through square holes, as in the Fig. 2. water at 20"c enters the disk at the center, as shown. The disk must drivb, at 250 rev/min, a smaLl device whose retarding torque is 1.5 Nm. What is the proper mass flow of water, in kg/s? 2cm (B) 1l*r-[-]*:2 cm -t{ Fig.2. 2 (8) (1)(b) I 32 ct I cm Itjt, O,, tlt!7 31560
  • 3. t (ii) A two-dimensional sheet of water, 10 cm thick and moving at'7 mls, strikes a fixed wall inclined at 20' with respect to the jet direction. Assuming frictionless flow, find the normal force on the wall per . meter of depth, and the widths of the sheet deflected upstream and downstream along the wall. (8) t2. (a) (1) Consider turbulent flow (f = 0.184 Re{ 2) of a fluid through a square ' channel with smooth surfaces. Now the mean velocity of the fluid is doubled. Determine the change in the head loss of the fluid. Assume the flow regime remains unchanged. What will be the head loss for fully turbulent flow in a rough pipe? (1i) Discuss on vari.ous minor losses in pipe flow. Or (b) (I) Two tanks of fluid (p = 998 kg/m3 and p= 0.001 kg/ms.) at 20oC are connected by a capillary tube 4 mm in diameter and 3'5 m long. The surface of tank 1 is 30 cm higher than the surface of tank 2. Estimate the flow rate in m3/h. Is the flow Laminar? For what tube diameter will Reynolds number be 500? (10) (i1) Explain the concept of boundary layer in pipes for both laminar and turbulent flows with neat sketches. (6) 13. (a) (r) Derive an expression for the shear stress at the pipe waII when an incompressible fluid flows through a pipe under pressure. IJse dimensional analysis with the following significant parameters: pipe diameter D, flow velocity V, and viscosity p and density p of the fluid.. (10) (u) Use dimensional analysis and the MLT system to arrange the following into a dimensionless number: L, p, p and o - (6) Or G) (, Consider viscous flow ever a very small object. Analysis of the ' equations of motion shows that the inertial terms are much smaller than viscous and pressure terms. Fluid density drops out, and these are called. creeping flows. The only irnportant parameters are velocity IJ, viscosityp, and body length scale d. For three- dimensional bodies, like spheres, creeping flow analysis yields very good results. It is uncertain, however, if creeping flow applies to two-dimensional bodies, such as cylinders, since even though the diameter may be very small, the length of the cylinder is infinite. Let us see if d.imensional analysis can help. (1) Apply the Pi theorem to two-d.imensional drag force Fr-oas a function of the other parameters. Be careful: two-dimensional drag has dimensions of force per unit length, not simply force, (2) Is your atalysis in part (1) physicaily plausible? If not, explain why not. (3) It turns out that fluid density p cannot be negldcted in analysis of creeping flow over two dimensional bodies. Repeat the dimensional analysis, this time including p as a variable, and find the resulting non- dimensional relation between the parameters in this problem. (10) (10) (6) 31560
  • 4. 14. (a) a (i0 When fluid in a pipe is accelerated. linearly from rest, it begins as laminar flow and then undergoes transition to turbulence at a time f,, which depends upon the pipe diameter D, flui.d acceleration a, density p and viscosityp. Arrange this into a dimensionless relation between fr. and D. (6) (r) A Kaplan turbine delivers 10 MW under a head of 25 m. The hub and tip diameters are 1.2 m and 3 m. Hydraulic and overall efficiencies are 0.90 and 0.85. If both velocity triangles are right angled triangles, determine the speed, guide blade outlet angle and (10)blade outlet angle. (ir) Discuss - characteristics of centrifugal pump at constant speed. (6) Or (1) A centrifugal pump with an impeller diameter of 0.4 m runs at 1450 rpm. The angle at outlet of the backward curved vane is 25o with tangent. The flow velocity remains constant at 3 m/s. If the manometric efficiency is 84% determine the fraction of the kinetic energ:y at outlet recovered as static head. (10; characteristics of hydraulic turbines &) (i, Explain the load efficiency with a diagram. 15. (a) Discuss on the following: Working of double acting diagram, acceleration head, friction head. . (6) pump, inficator (16) Or (b) With neat sketches, discuss about the rotary positive displacement pump-' (16) 31560