engineering mechanics · 2018-07-06 · block, screw jack, calculation of mechanical advantage,...
TRANSCRIPT
FY CIVIL Second Sem
Sanjay Ghodawat Polytechnic, Atigre 1
ENGINEERING MECHANICS
1. SIMPLE MACHINES 20 Marks
Specific Objectives:
Calculate velocity ratio for given machine.
Find Efficiency of given machine.
Contents:
1.1 Definitions: …………………………………………..... (06 Marks)
Simple machine, compound machine , load , effort , mechanical advantage , velocity
ratio , input of a machine ,output of a machine efficiency of a machine , ideal
machine, ideal effort and ideal load, load lost in friction, effort lost in friction.
1.2 Analysis: …………………………………………..... (04 Marks)
Law of machine, maximum mechanical advantage and maximum efficiency of a
machine, reversibility of a machine, condition for reversibility of a machine, self locking
machine. Simple numerical problems.
1.3 Velocity Ratio for Simple Machines: …………….... (10 Marks)
Simple axle and wheel, differential axle and wheel, Weston‟s differential pulley block,
single purchase crab, double purchase crab, worm and worm wheel, geared pulley
block, screw jack, calculation of mechanical advantage, efficiency, identification of
type such as reversible or not etc.
Man invented various types of machines for his easy work.
Sometimes, one person cannot do heavy work, but with the help of
machine, the same work can be easily done.
To change the tyre of a car, number of person will be required. But
with the help of a “Jack”, the same work can be done by a single man.
Therefore, jack acts as a machine by which the load of a car can be
lifted by applying very small force as compared to the load of car.
Simple Machine or Lifting Machine:
A machine a device by which heavy load can be lifted by
applying less effort as compared to the load.
e.g. Heavy load of car can be lifted with the help of simple screw
jack by applying small force.
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Compound Machine:
Compound machine is a device which may consists of number of
simple machines. A compound machine may also be defined as a
machine which has multiple mechanisms for the same purpose.
Compound machines do heavy work with less efforts and greater
speed.
e.g. In a crane, one mechanism (gears) are used to drive the rope
drum and other mechanism (pulleys) are used to lift the load. Thus, a
crane consists of two simple machines or mechanisms i.e. gears and
pulleys. Hence, it is a compound machine.
Effort:
It may be defined as, the force which is applied so as to
overcome the resistance or to lift the load.
It is denoted by „P‟.
Magnitude of effort (P) is small as compared to the load (W).
Load:
The weight to be lifted or the resistive force to be overcome with the
help of a machine is called as load (W).
Velocity Ratio (V.R.):
It is defined as the ration of distance traveled by the effort (P) to
the distance traveled by the load (W)
loadby travelledDistance
effortby travelledDistance V.R.
Velocity ratio will be always more than one and for a given
machine, it remains constant.
Mechanical Advantage:
It is defined as the ratio of load to be lifted to the effort applied.
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P
W
(P)Effort
(W) Load M.A.
Input:
The amount of work done by the effort is called as input and is
equal to the product of effort and distance travelled by it.
Input = P x X, where, P – Effort and X – distance
travelled by the effort
Output:
The amount of work done by the load is called as output and is
equal to the product of load and distance travelled by it.
Output = W x Y where, W – Load and Y – distance
travelled by the load
Efficiency:
The ratio of output to input is called as efficiency of machine and
it is denoted by Greek letter eta (η)
Generally, efficiency is expressed in percentage
% 100xInput
Outputη
It is always less than 100 because of friction, therefore output <
input.
But Output = W.Y and Input = P.X
% 100xXxP
YxW100x
Input
Outputη
% )Y
XV.R.and
P
WM.A.(Since100x
V.R.
M.A.100x
Y
XP
W
η
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Therefore, efficiency of a machine is also defined as the ratio of
mechanical advantage (M.A.) to the velocity ratio (V.R.). It is also
expressed in percentage.
% 100xV.R.
M.A.η
It is always less than 100 because of friction, therefore M.A. < V.R.
Actual Machine:
The machine whose efficiency is always less than 100 % due to
frictional resistance offered by the different moving component parts of
the machine is called as actual machine.
For such machines, η < 100 % and hence M.A. < V.R.
Ideal Machine:
The machine whose efficiency is 100 % and in which friction is
totally absent or zero, is called as ideal machine.
For ideal machines, η = 100 % and hence M.A. = V.R.
Ideal Effort (Pi):
The effort which is required to lift the load when there is no friction
is called as an ideal effort (Pi)
Ideal Effort Pi = V.R.
W
Where, Pi = Ideal Effort, W = Load to be lifted, V.R. = Velocity Ratio
Ideal Load (Wi):
The load which can be lifted by an effort (P), when there is no
friction, is called as an ideal load (Wi)
Ideal Load Wi = P x V.R.
Where, P = Effort applied, Wi = Ideal Load, V.R. = Velocity Ratio
Lever Arm:
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A rigid bar which is provided in machines so as to apply the effort
(P) is called as lever arm or handle.
LAW OF MACHINE:
The equation which gives the relation between load lifted and
load applied in the form of a slope and intercept of a straight line is
called as Law of a machine i.e. P = mW + C
Where, P = effort applied, W = load lifted, m = slope of the line and
C = y – intercept of the straight line.
To draw the graph of Load (W) V/s Effort (P), effort is applied on a
machine and the corresponding values of the loads are noted down.
The graph of Load (W) V/s Effort (P) is drawn by taking load (W) on the x-
axis and the effort (P) on the y-axis as shown in the figure.
12
12
XX
YYθtanm
It has been observed that,
the graph of load v/s effort is a
straight line cuts the Y-axis giving
the intercept „C‟ which indicates
the effort lost on friction, when no
load is applied.
Is must be noted that, if the
machine is an ideal machine, the
straight line of the graph will pass
through the origin.
Comparing to the equation of straight line i.e. y = mX + C, we get
P = mW + C
Where, P =Effort applied, W = Load applied, m = slope of the line
and C = Y-intercept of the line.
Effort
(P)
Load (W)
C
P = mw + C
(X2, Y2)
(X1, Y1)
O
O
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Note:
If we know the law of machine i.e. values of „m‟ and „C‟ are
known, then for a given load effort can be found out or for a given effort
corresponding value of the given load can be found out. The law of
machine also indicates the friction in the machine and maximum M.A.
Maximum Mechanical Advantage (Max. M.A.):
We know that,
m
1M.A.Max.
maximumbewillM.A.,W
CratiotheNeglecting
smallverybewillW
Cratiothemore,isW''ifequationabovetheIn
W
Cm
1M.A.
getweW''byrDenominato&numeratortheDividing
CmW
WM.A.
CmWPBut,
P
WM.A.
Maximum Efficiency:
The ratio of maximum M.A. to the V.R. is called as maximum
efficiency.
It is also expressed in percentage as
)m
1M.A.MaxSince(100x
V.R.
1x
m
1100x
V.R.
M.A.MaxηMaximum%
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Reversible Machine:
When a machine is capable of doing some work in the reverse
direction even on removal of effort, it is called as reversible machine.
Condition for Reversible Machine:
The efficiency of the machine should be more than 50%.
Irreversible Machine / Non-reversible Machine / Self Locking Machine:
When a machine is not capable of doing some work in the reverse
direction even on removal of effort, it is called as irreversible machine or
non-reversible machine or self locking machine.
Condition for Irreversible Machine:
The efficiency of the machine should be less than 50%.
Friction in Machines in terms of Effort and Load:
In any machine, there are number of parts which are in contact
with each other in their relative motion. Hence, there is always a
frictional resistance and due to which the machine is unable to produce
100 % efficiency.
Let, P = Actual Effort, Pf = Effort Lost in friction, Pi = Ideal Effort
Effort Lost in friction (Pf) = Actual Effort (P) – Ideal Effort (Pi)
)V.R.
WP(Since
V.R.
WPPPP iif
Let, W = Actual load lifted, Wf = Load Lost in friction, Wi = Ideal
Load
Load Lost in friction (Wf) = Ideal Load (Wi) – Actual load lifted
(W)
V.R.)xPW(SinceWV.R.)x(PWWW iif
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GRAPHS:
1. Load v/s Effort:
The graph of load against
effort is a straight line, cuts the y-axis
giving the intercept „C‟ which
represents the effort lost in friction at
zero load.
12
12
XX
YYθtanm
2. Load v/s Percentage Efficiency (%η):
The graph of load v/s % efficiency is
a curve as shown in the above figure. As
load increases, percentage efficiency
also increases and therefore gives rise to a
smooth curve gradually increasing and
becomes more or less parallel to x-axis.
3. Load v/s Mechanical Advantage:
The graph of load v/s Mechanical
Advantage is a curve as shown in the
above figure. As load increases,
mechanical advantage also increases
and therefore gives rise to a smooth
gradually increasing curve.
Effort
(P)
Load (W)
C
P = mw + C
(X2, Y2)
(X1, Y1)
O
O
X
Y
O
Load (W)
% n
X
Y
O
Load (W)
M.A.
Max. M.A. = 1/m
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4. Load v/s Ideal Effort (Pi):
The graph of load v/s ideal effort is a straight line passing through
origin as shown in the above figure.
5. Load v/s Effort lost in friction (Pf):
The graph of load against effort lost in friction is a straight line as
shown in the figure.
X
Y
O
Load (W)
Ideal
Effort
(Pi)
Effort
lost in
friction
(Pf)
Load (W)
O
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STUDY OF SOME SIMPLE MACHNES:
We know that, velocity ratio of a machine is the ratio of distance
travelled by the effort to the distance travelled by the load. It is
observed that, the distance travelled by the effort is greater than the
distance moved by the load. Experimentally, it has been found that, the
velocity ratio remains constant for all loads. The velocity ratio changes
from machine to machine but remains constant for a given machine.
1. Simple Wheel and Axle:
In simple wheel and axle, effort wheel and axle are rigidly
connected to each other and mounted on a shaft. A string is wound
round the axle so as to lift the load (W) another string is wound round the
effort wheel in opposite direction so as to apply the effort (P) as shown in
the figure.
Let, W = Load lifted, P = Effort Applied D = Diameter of the
effort wheel d = diameter of the load axle.
When, the
effort wheel
completes
one revolution,
the effort
moves through
a distance
equal to the
circumference
of the effort
wheel (πD)
and simultaneously the load moves up through a distance equal to the
circumference of the load axle (πd)
d
D
dπ
Dπ
LoadthebytravelledDistance
EffortthebytravelledDistanceV.R.
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2. Differential Axle and
Wheel:
Differential axle and
wheel is a further
modification and
improvement over the
simple axle and wheel.
It consists of a load
axle made up of bigger
axle of diameter d1 and
smaller axle of diameter
d2 rigidly connected to each other and an effort wheel of diameter „D‟.
Since, the load axle is made up of two axles of different diameters; it is
called as a differential axle. Differential axle and effort wheel are
mounted on the same shaft which is supported on ball bearings as
shown in the figure.
A string is wound round the effort wheel so as to apply the
effort „P‟. Another string is wound round the bigger axle further passing
over the pulley carrying the load „W‟ attached to the snatch block. The
same string is further wound round the smaller axle in the opposite
direction to that of bigger axle. The winding of string on effort wheel and
smaller axle is done in the same direction; the string unwinds from the
effort wheel & smaller axle and winds over the bigger axle
simultaneously, when the effort „P‟ is applied.
When effort wheel complete one revolution, the differential axle
also completes one revolution.
Distance travelled by the effort = πD
Length of the string wound over the bigger axle = πd1
Length of the string unwound over the smaller axle = πd2
Total winding over the bigger axle = πd1 - πd2 = π(d1 – d2)
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But, the load „W‟ is lifted through half of the total winding because
snatch block with a movable pulley supports the load „W‟
)dd(2
π)dd(π
2
1winding)total(
2
1loadthebytravelledDistance 2121
We know that,
21
21
dd
D2
)dd(2
π
Dπ
loadthebytravelledDistance
effortthebytravelledDistanceV.R.
Where, D = Diameter of effort wheel, d1 = diameter of bigger axle,
d2 = diameter of smaller axle.
If radius of effort wheel, bigger axle and smaller axle are given
then,
21 RR
R2V.R.
Where, R = Diameter of effort wheel, R1 = diameter of bigger axle,
R2 = diameter of smaller axle.
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3. A Simple Screw Jack:
A screw jack is commonly used for lifting and supporting the
heavy load. A very small effort can be applied at the end of the lever or
handle or tommy bar for lifting the heavy loads. This effort is very small as
compared to the load to be lifted. As jack has a simple mechanism, it is
most commonly used in repair work of vehicles.
When the effort is applied to the handle or lever arm to complete
one revolution then load is lifted through one pitch of the screw (p),
therefore the distance moved by the load is equal to the pitch of the
screw and the distance moved by the effort is equal to 2πL
Let, L = length of the handle or lever arm and p = pitch of the thread or
screw, then
p
L2π
loadthebytravelledDistance
effortthebytravelledDistanceV.R.
If the effort wheel is used at the place of handle or lever arm for
applying the effort, then
p
Dπ
loadthebytravelledDistance
effortthebytravelledDistanceV.R.
Where, D = diameter of the effort wheel and p = pitch of thread or
screw.
4. Weston’s Differential Pulley Block:
It consists of upper and lower
block. Upper block is having bigger
pulley and smaller pulley of different
diameter mounted on same common
axle and that of lower block is having a
single pulley. The weight „W‟ is attached
to the lower block. Upper block is fixed
and lower block is movable.
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An endless chain passes over the bigger and pulley and single
pulley in lower block as shown in the figure.
When there is one complete revolution of the bigger pulley,
distance moved by the effort is equal to the circumference of the
bigger pulley (πD). When the bigger pulley completes one revolution,
the smaller pulley also completes one revolution because both pulleys
are fixed on the same axle. Therefore, for one complete revolution, the
length of the chain wound round the bigger pulley is equal to the
circumference of the bigger pulley (πD) and at the same time, the
length of the chain unwound from the smaller pulley is equal to the
circumference of the smaller pulley (πd).
Net winding = πD – πd
As the load (W) attached to the lower block, is equally distributed
between the two parts of the chain, distance moved by load is equal to
the half of the net winding.
Distance moved by the load = ½ ( πD – πd )
dD
D2V.R.
d)πDπ(2
1
Dπ
loadthebytravelledDistance
effortthebytravelledDistanceV.R.
Where, D = diameter of bigger or upper pulley, d = diameter of
smaller or lower pulley
If radii of bigger and smaller pulley are given, then
rR
R2V.R.
Where, R = radius of bigger or upper pulley, r = radius of smaller or
lower pulley
If number of teeth or cogs of the bigger and smaller pulley are
given, then
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21
1
TT
T2V.R.
Where, T1 = number of teeth or cog on bigger or upper pulley, T2 =
number of teeth or cog on smaller or lower pulley
5. Worm and Worm
Wheel:
This machine is
made of toothed wheel
known as worm wheel
and a square threaded
screw known as worm.
Worm and worm wheel is
geared with each other.
The effort wheel is
attached to the worm. A
load drum is centrally
fixed to the worm wheel as shown in the figure. The effort can be either
by wheel or handle. The worm may be single threaded or multi-
threaded.
Let, w = load lifted, T = number of teeth on the worm wheel,
P = effort applied, r = radius of load drum, R = radius of effort
wheel.
Consider the worm is single threaded.
For one complete revolution of effort wheel, distance moved by
the effort P = 2 π R and load drum performs (1/T) revolution.
Distance moved by the load = T
rπ2
We know that,
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r
TRV.R.
r
TR
T
rπ2
Rπ2
loadthebytravelledDistance
effortthebytravelledDistanceV.R.
If handle is used in place of effort wheel,
r
TLV.R. Where, L = length of the handle
In general, if worm is „n‟ threaded,
rn
TL
rn
TRV.R. Where, n = number of thread on worm
If the worm is double threaded,
r2
TL
r2
TRV.R. since, n = 2
6. Single Gear Crab or Single Purchase Winch Crab:
This machine consists of mainly the larger gear wheel known as
Spur or main gear and smaller gear known as pinion. Spur or main gear is
mounted rigidly on the load drum or load axle and the spur is geared to
the pinion which is further mounted rigidly on the shaft to which the
effort wheel or handle is attached.
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A rope or string is wound round the load drum so as to lift the load
„W‟ and an another string is wound round the wheel so as to apply the
effort „P‟ as shown in the figure.
Let, W = Load lifted, P = Effort applied, D = diameter of effort
wheel, T1 = number of teeth on spur or main gear, T2 =
number of teeth on pinion d = diameter of load drum or load
axle.
For one complete revolution of effort wheel, distance moved by
the effort = πD and the pinion also completes one revolution, that time
spur performs 1
2
T
T revolutions and as load drum and spur being rigidly
connected, the load drum also performs 1
2
T
T revolutions.
Distance moved by the load = 1
2
T
T x circumference of load drum
= 1
2
T
Tx πd
We know that,
1
2
1
2
T
Tx
d
DV.R.
dxπT
T
Dπ
loadthebytravelledDistance
effortthebytravelledDistanceV.R.
If handle of length „L‟ is used in place of effort wheel,
1
2
T
Tx
d
L2V.R. where, L =length of the handle.
7. Double Gear Crab or Double Purchase Winch Crab:
This machine consists of two larger gear wheels A and C called as
spurs or main gears and smaller gear wheels B and D called as pinions as
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shown in the figure. A load drum or load axle is rigidly connected to the
spur A, which is further geared with pinion B. Pinion B and spur C are
rigidly mounted on same shaft called as intermediate shaft or axle and
spur C is further geared with pinion D mounted on the shaft. So called as
effort axle to which the effort wheel is attached.
Let, W = Load lifted, P = Effort applied, D = diameter of effort wheel,
d = diameter of load drum or load axle.
T1 = number of teeth on spur A, T2 = number of teeth on
pinion B mounted on intermediate shaft, T3 = number of teeth
on spur C mounted on intermediate shaft,
T4 = number of teeth on pinion D mounted on effort axle
For one complete revolution of effort wheel,
Distance moved by effort = πD
The pinion D on the effort axle also makes one revolution and
therefore spur C and pinion B on the intermediate shaft performs
3
4
T
Trevolution.
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That time, spur A and load drum performs same revolutions as
1
2
3
4
T
Tx
T
T because both are rigidly connected to each other.
Distance moved by the load= 1
2
3
4
T
Tx
T
T revolutions x
circumference of load drum = 1
2
3
4
T
Tx
T
T x πd
We know that,
4
3
2
1
1
2
3
4
T
Tx
T
Tx
d
DV.R.
dπxT
Tx
T
T
Dπ
loadthebytravelledDistance
effortthebytravelledDistanceV.R.
If handle of length „L‟ is used in place of effort wheel,
4
3
2
1
T
Tx
T
Tx
d
L2V.R. where, L =length of the handle.
8. Geared Pulley Block:
It consists of effort wheel or cog wheel A and a small gear wheel
called as pinion B mounted on
the same shaft. It also consists
of a load wheel C and a spur
wheel D, mounted on the same
shaft. The spur wheel D is
geared with the pinion wheel B.
An endless chain passes
over effort wheel from which
effort „P‟ is applied. The load
„W‟ is attached to a chain
which passes over the load
wheel C as shown in the figure.
Let,
T1 = number of cogs on the effort wheel A,
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T2 = number of teeth on pinion wheel B,
T3 = number of teeth on spur wheel or main gear D,
T4 = number of cogs on the load wheel C
For one complete revolution of effort wheel A (cg wheel), we get
Distance moved by effort = T1
Pinion wheel B also completes one revolution and this causes the
spur wheel D to rotate through 3
2
T
Trevolutions.
Distance moved by the load = 3
2
T
Tx T4
We know that,
4
3
2
1
3
2
T
Tx
T
TV.R.
TxT
T
T
loadthebytravelledDistance
effortthebytravelledDistanceV.R.
4
1
If the diameters of effort wheel A and load wheel C are given, then
4
3
T
Tx
d
DV.R.
Where, D = diameter of effort wheel A, d = diameter of
load wheel C
T3 = number of teeth on spur wheel B,
T4 = number of teeth on pinion wheel D
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2. FORCE SYSTEMS 12 Marks
Specific Objectives:
Define related terms in mechanics.
Calculate Components of forces.
Contents:
2.1 Fundamentals and Force Systems:……………………..... (06 Marks)
Definitions of mechanics, Engineering mechanics, statics, dynamics, Kinetics,
Kinematics, rigid body, classification of force system according to plane coplanar and
non coplanar, sub classification of coplanar force system-collinear , concurrent, non
concurrent, parallel, like parallel, unlike parallel, general etc. Definition of a force, S.I.
unit of a force, representation of a force
by vector and by Bow‟s notation method. Characteristics of a force, effects of a force,
principle of transmissibility.
2.2 Resolution of a force and Moment of a force: ………..... (04 Marks)
Definition, Method of resolution, along mutually perpendicular direction and along two
given direction. Definition of moment, S. I. unit, classification of moments, sign
convention, law of moments Varignon‟s theorem of moment and it‟s use, definition of
couple, S.I. unit, properties of couple with example.
Necessity of Knowledge of Engineering Mechanics:
In technical field, everywhere we are coming across different
forces and we have to study their effects. Engineering mechanics deals
with the study of forces and their effects. The knowledge of mechanics is
required in the subjects like strength of materials, theory of machines,
design of machines, in future. Hence for every engineer it is necessary to
have knowledge of Engineering Mechanic, so that he can develop
some technologies in any field of Engineering.
Rigid body:
The body, which do not undergo any change in its dimensions
even after application of the force.
No body is perfectly rigid. Everybody undergoes negligible
deformation, but as the deformation is negligible, the body can be
considered as rigid body. In Engineering Mechanics all the bodies are
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assumed as rigid bodies so that it becomes convenient and easy to
solve problems.
Particle:
The point mass (definitely small mass) which possesses negligible
size, shape mass and volume.
A particle is a very small amount of matter which may be
assumed to occupy a single point in space. Practically, any object
having very small dimensions as compared to its range of motion can be
called as particle, e.g. stars, planets, rockets etc
Body:
An object having definite mass, occupying definite space and
possessing properties like mass, volume etc.
Elastic Body:
It is defined as a body which regains the original size and shape
after removal of entire external load causing deformation.
Scalar Quantity:
It is defined as a physical quantity which requires only magnitude
and no direction.
e.g. Time, mass, Speed, Power, Volume etc.
Vector Quantity:
It is defined as a physical quantity which requires both magnitude
and direction. e.g. Force, Velocity, Acceleration, Displacement etc.
TYPES OF UNITS:
Basic Units:
These are the units which do not depend on any other units for
their measurements.
Length (l), mass (m) and Time (t) are said to be basic units.
Derived Units:
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These are the units which depend on other units/ basic units for
their measurements.
e.g. Velocity =Displacement / Time, Force = mass x acceleration
SYSTEMS OF UNITS:
There are four systems of units which are commonly used
M. K. S. Unit:
In this system basic units are measured as follows:
Length is measured in mm/m, Mass is measured in Kg and Time is
measured in sec.
C. G. S. Unit:
In this system basic units are measured as follows:
Length is measured in cm, Mass is measured in gram (g) and Time
is measured in sec.
F. P. S. Unit:
In this system basic units are measured as follows:
Length is measured in foot (ft), Mass is measured in Pounds and
Time is measured in sec.
S. I. Unit:
This system is universally accepted and being used in majority of
countries in the world. In this system basic units are measured as follows:
Length is measured in m, Mass is measured in Kg and Time is
measured in sec.
Engineering Mechanics or Applied Mechanics:
It is the branch of science, which deals with study of system of
forces and their effects on bodies in motion or at rest.
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Thus, the subject Engineering Mechanics covers not only the study
of forces but also it covers the effects of the forces on the bodies. The
body under consideration may be in motion or at rest. Depending on
the state of the body (in motion or at rest) Applied Mechanics is further
divided as:
Statics:
It is defined as the branch of Engineering Mechanics, which deals
with the study of system of forces and their effects on bodies at rest.
Dynamics:
It is defined as the branch of Engineering Mechanics, which deals
with the study of system of forces and their effects on bodies in motion.
The motion of a body will depend on its mass and some external
force acting on it. Depending on this, Dynamics is further divided as:
Kinematics:
It is defined as the branch of Dynamics, which deals with the study
of system of forces and their effects on bodies in motion, without
considering the mass of the body and the force causing the motion.
Kinetics:
It is defined as the branch of Dynamics, which deals with the study
of system of forces and their effects on bodies in motion, considering the
mass of the body and the force causing the motion.
FORCE:
It is an external agency, which changes or tends to change the
state of the body i.e. force will tend to change the static state of a body
to dynamic or vice versa.
Force is a vector quantity, having „N‟ (Newton) as S.I. unit.
1 KN (kilo Newton) = 1000 N
1 MN (Megs Newton) = 106 N
1 GN (Giga Newton) = 109 N
Unit Newton force:
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It is the force, which will produce an acceleration of 1 m/s2 to an
object having mass 1 kg.
Representation of Force by Vector:
A force can be represented
by a vector, graphically by drawing
a straight line parallel to the line of
action of the force, to a suitable
scale, indicating magnitude of
force and direction by an arrow head.
A force in the figure is represented by a vector of length 5 cm
(scale 1 cm = 5 N) by drawing a line parallel to the given force and
arrowhead indicates the direction of the force.
Graphical Representation of a Force:
A force can be represented graphically by drawing a straight line
to a suitable scale and parallel to the line of action of the given force
and an arrowhead indicates the direction.
Bow’s Notation:
Any force systems, when represented by a drawing, some spaces
are formed around each force. These spaces are named by capital
letters such as A, B, C …. in order. This method of putting capital letters
for each space (on either side of a force) in order is called as Bow‟s
Notation.
Bow‟s notations are used to represent any force in the graphical
solution of the problem.
F1 F2
B
AB
a
b
25 N
5 cm
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C
F3 A
D F4
In the above figure, force „F1‟ lies in between the spaces B and C,
so it can be represented as force „bc‟. The force „F4‟ lies in between the
spaces D and A, hence it can be represented as force „da‟.
Space Diagram:
It is a diagram in which all the forces of a system are drawn in the
space to a suitable scale and spaces so formed are named by Bow‟s
notations.
F2 F1
B
C θ3 θ2 A
θ1
F3 θ4
D F4
A, B, C, D --- Bow‟s Notations
Θ1, θ2, θ3, θ4 --- angles accurately measured
In case of non-concurrent forces, a suitable scale is also selected
to represent the distance between the forces
F2
C
F1 F2 F3 F4 F3
A B C D
2 m 3 m 3.5 m D 4 m
B
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F1
F4 4 m A
Vector Diagram:
The diagram in which, the forces are taken to a suitable scale and
drawn parallel to their respective lines of action of forcers drawn in the
space diagram by maintaining the same order as it was maintained in
the space diagram, is called as vector diagram.
F1=100 N
F2=80 N
F4=60 N A
BDC
F3=40 N
a b
R
a'
c
d
Space Diagram Vector
Diagram
Characteristics of a force:
1. Magnitude: The quantity of force is known as its magnitude. It is
expressed in terms of N or kN.
2. Direction: The line of action along which force acts is called as
direction. Generally it is the angle made by the force with
reference line or horizontal.
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3. Sense of Nature: The sense is indicated by an arrowhead from
which the sense like pull / push can be easily understood.
4. Point of Application: The exact point at which the force acts is
known as point of application.
Effects of a Force:
Whenever a force acts on a body, the following may be the
effects of that force on the body:
1. It may change the state of the body i.e. from ret to motion or
motion to rest.
2. It may accelerate or retard the motion of the body.
3. It may change the size and shape of the body.
4. It may turn or rotate the body.
5. It may keep the body in equilibrium (rest).
System of Forces:
When two or more forces act on a body, it is the system of forces.
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There are two main systems of forces: Coplanar and Non-coplanar
forces.
Coplanar Forces:
If lines of action (the line along which the force acts) of all forces
lie in a single plane, the force system is called as coplanar force system.
(Refer fig. 1)
F1
F3
F2 Fig: 1
Fig. 2
Systems of Forces
Coplanar Forces Non-coplanar Forces
Collinear Concurrent Non-concurrent Parallel
Forces Forces Forces Forces
Like Parallel Unlike Parallel
Forces Forces
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F2
Non-Coplanar Forces:
If lines of action (the line along which the force acts) of all forces
do not lie in a single plane, the force system is called as non-coplanar
force system. (Refer fig.2)
Types of Coplanar Forces:
Collinear Force System:
If all the forces are acting along the same straight line, the force
system is called as collinear force system. (Refer fig. 3)
Concurrent forces:
If lines of action of all forces are passing
through a common point, the force system is
called as a concurrent force system. (Refer
fig. 4)
Non-concurrent forces:
F1 F2 F3 F4
Fig. 3
F1 F2
F3
F4 F5
Fig. 4
F1 F2
F3
Fig
F5 Fig. 5 F4
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If lines of action of all forces are not passing through a common
point, the force system is called as non-concurrent force system. (Refer
fig. 5)
Parallel Forces:
If the lines of action of all forces are parallel to each other, the
force system is called as non-concurrent force system. A parallel force
system is also a non-concurrent force system.
Like Parallel Forces:
If the lines of action of all forces are parallel to each other and the
all forces are acting in same direction, the force system is called as like
parallel force system. (Refer fig. 6)
Unlike Parallel Forces: If the lines of action of all forces are parallel to
each other but all forces are not acting in same direction, the force
system is called as unlike parallel force system. (Refer fig. 7)
Principle of Transmissibility of Force:
“ If a force acts at a point on a rigid body, it is assumed to act at
any other point on the line of action of the force within the same body”.
In fig (a), as per law of transmissibility of forces, the force „F‟ is
assumed to act at any other point on the line AB (without changing the
magnitude).
F1 F2 F3 F1 F2
F3
Fig. 6 Fig. 7
A B A B A B
Fig. (a) Fig. (b) Fig. (c)
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Limitation of Principle of Transmissibility of Force:
If two equal, opposite and collinear forces are acting on the
body, and if the forces are transmitted, then the combined effect is
different than the earlier.
In fig. (b), initially, the forces are trying to create the tension, but
after transmitting these forces, they try to create the compression (fig.
(c)). Hence, this law is not applicable to equal, opposite and collinear
forces.
Resolution of a Force:
The method of splitting a given force into its components, without
changing its effect on the body.
Generally, it is convenient to resolve the force along x and y axis.
These components along x and y axis are known as Orthogonal
Components/ rectangular components.
FFy
FxO
Y
X
-VE
-VE +VE
+VE
From figure,
θCosF.FxF
FxθCos
θSinF.FyF
FyθSin
θ
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Sign Convention:
Along x-axis: Towards right - +ve
Towards left - -ve
Along y-axis: Upward - +ve
Downwards - -ve
A force can also be resolved along the two directions which are
not at right angle to each other.
F1O
F2
2
FF2
1 O F1A
F2 F
B CF1
Let, F1 and F2 be the components of a force „F‟ along the axes 1
and 2 as shown in figure at an angles α and β with the direction of force
„F‟.
Complete the parallelogram OACB.
In triangle OAC, applying sine rule, we get
βα180Sin
F
αSin
F
βSin
F 21
βαSin
F
αSin
F
βSin
F 21
βαSin
F.SinF
βαSin
βF.SinF 21
Moment of a Force:
A force when act on a body produces turning or rotational effect
is called as a moment of a force.
β
α
β
α (α+β) 180-(α+β)
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Moment (M) of a force is equal to the product of the force (F) and
the perpendicular distance between the line of action of the force and
the reference point (x). FxM
F
Line of action of force
x
A
If the force is passing through the reference point, then the
Moment (M) of a force is zero because there is no perpendicular
distance between the force and the point.
Classification of Moments:
When any force acts on a body, the body may be rotated in
clockwise or anticlockwise direction, depending on how the force is
acting on the body.
If the body is rotated in clockwise direction, the moment of the
force is clockwise moment. (Refer fig. 1).
O
d
F
d
O
FFig. 1
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If the body is rotated in anti-clockwise direction, the moment of
the force is anticlockwise moment. (Refer fig. 2)
O
d
F
d
O
Fig. 2
F
VARIGNON’S THEOREM OF MOMENTS:
“When the number of forces are acting on a body, then the algebraic
sum of moments of all the forces about any point is equal to the
moment of their resultant about the same point”. RAFA MM
Consider, a rectangle ABCD, acted upon by three forces as
shown in the figure. Let, „R‟ be the resultant of the given force system.
Let „x‟ be the perpendicular distance between the resultant „R‟ and the
point „A‟.
Now, taking moments of all the forces about point „A‟,
(considering clockwise moments +ve and anti-clockwise moments –ve)
we get
332211FA x.Fx.Fx.FM
Now, moment of resultant about point „A‟, x.RMRA
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Now, according to Varignon‟s theorem of moments,
RAFA MM
R
x.Fx.Fx.Fx
x.Rx.Fx.Fx.F
332211
332211
F2
F1R
F3
X1
X2X3
X
B
CD
A
SIGN CONVENTION FOR MOMENTS
+VE MOMENT(CLOCKWISE)
-VE MOMENT(ANTI-CLOCKWISE)
Thus, using Varignon‟s theorem of moments, we can find out the
position of the resultant w.r.t. to the reference point.
Couple:
Two equal, opposite and parallel forces acting on a body forms a
couple.
As the two forces are equal and opposite, their resultant is zero,
but they will produce rotational effect i.e. they will create the moment.
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a
P
P
O A B
Properties of a Couple:
1. Couple can be replaced by a single force.
2. Couple can not produce translatory motion (straight line motion)
but it can produce rotation.
3. Moment of a couple = force x lever arm.
4. The moment of a couple is independent of the position of moment
centre and it remains constant.
e.g. from figure, ΣMA = P x a
ΣMO = (P x OB) – ( P x OA) = P ( OB – OA)
ΣMO = P x a
Important Formulae: Fx = X – component of a force = F cosθ
Fy = Y – component of a force = Fsin θ
θ = Angle made by F with horizontal
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3. COMPOSTION OF FORCE 20 Marks
Specific Objectives:
Calculate resultant analytically for given force system.
Calculate resultant graphically.
Contents:
3.1 Analytical method: ……………………………………… (10
Marks)
Definition of Resultant force, methods of composition of forces, Law of
parallelogram of forces, Algebraic method for determination of resultant for
concurrent and non concurrent, parallel coplanar force system.
3.2 Graphical method: …………………………………………... (10 Marks)
Space diagram, vector diagram, polar diagram, and funicular polygon.
Resultant of concurrent and parallel force system only.
Resultant:
It is the single force, which will produce the same effect (in
magnitude and direction) as it is produced by number of forces acting
together.
Thus, the resultant is a single force, which will give the same result
as it is produced by the number of forces acting on a body. We can
replace all the forces by the resultant. In other words, we can say that,
the resultant is the combined effect of all the force acting on the body
(in magnitude and direction).
Composition of Forces:
The process of determining the resultant of number of forces
acting simultaneously on the body is known as the composition of the
forces.
In short, the method to find the resultant of the given force system
is called as composition of forces.
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It is the method of reducing the given force system to its
equivalent simplest system of single force or couple. Combining the
forces of any given system is known as composition of forces.
Methods of Composition of Forces:
The following are the two methods used to find the resultant of a
given force system:
1. Analytical Methods:
(a) Trigonometric Method (Law of parallelogram of forces)
(b) Algebraic Method (Method of Resolution)
2. Graphical Methods:
(a) Triangle Law of Forces
(b) Polygon Law of Forces
Parallelogram Law of Forces:
“If two coplanar concurrent forces acting at and away from the
point and are represented by the two adjacent sides of a parallelogram
in magnitude and direction, then the resultant is given by the diagonal
of the parallelogram passing through the same common point”.
P = 100 NA
Q = 80 N
R
P B
Q
D C
θ θ
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Analytical Solution for Parallelogram Law of Forces:
Consider, two forces „P‟ and „Q‟ acting at and away from point
„A‟ as shown in figure.
Let, the forces P and Q are represented by the two adjacent sides
of a parallelogram AD and AB respectively as shown in fig. Let, θ be the
angle between the force P and Q. Extend line AB and drop
perpendicular from point C on the extended line AB to meet at point E.
BPA E
Q R
D C
Consider Right angle triangle ACE,
AC2 = AE2 + CE2 =(AB + BE) 2 + CE2
= AB2 + BE2 + 2.AB.BE + CE2 = AB2 + BE2 + CE2 + 2.AB.BE
……1
Consider right angle triangle BCE,
BC2 = BE2 + CE2 and BE = BC.Cos θ
……2
Putting BC2 = BE2 + CE2 in equation (1), we get
AC2 = AB2 + BC2 + 2.AB.BE
……3
Putting BE = BC. Cos θ in equation (3),
θ
α
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AC2 = AB2 + BC2 + 2.AB. BC. Cos θ
But, AB = P, BC = Q and AC = R
θ2.P.Q.CosQPR22
In triangle ACE,
BEAB
CE
AE
CEtan
But, CE = BC. Sin θ
θ.CosQP
θSinQ.αtan
STEPS TO FIND THE RESULTANT:
1. Resolve all the forces horizontally and find the algebraic sum of
all the horizontal components (Σ Fx). Here, Σ Fx represents the horizontal
component of the resultant.
2. Resolve all the forces vertically and find the algebraic sum of all
the vertical components (Σ Fy). Here, Σ Fy represents the vertical
component of the resultant.
3. Resultant „R‟ is given by the equation, 22R FyFx
4. Let, α be the angle made by the resultant „R‟ with the
horizontal, then Fx
Fytan
RESULTANT OF NON-CONCURRENT FORCE SYSTEM
STEPS TO FIND RESULTANT OF NON-CONCURRENT FORCES:
1. Resolve all the forces horizontally and find the algebraic sum of
all the horizontal components
(Σ Fx). Here, Σ Fx represents the horizontal component of the
resultant.
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2. Resolve all the forces vertically and find the algebraic sum of
all the vertical components (Σ Fy).
Here, Σ Fy represents the vertical component of the resultant.
3. Resultant „R‟ is given by the equation, 22R FyFx
4. Let, α be the angle made by the resultant „R‟ with the
horizontal, then Fx
Fytan
5. Select some reference point (say point A) and take moments of
all the forces about that point using
correct sign conventions.
6. Find algebraic sum of moments of all the forces about the
reference point i.e. ( FAM )
7. Let, „x‟ be the perpendicular distance between the resultant
and the reference point. Take moment of
the resultant about the reference point (MRA).
8. Apply Varignon‟s theorem of moments to find the position (i.e.
distance x) of the resultant about the
reference point.
Note: 1. If FAM is + ve, then the resultant will produce clockwise
moment about the reference point.
2. If FAM is - ve, then the resultant will produce anti- clockwise
moment about the reference point.
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1.6 COMPOSITION OF FORCES
I. ANALYTICAL METHODS
Type 1: Examples on parallelogram law of forces.
Type 1.1: Examples on resultant of two equal forces.
Type 1.2: Examples on resultant of two mutually perpendicular forces.
Type 1.3: Examples on maximum and minimum values of resultant.(when
θ=0or 180)
Type 1.4: General examples on parallelogram law of forces.
Type 1.5: Examples on calculating unknown forces or angles.
Type 2: Examples on resultant of concurrent forces.
Type 2.1: Examples on pull type concurrent forces.
R2 = P2 + Q2 + 2PQ Cos Ɵ OR R = 2Pcos (Ɵ/2)
R = √(P2 + Q2) ……… Magnitude of resultant
α = tan _1 (p/Q) ……. Direction of resultant
when Ɵ =O : R = P + Q and when Ɵ =18O : R = P - Q
R =√( P2 + Q2 + 2PQ Cos Ɵ) …….. Magnitude of resultant
tan α = Q sin Ɵ / (P + Q cos Ɵ) ……. Direction of resultant
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Type 2.2: Examples on pull and push type concurrent forces.
2. Type 2.3: Examples on E, N, W, S, NE, NW, SE, SW and other
directions.
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Type 2.4: Examples on pentagon and hexagon.
Type 2.5: Given R, to find out unknown force and its inclination.
Type 2.6: Miscellaneous examples.
Type 3: Examples on resultant of non-concurrent forces.
Type 3.1: Examples on resultant of non-concurrent forces acting along
the sides of hexagon and pentagon.
Type 3.2: Examples on resultant of non-concurrent forces acting along
the sides a square or rectangle.
Type 3.3: Examples on resultant of non-concurrent forces acting along
the sides a triangle.
Type 3.4: Examples on resultant of non-concurrent forces acting on bent
up bar, straight bar and vertical pole.
Type 4: Resultant of parallel forces.
Type 4.1: Resultant of two like and unlike parallel forces.
Type 3: Examples on resultant of non-concurrent forces.
Department of Civil Engineering
Sanjay Ghodawat Polytechnic, Atigre Page 1
For Details contact:
Mr. V.S. kumbhar
HOD
Civil Department,
Sanjay Ghodawat Polytechnic, Atigre.
Mob. No.: 7798306363
Ph. No.: 0230 -246312
Email ID: [email protected]