Engineering Mechanics - Unit1 - RA
Engineering Mechanics - Unit1 - RA
Engineering Mechanics - Unit1 - RA
STATICS OF PARTICLES
1.1 Introduction
Mechanics is that branch of physical science that deals with the study of a body or
bodies under the action of a force or system of forces. The application of principles of
mechanics to solve our day to day engineering problems, is called ‘Engineering
Mechanics’.
M e c h a n i c s
M e c h a n i c s Mo f e Fc h l u a i n d i sc s o f S o l i d s
R i g i d b o dDy e f o r m a b l e b o d y
m e c h a n i c s m e c h a n i c s
S t a t i c s D y n a m i c s
K i n e m a t iK c si n e t i c s
In rigid body mechanics, all bodies are assumed to be rigid. In fact no body is rigid
and all bodies deform when loaded. However, while studying the rigid bodies, the
deformation of the bodies are not important and the concept of rigid body is justified.
Mechanics of rigid body is further divided into statics and dynamics.
The branch of science which deals with the study of a body when the body is at rest
is known as statics while the branch of science which deals with the study of a body when
the body is in motion is known as dynamics. Dynamics is further divided into kinematics
and kinetics. The study of a body in motion, when the forces which cause the motion are
not considered is called kinematics and if the forces are also considered for the body in
motion is called kinetics.
F 2
R
α θ θ
0 F 1
Figure 1.2
From figure,
where, θ = Angle between the forces
α = Angle which the resultant force makes with one of the forces
F 2
R F 2
θ φ θ
F 1 F 1
( a ) ( b )
Figure 1.3
1.2.4 Lami’s Theorem
It states that, if three forces (F1, F2, F3) acting at a point be in equilibrium, each force
is proportional to the sine of the angle between the other two. This law is also known as
sine law.
F 1
β
γ F
0 2
α
F 3
Figure 1.4
b
b
=
a
a
F
Figure 1.5
F o r c e S y s t e m
C o p l a n a r ( p l a n e ) f oN r oc ne - s c y o s p t le a m n a r ( s p a c e ) f o r c e s y s t e m
C o l i n eC a o r n c u N r ro e n n - t c o n c C u or r n e c n u t r r e Nn to n - c o n c u r r e n t
P a r a l l eN l o n p a r a l l e l P a r a l Nl e ol n p a r a l l e l
If all forces acting on a particle or a rigid body lie in same plane, then it is called
coplanar forces. In case of non-coplanar forces, all forces acting on a rigid body or a
particle may not lie in the same plane but act in the different plane and have a common
line of action is known as a collinear force system. Similarly, if all the forces act in the
same plane and they intersect at a common point, then it is called coplanar concurrent
force system. On other hand, if the entire forces act in the same plane but do not have a
common point of application, then it is called coplanar non-concurrent force system. In
case of coplanar non-concurrent force system, forces acting on a body may parallel or non-
parallel to each other. If forces are parallel to each other, then it is called coplanar
nonconcurrent parallel force system while if forces are non-parallel, then it is called
coplanar nonconcurrent non-parallel force system.
In case of non-coplanar concurrent force system, all the forces act in different planes
but they intersect at a common point. However, the non-coplanar non-concurrent force
system, all forces act in different planes but do not intersect at a common point. Some of
the classification of forces are shown in figure 1.6
P L A N E
P L A N E
F F 3 o
F 1
2
a ) C o l l i n e a r f o r c eb )s y C s o t e n m c u r r e n t f o r c e s y s t e m
F 1
F
P L A N E F 3
1
F 2
F4
c ) P a r a l l e l f o r c de ) s yN s o t en m- c o n c u r r e n t n o n - p a r a l l e l
f o r c e s y s t e m
y
S P A C E S P A C E
e ) N o n c o p l a n a r p af )r a N l l oe ln f c o o r pc el a s n y a s r t en mo n c u r r e n t f o r c e s
b c
F 2
R
θ
α θ
a d
O F 1
F 2
R F 2
θ φ θ
0 F1 F1
( a ) ( b )
In this method, the resultant of two forces (F1, F2) acting at a point can be determined
by constructing a triangle such that the forces F1 and F2 are represented by two sides of the
triangle taken in an order. The closing side of the triangle represents the resultant of two
forces as shown in figure 1.8. The major limitation of this method is that it connot be used
for finding the resultant of more than two forces.
R
F 4
F 3 F 1
F 4
O
F 2
F 3
F 1
F 2
( a ) ( b )
b) Analytical Method
Resultant of concurrent forces can also be found out by the following analytical
methods.
i. Parallelogram Law of Forces
A B
F 2 R
θ
φ θ
O F C D
1
Figure 1.10 shows the law of parallelogram of forces where the resultant of two
forces (F1, F2) inclined at an angle ‘θ ’ and acting at point ‘O’ is given by the diagonal of a
parallelogram passing through O. The resultant ‘R’ is inclined an angle φ with force F1.
To get the resultant analytically, first draw BD perpendicular to OC.
From ∆ BOD, R2 = BD2 + OD2
= BD2 + (OC + CD)2 ( OD = OC + CD)
= BD + OC + CD + 2 OC · CD
2 2 2
∴ Resultant, R = F1 + F2 + 2 F1 F2 cos θ
2 2
BD CB sin θ F2 sin θ
tan φ = = =
OC + CD OC + CB cos θ F1 + F2 cos θ
R
2
F
α
φ θ
O F C D
1
∴ Resultant, R = F1 + F2 + 2 F1 F2 cos θ
2 2
∴ = F1 + F2 − 2 F1 F2 cos α
2 2
( α = 180 − θ)
BD CB sin θ F2 sin θ
tan φ = = =
OC + CD OC + CB cos θ F1 + F2 cos θ
F2 sin θ
∴φ = tan −1
F1 + F2 cos θ
F F 3
2
F 1
F 4
F 2
F 3
R 1 R 1
O
F 1
R
F4 O
( a ) ( b )
F 1 s in θ 1
F
2 F 1
θ2 θ1
x x
– 2 Fc o θ 2 s F 1 c o θ 1s
x
0
– 3 Fc o θ 3 s F 4 c o θ 4s
x x
θ3 θ4
F
– F 3 co s θ3
– F 4 s in θ4
4
3
F
y y
where,
∑Fx = Algebraic sum of the force components along x - axis.
∑Fy = Algebraic sum of the force components along y - axis.
∴ For equilibrium condition, ∑Fx = 0 and ∑Fy = 0
T B A
A
S t r i n g
R C B
C
B
W B
B o d y u n d e r e q u i l i b r Fi u . B m . D
C R
A B R A
B
W C
B o d y u n d e r e q u i l i b F r . iB u .m D
R B A
B A B
E R C W A R
A F
C
R B A
R D
W B
D
B o d y u n d e r e q u i l i b F r . Bi u . mC
T C B
T
A C A
B C
C
W C
B o d y u n d e r e q u i l i F b . rB i u . D m
P
P
A
F θ
θ θ W A
R A
B o d y u n d e r e q u i l i b F r . i Bu m. D
SOLVED PROBLEMS
1. If two forces F1 = 30 kN and F2 = 25 kN act on a particle as shown
figure 1.15.
kN
25
= 2
F
5 0 °
O F 1= 3 0 k N
Figure 1.15
Find the resultant of these two forces by following methods.
a) Parallelogram law of forces
b) Triangle law of forces.
Solution:
a) Parallelogram Law of Forces
We know,
Resultant, R = F1 + F2 + 2 F1 F2 cos θ
2 2
( 30 ) + ( 25 ) + 2 ( 30 ) ( 25 ) cos 50º
2 2
=
= 49.89 kN
Inclination of resultant force with F1,
F2 sin θ 25 sin 50º
tan φ = = = 0.4157
F1 + F2 cos θ 30 + 25 cos 50º
We know, R = F1 + F2 − 2 F1 F2 cos α
2 2
Resultnat force,
where, α = 180 – θ = 180º – 50º = 130º
( 30 ) + ( 25 ) − 2 (30 ) (25 ) cos130º
2 2
∴R =
= 49.89 kN
kN
R 25
=
α = 1 3 F0 2 °
φ θ = 5 0 °
O
F 1 = 3 0 k N
Figure 1.16
By applying law of cosines,
R 25
=
sin130º sin φ
25 × sin130º 25 × sin130º
sin φ = =
R 49.89
= 0.3839
∴ φ = sin–1 (0.3839) = 22º 341
2. Two forces 60 N and 70 N act on a screw at an angle of 30º and 80º from
the base respectively as shown in figure 1.17. Determine the magnitude
and direction of their resultant.
Solution:
Apply parallelogram law of forces.
F 2 = 7 0 k N
F 1 = 6 0 k N
8 0 °
3 0 °
O
Figure 1.17
Resultant, R= F + F + 2 F1 F2 cos θ
1
2 2
2
= 117.89 kN
Direction of resultant,
F2 sin θ 70 sin 50º
tan α = =
F1 + F2 cos θ 60 + 70 cos 50º
= 0.5107
∴ α = tan–1 (0.5107) = 27º 31
∴ Inclination of the resultant from the base
= α + 30º = 27º 31 + 30º
= 27º 31
3. A cart is pulled by two ropes as shown in figure 1.18. The tension in rope
PQ is 4 kN. The resultant acts along the axis of the cart. Determine the
tension in rope PR and the magnitude of the resultant of two forces.
Q
N
4 k
=
T 1
3 5 °
P
2 5 °
T 2
R
Figure 1.18
Solution:
Let T1 = Tension in rope PQ = 4 kN (given)
T2 = Tension in rope PR
Resolve the forces along x - axis.
ΣH = PQ cos 35º + PR cos 25º
= T1 cos 35º + T2 cos 25º
= 4 cos 35º + T2 cos 25º
Similarlly, resolve all the forces along y - axis.
Σv = T1 sin 35º − T2 sin 25º
= 4 sin 35º – T2 sin 25º
Given that the resultant acts along the axis of the cart.
i.e., ΣH = R and Σv = 0
∴ 4 sin 35º – T2 sin 25º = 0
4 sin 35º
∴ T2 = = 5.428 kN
sin 25º
Then, Resultant R = 4 cos 35º + 5.428 cos 25º
= 8.196 kN
4. Determine the magnitude and direction of the resultant of the forces
acting on the bolt as shown in figure 1.19.
2 0 N
3 0 N 1 0 N
3 0 2° 0 °
3 0 °
Figure 1.19
Solution:
Resolve all the forces along x - axis.
∑Fx = 10 cos 30º + 20 cos 70º – 30 cos 60º
= 0.50 N
Resolve all the forces along y - axis.
∑Fy=10 sin 30º + 20 sin 70º + 30 sin 60º
= 49.77 N
( ΣFx ) + ( ΣFy )
2 2
=
∴ Resultant, R
( 0.50 ) + ( 49.77 )
2 2
=
= = 49.8 N
Inclination of resultant,
ΣF 49.77
θ = tan −1 y = tan−1
ΣF
x 0.50
= 89.25º
5. The force system shown in figure 1.20 has a resultant of 100 N pointing up
along the y - axis. Compute the values of F and θ required to give this
resultant.
y
F
θ
2 0 0 N x
O
4 5 °
1 2 0 N
Figure 1.20
Solution:
Resolve all the forces along x and y axis.
ΣFx = F cosθ + 120 cos 45º – 200
ΣFy
= F sinθ – 120 sin 45º
Given that the resultant of 100 N pointing up along y - axis.
i.e., ∑Fx = R
and ∑Fy = 0
F cosθ + 120 cos 45º – 200 = 0
∴ F cosθ = 115.14
F sinθ – 120 sin 45º = 100
∴ F sinθ = 184.84
F sin θ 184.84
=
Then, F cos θ 115.14
tan θ = 1.6054
∴ θ = tan–1 (1.6054) = 58º 41
1150.14
F= = 217.6 N
cos 58º 41
y
6 P
P
4 5 ° 6 0 °
o 3 P
3 0 °
4 P
Figure 1.21
Solution:
Resolve all the forces along x and y direction.
i.e., ∑Fx = P cos 60º + 3P – 6P cos 45º + 4P cos 60º
= 1.257 P
∑Fy = P sin 60º + 6 P sin 45º – 4 P sin 60º
= 1.644 P
( ΣFx ) + ( ΣFy )
2 2
=
∴ Resultant, R
( 1.257 P ) + (1.644 P )
2 2
=
= 2.06 P
Direction of resultant force,
ΣF 1.644 P
θ = tan −1 y = tan−1
ΣFx 1.257 P
= 52º 351
7. Find the magnitude and direction of the resultant from the following cases.
a) 30 N inclined at 25º towards North of East
b) 25 N towards North
c) 35 N inclined at 40º towards south of west
d) 30 N towards North west.
N
2 5 N
3 0 N
3 0 N
4 5 ° 3 0 °
W E
O
4 0 °
3 5 N
Figure 1.22
Solution:
Let us consider x and y axes along the East and North directions.
Resolve all the forces along x and y direction
∑Fx = 30 cos 30º – 30 cos 45º – 35 cos 40º
= –22.04 N
∑Fy = 30 sin 30º + 25 + 30 sin 45º – 35 sin 40º
= 38.71 N
( ΣFx ) + ( ΣFy )
2 2
=
∴ Resultant, R
( −22.04 ) + ( 38.71 )
2 2
=
= 44.54 N
ΣFy 38.71
tan φ = =
ΣFx 22.04
∴ φ = 60.34º
∴ The resultant lies in the second quadrant.
8. Find the resultant of the system of forces shown in figure 1.23.
y - a x i s
1 0 N
1 5 N
5 3
1 2β 4
α
5 0 N
θ
8
1 5
1 2 N
7 0 N
Figure 1.23
Solution:
From figure 1.23
cos α = 4/5, or tan α = 3/4, sin α = 3/5
cos β = 12/13, sin β = 5/13
cos θ = 15/17, sin θ = 8/17
Resolve all forces along x and y axis
∑Fx = 50 + 15 cosα + 10 cosβ – 12 cosθ
= 50 + 15 × 4/5 + 10 × 12/13 – 12 × 15/17
= 60.64 N
∑Fy = 15 sinα – 10 sinβ – 12 sinθ – 70
= 15 × 3/5 – 10 × 5/13 – 12 × 8/17 – 70
= –70.49 N
( ΣFx ) + ( ΣFy )
2 2
=
∴ Resultant, R
( 60.64 )
+ (− 70.49 ) = 92.98 N
2 2
=
ΣFy 70.49
tan φ = =
ΣFx 60.64
θ = 49.29º
The resultant lies in the fourth quadrant.
9. A system of five forces of 4 kN, 5 kN, 6 kN, 7 kN and 8 kN act at one of the
angular points of a regular hexagon and pass through the other angular
points as shown in figure 1.24. Find the magnitude and direction of the
resultant of the force system.
7 k N 6 k N
5 k N
8 k N
3 0 3° 0 °
3 0 °
3 0 °4 k N
Figure 1.24
Solution:
Resolving all the forces along x and y directions.
∑Fx = 4 + 5 cos 30º + 6 cos 60º – 8 cos 60º
= 7.33 kN
∑Fy = 5 sin 30º + 6 sin 60º + 7 + 8 sin 60º
= 21.62 kN
( ΣFx ) + ( ΣFy )
2 2
=
Resultant, R
( 7.33) + ( 21.62 )
2 2
=
= 22.23 kN
ΣFy 21.62
tan φ = = = 2.95
ΣFx 7.33
∴ φ = 71.3º
10. A system of four forces act on a bolt as shown in figure 1.25. Determine the
resultant of the forces on the bolt.
8 0 N Y
2 0 ° 1 5 0 N
3 0 °
X
1 5 °
1 0 0 N
1 1 0 N
Figure 1.25
Solution:
Resolve all the forces along x and y directions.
∑Fx = 150 cos 30º + 100 cos 15º – 80 cos 70º
= 199.134 N
∑Fy = 150 sin 30º – 100 sin 15º + 80 sin 70º – 110
= 14.293 N
( ΣFx ) + ( ΣFy )
2 2
=
∴ Resultant, R
( 199.134 ) + ( 14.293 )
2 2
=
= 199.64 N
ΣFy 14.293
tan φ = =
ΣFx 199.134
∴ φ = 4.10º
Direction of resultant,
−6
tan φ =
8
∴ φ = tan–1 (–6/8) = –36º 521
Counterclock wise angle (ccw) = 360 – 36º 521 = 323.48º
12. Three forces +20N, –10N and +30N are acting perpendicular to xz plane
as shown in figure 1.26. The lines of action of all the forces are parallel to
axis. The co-ordinate of the point of action of these forces along x and z
directions are respectively (2, 3), (4, 2) and (7, 4). All distances being
refered in metres find out, a) The magnitude of the resultant force,
b) The location-of the resultant.
Solution:
Resolve all forces along y – axis.
∴ Resultant R= ∑Fy = 20 – 10 + 30 = 40 N(↑)
In order to determine the location of resultant from oz, equate the moment of
resultant with moment of the algebraic sum of all the force with respect to plane.
y
2 0 N 1 0 N 3 0 N
2 m 2 m 3 m
O x
Figure 1.26
∴R×x = Σ Mz = Σ Mo
40 × x = (20 × 2) – (10 × 4) + (30 × 7)
210
∴x = = 5.25m
40
To determine the z co-ordinates of the resultant from ox, equate the moment of
resultant with moment of the algebraic sum of all the forces with respect to yz plane.
∴ R × z = Σ M x = ΣM o
40 × z = –(30 × 4) – (20 × 3) + 10 × 2 = –160 N.M
−160
∴z = = − 4.0 m
40
y
3 0 N 2 0 N 1 0 N
1 m 1 m 2 m
z O
However, the z co-ordinate must be such that a force of 40 N (acting up) will have
negative moment of 100 N-M. Therefore, R must be to the left of O. In this case the z co-
ordinate is positive when it is to the left of O.
∴ z = + 4.0 m
∴ The resultant of 40N (↑) locating at (5.25, 4.0)m
13. A force ‘F’ acts at the origin of a co-ordinate system in a direction defined
by the angles θ x = 69.3º and θ 2 = 57.9º. If the components of the force
‘F’ along y - directions is –174 N. Determine
a) The angle θ y
b) Other components of the force ‘F’
c) The magnitude of the force ‘F’ .... (Nov. 2001)
Solution:
Given, θ x
= 69.3º and θ z
= 57.9º, Fy = –174 N
We know,
cos2 θ x + cos2 θ y
+ cos2θ 2
= 1
cos2 (69.30º) + cos2 (57.9º) + cos2θ y
= 1
or cos2 θ y
= 0.5928
or cos θ y
= ± 0.7699
∴ θ y
= 40º or θ y
= 140º
Magnitude of the force cannot be negative though its components may be negative,
hence θ y should be 140º.
F = –174 / cos 140º = 227.14 N
Fx = F cos θ x = 227.14 × cos (69.3º) = 80.28 N
Fz = F cosθ z = 227.14 × cos (57.9º) = 120.70 N..
Solution:
Given Fx= 30 kN, Fy = –24 kN and Fz = 18 kN.
∴ Force vector, F = Fx i + Fy j + Fz k
= 30i − 24 j + 18k
Also, the component of the force along AB
= F · nˆ AB
where, n̂ = Unit vector along AB
AB
=
AB
( x B − x A ) i + ( y B − y A ) j + ( z B − z A) K
=
( x B − x A ) + ( y B − y A ) + ( z B − z A)
2 2 2
−2i − 4 j − 5k
=
( −2 ) + ( −4 ) + ( 5 )
2 2 2
= F nˆ AB
= ( 30i − 24 j + 18k ) ( −0.30i − 0.60 j + 0.75k)
= –9 + 14.4 + 13.5
= 18.9 N
15. If five forces act on a particle as shown in figure 1.27, and if the algebraic
sum of horizontal components of all forces is +250 N, calculate the
magnitude of ‘F’ and the resultant of all the forces.
y
2 5 k N
1 0 k N
F
3
7 k N 4 53 °0 ° 4
x
O
Figure 1.27
Solution:
From figure,
Resolve all the forces along x - axis
∑Fx = F cos (36.87º) + 25 cos 45º – 10 cos 30º – 7
= F cos 36.87º + 4.59
But, ∑Fx = +250N (Given)
or + 250= F cos 36.87º + 4.59
∴ F = 363.28 kN
Resolve all the forces along y - axis.
∑Fy = 363.28 sin 36.87º – 25 sin 45º + 10 sin 30º
= –299 kN
( ΣFx ) + ( ΣFy )
2 2
=
Resultant, R
( 250 ) + ( −299 ) = 389.8 kN
2 2
=
ΣF
φ = tan −1 y = 50.10º
ΣFx
16. Examine the equilibrium condition for the particle as shown in figure 1.28.
4 0 0 N y
6 0 °
x 3 0 0 N
O
6 0 °
1 7 3 . 2 N
2 0 0 N
Figure 1.28
Solution:
The necessary condition for equilibrium of particle are,
∑Fx = 0 and ∑Fy = 0
∑Fx = 300 – 200 cos 60º – 400 cos 60º = 0
∑Fy = –173.2 – 200 sin 60º + 400 sin 60º = 0
Hence the particle will be in equilibrium.
17. Two cables are tied together at ‘N’ and loaded as shown in figure 1.29.
Determine the tension in cables MN and ON,
O
6 0 °
N
2 0 °
M
5 0 0 N
Figure 1.29
Solution:
Let, T1 and T2 be the tension in cable MN and ON respectively.
The particle N will be in equilibrium if the resultant of all the forces acting on it is
zero.
y T
y T 2
2
1 4 0 °
6 0 °
x x
2 0 °
1 5 0 °
7 0 °
T 1 T 1
W = 5 0 0 N W = 5 0 0 N
Q 2 0 °
3 0 ° P
4 5 0 N
4 0 k g
Figure 1.30
Solution:
y
T 2
T 1
5 0 3° 0 °
x 4 5 0 N
P
W = 4 0 k g = 4 0 × 9 . 8 1 = 3 9 2 . 4 N
2 0 °
W = 3 0 0 N
Figure 1.31
Solution:
F.B.D of sphere
T
T
1 1 0 °
7 0 °
R
R 1 6 0 °
W = 3 0 0 N
W = 3 0 0 N
Let R be the reaction of the wall and T be the tension in the string.
Apply lami’s theorem.
300 T R
= =
sin110º sin 90º sin160º
300 × sin 90º 300 × sin160º
∴T = = 319.25 N ∴R = = 109.19 N
sin110º sin110º
20. A chord supported at A and B carries a load of W at ‘C’ as shown in
figure 1.32. Find the value of W so that CD remains horizontal.
A B
6 0 ° 3 0 °
C D
W 2 0 k N
Figure 1.32
Solution:
Draw the F.B.D of the system.
T D B T D B
3 0 ° 1 5 0 °
T D C
D
T D C 1 2 0 °
W = 2 0 k N W = 2 0 k N
Let TDC and TDB be the tension in the chord DC and DB respectively.
Apply lami’s theorem.
20 TDB TDC
= =
sin150º sin 90º sin120º
20 × sin 90º
∴ TDB = = 40 kN
sin150º
20 × sin120º
TDC = = 34.64 kN
sin150º
T T C A
C A
1 2 0 °
6 0 ° T C A= T D C= 3 4 . 6 4 k N
C 1 5 0 ° T C D= 3 4 . 6 4 k N
W W
and
34.64 × sin120º
W= = 60 kN
sin150º
21. Determine the tension in various segments of the connected flexible cables
shown in figure 1.33.
3 0 °
P Q
6 0 °
3 0 0 N
T
4 5 °
S
4 0 0 N
Figure 1.33
Solution:
Consider the free body diagram of joint ‘S’
T S Q T S T T S Q T S T
1 0 5 °
3 0 ° S 4 5 °
1 2 0 ° 1 3 5 °
4 0 0 N 4 0 0 N
Let TSQ and TST be the tensions in the cable SQ and ST respectively.
Apply lami’s theorem.
400 TST TSQ
= =
sin105º sin120º sin135º
∴
400 × sin120º
TST = = 358.7 N
sin105º
400 × sin135º
TSQ = = 292.82 N
and, sin105º
T Q R
6 0 °
T Q P Q 3 0 °
T Q =S S TQ = 2 9 2 . 8 2 N
3 0 0 N
22. A wire fixed at two points A and D as shown in figure 1.34. Two weights of
10 kN and 30 kN are supported at B and C respectively. When
equilibrium is reached it is found that the inclination of AB is 20º and that
of CD is 50º to the verticle, determine the tension in the segment AB, BC
and CD of the wire and also the inclination of BC to the verticle.
D
A
5 0 °
2 0 °
B θ
C
3 0 k N
3 0 k N
Figure 1.34
T C B T C D
7 0 ° θ 4 0 °
θ C
B
T B C
3 0 k N 3 0 k N
For joint B
Resolve all the forces along x and y axis.
= 0
TBC cos θ – TBA cos 70º = 0
or
TBA cos
TBA = = 2.92 TBC cos θ
cos 70º
Similarly, = 0
–TBC sinθ – 10 + TBA sin 70º = 0
–TBC sinθ + 2.92 TBC cosθ sin 70º = 10
–TBC sinθ + 2.74 TBC cosθ = 10
TBC (2.74 cosθ – sinθ ) = 10 .... (1)
For joint C
∑Fx = 0
TCB cos 40º – TCB cosθ = 0
or TCD = 1.30 TCB cosθ
Similarly, = 0
TCD sin 40º + TCB sinθ – 30º = 0
1.30 TCB cosθ sin 40º + TCB sinθ = 30
0.839 TCB cosθ + TCB sinθ = 30
TCB (0.839 cosθ + sinθ ) = 30 .... (2)
Divide (1) / (2)
T BC ( 2.74 cos θ − sin θ ) 10
= ( TBC = TCB )
T CB ( 0.839 cos θ + sin θ ) 30
23. A fine light string ABCDE whose extremity ‘A’ is fixed, has weights
W1 and W2 attached to it at B and C. It passes round a small smooth pulley
at D carrying a weight of 40 kg at the free end E as shown in figure 1.35.
1 5 0 ° 1 2 0 °
E
B C
4 0 k g
W 1 W 2
Figure 1.35
If in the position of equilibrium, BC is horizontal and AB and CD makes
150º and 120º with BC, find i) Tensions in the portion AB, BC and DC of
the string, ii) Magnitudes of W1 and W2.
Solution:
T B A T C D = 4 0 × 9 . 8 1
= 3 9 2 . 4 N
1 5 0 ° 1 2 0 °
B C
1 2 0 ° T T C B
1 5 0 °
B C
W 1 W 2
For joint B
Applying lami’s equation at ‘B’
TBA W1 196.2
= =
sin 90º sin150º sin120º
196.2 × sin 90º
TBA = = 226.6 N
∴ sin120º
196.2 × sin150º
W1 = = 113.27 N
and, sin120º
B
kN
F =2
W
3 0 °
3 0 °
A
R
W
Figure 1.36
Solution:
R
1 2 0 °
3 0 °
F
1 5 0 °
W = 2 0 0 0 N
F.B.D
Apply lami’s equation
F 2000 R
= =
sin150º sin120º sin 90º
2000 × sin150º 2000 × sin 90º
F= = 1154.70 N R= = 2309.4 N
∴ sin120º sin120º
1 0 0 0 N
E
D
4 0 ° 5 0 °
Figure 1.37
Solution:
R R
1 0 0 0 N E
D
9 0 °
1 3 0 ° 1 4 0 °
5 0 ° 4 0 °
R D R E
1 0 0 0 N
F.B.D of Ball
Apply lami’s theorem.
1000 RD RE
= =
sin 90º sin130º sin140º
1000 × sin130º
∴ RD = = 766.04 N
sin 90º
1000 × sin140º
RE = = 642.78 N
and, sin 90º
26. Two identical rollers each weighing 200 N are placed in a trough as shown
in figure 1.38. Assuming all surfaces of contact are smooth, find the
reactions developed at the point of contact surfaces.
B
A
D
4 0 °
Figure 1.38
Solution:
O 1
R B
4 0 °
R O 2
D 4 0 °
5 0 °
R A
2 0 0 N
5 0 °
R C
2 0 0 N
R C R R
A B
5 0 ° O 2 9 0 °
R D 5 0 ° 4 0 °
4 0 °
1 4 0 ° 1 3 0 °
R B
2 0 0 N
2 0 0 N
F.B.D of Balls
For Ball O1
Apply lami’s theorem,
200 RB RA
= =
sin 90º sin140º sin130º
200 × sin140º
∴ RB = = 128.6 N
sin 90º
200 × sin130º
RA = = 153.20 N
sin 90º
For Ball O2
Resolve all forces along x and y axis.
∑Fx = 0
RD – RB cos 40º – RC cos 50º = 0
∴ RD = RB cos 40º + RC cos 50º .... (1)
∑Fy = 0
–200 – RB sin 40º + RC sin 50º = 0
R B sin 40º + 200 128.6 sin 40º + 200
RC = =
∴ sin 50º sin 50º
= 368.98 N
Substituting RD in equation (1)
∴ RD = 128.6 cos 40º + 368.98 cos 50º
= 335.69 N
27. Two cylinders M and N rest in a channel as shown in figure 1.39. The
cylinder M has diameter of 100 mm and weighs 200 N, whereas the cylinder
N has diameter of 180 mm and weighs 500 N. If the bottom width of the
box is 180 mm with one side vertical and the other inclined at 60º, determine
the pressures at all the four points of contact.
C
D
M
+ H
N G
+
F
6 0 °
A E B
1 8 0 m m
Figure 1.39
Solution:
( RE – 5 0 0 )
M R G
J R R C
H
5 6 ′ ° 9
R 3 0 °
N G
2 0 0 N R J
H 5 6 ′ ° 9I
I θ K
9 0 m m
5 0 0 N
2 0 0 N R G
3 06 ° 0 °
R F A E L B
R E
F.B.D of cylinders
From the geometry of the figure,
IAE = 60º
AE = IE cot 60º = (180/2) × 0.577 ( cot θ = 1/tanθ )
= 52 mm
LB = 100/2 = 50 mm
EL = IK = 180 – 52 – 50 = 78 mm
IJ = 90 + 50 = 140 mm
IK 78
∴ cos θ = = = 0.5571
IJ 140
∴ θ = 50º 9’
Considering the equilibrium of cylinder M.
Apply lami’s equation at J.
RH RG 200
= =
sin ( 90º + 56º 9 ' ) sin 90º sin (180º − 58º 9 ' )
200 × sin ( 90º + 56º 9 ')
∴ RH =
sin ( 180º − 56º 9 ')
= 134.2 N
200 × sin 90º
RG =
sin ( 180º − 56º 9 ' )
and
= 240.8 N
Considering the equilibrium of cylinder N.
Apply lami’s theorem.
( RE − 500 )
=
240.8
=
RF
sin ( 180º + 30º − 50º 9') sin 60º sin ( 90º + 50º 9 ')
240.8 × sin ( 90º + 56º 9 ')
∴ RF =
sin 60º = 154.9 N
240.8 × sin ( 180º + 30º − 56º 9 ')
R E − 500 =
sin 60º = 122.5 N
∴ RE = 122.5 + 500 = 622.5 N
1.4 Introduction to Equilibrium of Rigid bodies
In the previous unit, we have analyzed the system of forces on a particle in which we
assumed each body as a particle. This assumption is valid, if the body has negligible size.
But in many cases, this assumption may not be possible. When a body is not subjected to
concurrent force system then the body is said to be a rigid body. A rigid body is a
combination of particles in large numbers. For the equilibrium of rigid body, the size of
the body, forces acting on different point of applications has to be taken into
consideration.
The basic and important conditions to be considered for the equilibrium of a rigid
body are the summation of forces and moments in each direction is taken as zero. By
taking the above conditions, the forces and moments of forces are balanced in each
direction. Another important consideration is that the system of external forces will not
impart translational or rotational motion on the body taken. When a stationary body is
acted upon by some external forces, the body may start to rotate (or) may start to move
about any point or an axis. If the body does not move or rotate about any point or an axis,
then the body is said to be in equilibrium.
A o 2
d 2
d1
o1
Figure 1.40
Consider a force ‘F’ applied to a rigid body (Figure 1.40) at A. The force tends to
rotate the body about O. The point ‘O’ is called the moment centre. The perpendicular
distance between the line of action of force and the point about which moment is
calculated is called moment arm.
Mathematically,
M=F×d
where, F = Force applied
d = Moment arm
If point O1 is taken as the moment centre,
M1= F × d1 CCW (Counter clockwise sense)
If point O2 is taken as the moment centre,
M2= F × d2 CW (Clockwise sense)
The tendency of the moment is to rotate the body in the clockwise direction about O.
Hence the moment is called clockwise moment. If the tendency of a moment is to rotate
the body in anticlockwise direction, then that moment is known as anticlockwise moment.
F 1
d 1
d
d2 F
F 2
A
Figure 1.41
1.7 Couple
A couple is defined as two parallel forces that have the same magnitude, opposite
directions and are separated by a perpendicular distance ‘d’ as shown in figure 2.42. The
perpendicular distance between the parallel forces is called arm of the couple. Couple has
a tendency to rotate the body.
– F
F
Figure 1.42
Moment of a couple is the product of any one of the parallel forces and
perpendicular distance between the forces.
Moment of couple = Force × arm of the couple
F F
M M
= = F
d d
F M = F d
N
N F N
( a ) ( b ) ( c )
Figure 1.43
Apply equal and opposite forces at N (Figure 1.43(b)) so that the equilibrium of the
system is not disturbed. The system of forces shown in figure 1.43 (b) is same as that
shown in figure 1.43 (a). Now the force at M and the downward force at N form a couple
of magnitude M = F ×d (Clockwise). Hence at N, we have a couple M and a force ‘F’ as
shown in figure 1.43(c). The system shown in figure 1.43(c) is same as that shown in
figure 1.43(b).
1.12 Resultant of Coplanar Non-Concurrent Forces in Plane
F 3
F 3
F 1
F 1
Σ Μ ο
o o
( a ) F 2 F 2
( b )
Σ Μ ο
o
y R
( c )
φ
R
A
R
R d x
o
o
Σ Μ ο
( d ) ( e )
Figure 1.44
C
B 0 1
D
F
0 2
E
0 . 8 m m
of 150 N is acting towards the origin at 115º to the horizontal. Find the total verticle
and horizontal components of these two forces. Also find the magnitude and
direction of resultant.
(Ans: Σ H = 154 N, Σ V = –93.68 N, R = 180.25 and φ = 31.31º
24. A lamp weighing 10N is suspended from the ceiling by a chain. It is pulled aside
by a horizontal cord until the chain makes an angle of 60º with the ceiling as shown
in figure. Find the tension in the chain and the cord by applying lami’s theorem.
A
6 0 °
C h a i n
B
O C o r d
2 0 N
5
1 2
2 5 N
3 0 º
1 0 N
26. A force acts at the origin in a direction defined by the angles θ y = 65° and θ z = 40°.
Knowing that the x component of force is -90kN, determine (a) the other components and
magnitude of force. (b) the value of θ x.
27. The x,y,z components of a force are 36kN, -24kN and 24kN respectively. Find the
component of this force along the line joining A(1,2,-3) and B(-1,-2,2).