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INSTITUTE OFAERONAUTICAL
ENGINEERING
(Autonomous)
Dundigal, Hyderabad - 500043
Course : ENGINEERING MECHANICS
(AME002)
Prepared by : Mr. B.D.Y.Sunil
Assistant Professor
1
Engineering Mechanics – Dynamics
Subject
Engineering Mechanics – Dynamics 2
30%
70%
 Graduates:
◦ Midterm exam
◦ Final exam
 Course Materials
◦ Lecture notes
 Power points slides
 Class notes
◦ Textbooks
 Engineering Mechanics: Statics 10th Edition by R.C.
Hibbeler
2
Engineering Mechanics – Dynamics
COURSE OBJECTIVES
Engineering Mechanics – Dynamics 3
The course should enable the students to:
III.
I. Develop the ability to work comfortably with basic engineering mechanics
concepts required for analysing static structures.
II. Identify an appropriate structural system to studying a given problem and
isolate it from its environment, model the problem using good free body
diagrams and accurate equilibrium equations.
Identify and model various types of loading and support conditions that act
on structural systems, apply pertinent mathematical, physical and
engineering mechanical principles to the system to solve and analyze
the problem.
IV. Solve the problem of equilibrium by using the principle of work and energy
in mechanical design and structural analysis.
V. Apply the concepts of vibrations to the problems associated with dynamic
behavior.
3
Engineering Mechanics – Dynamics
COURSE OUTCOMES
Engineering Mechanics – Dynamics 4
After completing this course the student must
demonstrate the knowledge and ability to:
1.Classifying different types of motions in kinematics.
2.Categorizing the bodies in kinetics as a particle,rigid
body in translation and rotation.
3.Choosing principle of impulse momentum and virtual
work for equilibrium of ideal systems, stableand
unstable equilibriums
4.Appraising work and energy method for particle
motion and plane motion.
5.Apply the concepts of vibrations.
4
Engineering Mechanics – Dynamics
KINEMATICS
KINETICS
NEWTON’S LAW
KINETICS
ENERGY & MOMENTUM
PARTICLE SYSTEM OF
PARTICLES
RIGID BODIES
Chapter 1
Chapter 2
Chapter 3
Chapter 4
Chapter 3
Chapter 4
Chapter 5
Course Outline
Engineering Mechanics – Dynami5cs 5
Engineering Mechanics – Dynamics
Introduction to Mechanics
Mechanics
Statics Dynamics
Kinematics Kinetics
Engineering Mechanics – Dynamics 6
 What is mechanics?
Physical science deals
with the state of rest or
motion of bodies under
the action of force
 Why we study mechanics?
This science form the
groundwork for further
study in the design and
analysis of structures
6
Engineering Mechanics – Dynamics
BasicTerms
Engineering Mechanics – Dynamics 7
 Essential basic terms to be understood
◦ Statics: dealing with the equilibrium of a rigid-body at rest
◦ Rigid body: the relative movement between its parts are negligible
◦ Dynamics: dealing with a rigid-body in motion
◦ Length: applied to the linear dimension of a straight line or curved line
◦ Area: the two dimensional size of shape or surface
◦ Volume: the three dimensional size of the space occupied by substance
◦ Force: the action of one body on another whether it’s a push or a pull
force
◦ Mass: the amount of matter in a body
◦ Weight:the force with which a body is attracted toward the centre of the
Earth
◦ Particle:a body of negligible dimension
7
Engineering Mechanics – Dynamics
Units of Measurement
1/27/2017 Engineering Mechanics – Dynamics 8
 Four fundamental quantities in mechanics
◦ Mass
◦ Length
◦ Time
◦ Force
 Two different systems of units we dealing with during the
course
◦ Units (CGS)
 Length in centimeter(cm)
 Time in Seconds (s)
 Force in kilograms (kg)
◦ International System of Units or Metric Units (SI)
 Length in metre (m)
 Time in Seconds (s)
 Force in Newton (N)
8
Engineering Mechanics – Dynamics
Units of Measurement
Engineering Mechanics – Dynamics 9
Quantity
SI Units US Units
Unit Symbol Unit Symbol
Mass kilogram kg slug -
Length meter m foot ft
Time second s second sec
Force newton N pound lb
Summery of the four fundamental quantities
in the two system
9
Engineering Mechanics – Dynamics
Units of Measurement
Engineering Mechanics – Dynamics 10
 Metric System (SI)
◦ SI System offers major advantages relative to the FPS system
 Widely used throughout the world
 Use one basic unit for length  meter; while FPS uses many basic units
 inch,foot,yard,mile
 SI based on multiples of 10, which makes it easier to use & learn whereas
FPS is complicated,for example
 SI system 1 meter = 100 centimeters,1 kilometer = 1000 meters,etc
 FPS system 1 foot = 12 inches,1 yard = 3 feet,1 mile = 5280 feet,etc
 Metric System (SI)
◦ Newton’s second law F = m.a
 Thus the force (N) = mass (kg)  acceleration (m/s2)
◦ Therefore 1 Newton is the force required to give a mass of 1 kg
an acceleration of 1 m/s2
10
Engineering Mechanics – Dynamics
Units of Measurement
 U.S. Customary System (FPS)
◦ Force (lb) = mass (slugs)  acceleration (ft/sec2 )
 Thus (slugs) = lb.sec2/ft
◦ Therefore 1 slug is the mass which is given an
acceleration of 1 ft/sec2 when acted upon by a force
of 1 lb
 Conversion of Units
◦ Converting from one system of unit to another;
 The standard value of g (gravitational
acceleration)
◦ SI units g = 9.806 m/s2
◦ FPS units g = 32.174 ft/sec2
Quantity FPS Equals SI
Force 1 lb 4.448 N
Mass 1 slug 14.593 kg
Length 1 ft 0.304 m
Engineering Mechanics – Dynamics 11
11
Engineering Mechanics – Dynamics
Objectives
Engineering Mechanics – Dynamics 12
T
oprovide an introductionof:
※ Fundamental concepts,
※ General principles,
※ Analysis methods,
※ Future Studies
in Engineering Mechanics.
12
Engineering Mechanics – Dynamics
Outline
Engineering Mechanics – Dynamics 13
 1. EngineeringMechanics
 2. FundamentalConcepts
 3. GeneralPrinciples
 4. StaticAnalysis
 5. DynamicAnalysis
 6. FutureStudies
13
Engineering Mechanics – Dynamics
1. Engineering Mechanics
Engineering Mechanics – Dynamics 14
 Mechanics :
- Rigid-body Mechanics
- Deformable-body Mechanics
- Fluid Mechanics
 Rigid-body Mechanics :
- Statics
- Dynamics
14
Engineering Mechanics – Dynamics
 Statics – Equilibrium Analysis of
particles and bodies
 Dynamics – Accelerated motion of
particles and bodies
Kinematics and Kinetics
 Mechanics of Materials…
 Theory ofVibration…
1. Engineering Mechanics
Engineering Mechanics – Dynamics 15
15
Engineering Mechanics – Dynamics
2. Fundamentals Concepts
Engineering Mechanics – Dynamics 16
Basic Quantities
 Length, Mass,Time,Force
Units of Measurement
 m, kg,s,N… (SI, Int.System of Units)
- Dimensional Homogeneity
- Significant Figures
16
Engineering Mechanics – Dynamics
2. Fundamentals Concepts
Engineering Mechanics – Dynamics 17
Idealizations
 Particles
– Consider mass but neglect size
 Rigid Body
– Neglect material properties
 Concentrated Force
 Supports and Reactions
17
Engineering Mechanics – Dynamics
3. General Principles
Engineering Mechanics – Dynamics 18
- Newton’s Laws of Motion
 First Law, Second Law,Third Law
 Law of GravitationalAttraction
- D’Alembert Principle :F+(-ma)=0
- Impulse and Momentum
- Work and Energy
- Principle ofVirtualWork (Equilibrium)
18
Engineering Mechanics – Dynamics
4. StaticAnalysis
Engineering Mechanics – Dynamics 19
 Force and Equilibrium
 Force System Resultants
 StructuralAnalysis
 Internal forces
 Friction
 Centroid and Moments of Inertia
 VirtualWork andStability
19
Engineering Mechanics – Dynamics
5. DynamicAnalysis
Engineering Mechanics – Dynamics 20
 Kinematics of a Particle
 Kinetics: Force andAcceleration
 Work and Energy
 Impulse and Momentum (Impact)
 Planar Kinematics and Kinetics
 3-D Kinematics and Kinetics
 Vibrations
20
Engineering Mechanics – Dynamics
UNIT-I
KINEMATICS OF
PARTICLES IN
Engineering Mechanics – Dynamics 21
RECTILINEAR MOTION
Motion of a particle, rectilinear motion, motion curves, rectangular
components of curvilinear motion, kinematics of rigid body, types of
rigid body motion, angular motion, fixed axis rotation.
21
Engineering Mechanics – Dynamics
INTRODUCTION TODYNAMICS
Engineering Mechanics – Dynamics 22
 Galileo and Newton (Galileo’s
experiments led to Newton’s laws)
 Kinematics – study of motion
 Kinetics – the study of what causes
changes in motion
 Dynamics is composed of kinematics
and kinetics
22
Engineering Mechanics – Dynamics
Engineering Mechanics – Dynamics 23
Introduction
• Dynamics includes:
- Kinematics: study of the motion (displacement, velocity,
acceleration, & time) without reference to the cause of motion
(i.e. regardless of forces).
- Kinetics: study of the forces acting on a body, and the resulting
motion caused by the given forces.
• Rectilinear motion: position, velocity, and acceleration of a
particle as it moves along a straight line.
• Curvilinear motion: position, velocity, and acceleration of a
particle as it moves along a curved line.
23
Engineering Mechanics – Dynamics 24
RECTILINEAR MOTION OF PARTICLES
24
Rectilinear Motion: Position,
Velocity & Acceleration
Engineering Mechanics – Dynamics 25
Acceleration
MECHANICS
Kinematics of Particles
Motion in One Dimension
26
Engineering Mechanics – Dynamics
Summary of properties of vectors
27
Engineering Mechanics – Dynamics
POSITION, VELOCITY, AND
ACCELERATION
For linear motion x marks the position of an object.
Position units would be m, ft, etc.
Average velocity is
t
Velocity units would be in m/s, ft/s, etc.
The instantaneous velocity is
v 
x
dt
v  lim
x

dx
28
En

gin
te
ering0
Mech

anict
s – Dynamics 28
Engineering Mechanics – Dynamics
The average acceleration is
a 
v
t
The units of acceleration would be m/s2, ft/s2, etc.
The instantaneous acceleration is
t0 t
a  lim 2
Engineering Mechanics – Dynamics 29
dt dt dt dt
v

dv

d dx

d 2
x
dt dx dt dx
a 
dv

dv dx
 v
dv
One more derivative
dt
da
 Jerk
Notice If v is a function of x, then
Engineering Mechanics – Dynamics 30
Consider the function
x  t3
 6t2
v  3t2
12t
a  6t 12
x(m)
0
16
32
2 4
t(s)
6
t(s)
Plotted
a(m/s2)
12
0
-12
-24
2 4 6
0
v(m/s)
12
-12
-24
-36
2 4
Engineering Mechanics – Dynamics 31
t(s)
6
Rectilinear Motion: Position, Velocity &
Acceleration
• Particle moving along a straight line is said
to be in rectilinear motion.
• Position coordinate of a particle is defined
by (+ or -) distance of particle from a fixed
origin on the line.
• The motion of a particle is known if the
position coordinate for particle is known for
every value of time t. Motion of the particle
may be expressed in the form of a function,
e.g., 3
x  6t2 t
or in the form of a graph x vs. t.
Engineering Mechanics – Dynamics 32
Rectilinear Motion: Position, Velocity & Acceleration
• Consider particle which occupies position P
at time t and P’at t+t,
t
Average velocity 
x
Instantaneous velocity  v  lim
x
t0 t
• Instantaneous velocity may be positive or
negative. Magnitude of velocity is referred
to as particle speed.
• From the definition of a derivative,
dt
Engineering Mechanics – Dynamics
v 
dx
12t 3t2
v  lim
x

dx
t0 t dt
e.g., x  6t2 t3
33
Rectilinear Motion: Position, Velocity & Acceleration
dt
dt2
a 
dv
12  6t
e.g. v 12t 3t2
t dt
v dv d2x
a  lim  
t0
• Consider particle with velocity v at time t and
v’at t+t,
Instantaneous acceleration a  lim
v
t0 t
• From the definition of a derivative,
Engineering Mechanics – Dynamics 34
Rectilinear Motion: Position, Velocity & Acceleration
• Consider particle with motion given by
x  6t2 t3
dt
v 
dx
12t 3t2
dv d2x
Engineering Mechanics – Dynamics
a   126t
dt dt2
• at t = 0, x = 0, v = 0, a = 12 m/s2
• at t = 2 s, x = 16 m, v = vmax = 12 m/s, a = 0
• at t = 4 s, x = xmax = 32 m, v = 0, a = -12m/s2
• at t = 6 s, x = 0, v = -36 m/s, a = -24 m/s2
35
Engineering Mechanics – Dynamics 36
DETERMINATION OF THE
MOTION OF A PARTICLE
Three common classes of motion
Engineering Mechanics – Dynamics 37

0
0
v v 
dt
dv  adt  f (t )dt
t
1. a  f (t )  dv
0
dt
f ( t )dt  dx v
t

0
0 f (t )dt
dt
dx  v 
Engineering Mechanics – Dynamics 38
t

0
0 f (t )dt
dt
dx  v 


t
t
0 0
x  x0  v0 t   f (t )dt dt


t
0
dx  v0 dt   f (t )dtdt
Engineering Mechanics – Dynamics 39


0 0
t
t
x  x0  v0t   f (t )dtdt
x

xo
f (x)dx
0
2
1 (v2
 v2
)
dt
dx
with v  then get x  x(t)
2. a  f ( x )  v
dv
Engineering Mechanics – Dynamics 40
dx
vdv adx  f ( x)dx
v t
dv
v0 0
x v
x0 v0
vdv
dx   f (v )
Both can lead to
x  x( t )
or
dt dx
Engineering Mechanics – Dynamics 41
3. a  f ( v ) 
dv
 v
dv
 f (v )
 dt  t
1/27/2017 42
UNIFORM RECTILINEAR
MOTION
v  constant
a 0
v 
dx
dt
x  x0  vdt  vt
x 
Engineeri
x
ng M
0
echani

cs – Dyn
v
amics
t 42
Engineering Mechanics – Dynamics
Also
dx
v
dv
 a
UNIFORMLY ACCELERATED
RECTILINEAR MOTION
a  constant
v  v0  at
2
o 0
x  x  v t  1 at 2
1/27/2017 43
v2
 v2
 2a( x  x )
En
0
gineering Mechanics – Dynamics 0 43
Engineering Mechanics – Dynamics
Determining the Motion of a Particle
• Recall, motion is defined if position x is known for all time t.
• If the acceleration is given, we can determine velocity and
position by two successive integrations.
• Three classes of motion may be defined for:
- acceleration given as a function of time, a = f(t)
- acceleration given as a function of position, a = f(x)
- acceleration given as a function of velocity, a = f(v)
v 
dx
a 
dv
dt dt
d2
x
dt2
a  a 
dv

dv dx
 v
dv
dt dx dt dx
14/247/2017 Engineering Mechanics – Dynamics 44
Determining the Motion of a Particle
• Acceleration given as a function of time, a = f(t):
a  f (t) 
dv
 dv
dt
v
 f (t)dt  
v0
t
dv   f (t)dt 
0
t
v  v0   f (t)dt
0
v 
dx
dt
 dx vdt
x t
 dx  vdt
x0 0
t
 x  x0 vdt
0
2 2
0
1 1
2 2
v x x
v0 x0 x0
dv
a  f (x)  v
dx
 v  v  f (x)dx
 vdv  f (x)dx  vdv   f (x)dx 
•Acceleration given as a function of position, a = f(x):
0
14/257/2017 Engineering Mechanics – Dynamics
x
x
dx
dx
dt
dx
v v
v    dt  
t
 dt
0
45
Determining the Motion of a Particle
v
dv
dt
dv
f (v)
dv
f (v)
dv
f (v)
a  f (v)   t
v
 dt  
0
t v
 dt  
0 v0
x v
14/267/2017 Engineering Mechanics – Dynamics
x0 v0 v
dv
dx
vdv
f (v)
vdv
f (v)
vdv
f (v)
a  f (v)  v  dx  dx  
v
 x  x0 
0
• Acceleration given as a function of velocity, a = f(v):
46
Summary
Procedure:
1. Establish a coordinate system & specify an origin
2. Remember: x,v,a,t are related by:
3. When integrating, either use limits (if
integration
dt dt
v 
dx
a 
dv d2
x
dt2
a  dt dx dt dx
known) or add a constant of
a 
dv

dv dx
 v
dv
14/277/2017 Engineering Mechanics – Dynamics 47
Sample Problem 1
Ball tossed with 10 m/s vertical velocity from window 20 m above ground.
Determine:
• velocity and elevation above ground at time t,
• highest elevation reached by ball and corresponding time, and
• time when ball will hit the ground and corresponding velocity.
14/287/2017 Engineering Mechanics – Dynamics 48
Sample Problem 1
dt
t
vt
v0 0
vt  v0  9.81t
dv
 a  9.81m s2
dv  9.81dt
 
 s2 
s
vt10
m
9.81
m t
2
dt
t
yt
y0 0
yt y0 10t  1 9.81t2
dy
 v 109.81t
dy  109.81tdt
2
s 
m 


m 
t  4.905 2 t


s

 

yt 20m  10
SOLUTION:
• Integrate twice to find v(t) and y(t).
14/297/2017 Engineering Mechanics – Dynamics 49
Sample Problem 1
• Solve for t at which velocity equals zero and evaluate
corresponding altitude.
s s 
 2 

vt10
m
9.81
m t  0
t 1.019s
2
2
1.019s
m
m
2 
s 




1.019s 4.905


s

 


 s 
m  m 


s

 

y  20m  10
t  4.905 2 t
yt 20m  10
y  25.1m
15/207/2017 Engineering Mechanics – Dynamics 50
Sample Problem 1
• Solve for t at which altitude equals zero and
evaluate corresponding velocity.
2

 s 
m  m 


s

 

t  4.905 2 t  0
yt 20m  10
t  1.243s meaningless
t  3.28s
s
s
 2 
 s 
 2 
 s 
v3.28s10
m
9.81
m 3.28s
vt10
m
9.81
m t
s
v  22.2
m
15/217/2017 Engineering Mechanics – Dynamics 51
What if the ball is tossed downwards with the same speed? (The
audience is thinking …)
vo= - 10 m/s
15/227/2017 Engineering Mechanics – Dynamics 52
Uniform Rectilinear Motion
Uniform rectilinear motion acceleration = 0 velocity = constant
dt
x t
dx  v dt
x0 0
x  x0  vt
x  x0 vt
dx
 v  constant
15/237/2017 Engineering Mechanics – Dynamics 53
Uniformly Accelerated Rectilinear Motion
Uniformly accelerated motion acceleration = constant
v  v  at
t

dt
v  v0  at
0
dv  a dt
0
v

v0
dv
 a  constant
2
2
0 0
0
0
dt
t
x  x0  v0t  1 at2
x  x  v t  1 at 2
v  atdt
dx  
 at
dx
 v  0
x

x0
0
0
2 2
1
2
dx
v2  v2  2ax  x 
0 0
ax  x 
v  v 
vdv  a dx
x0
v
dv
 a  constant
x

v

v0
Also:
15/247/2017 Engineering Me
c
haAnic
sp–pD
y
ln
ia
m
ci
ac
s
tion:free fall 54
Engineering Mechanics – Dynamics
MOTION OF SEVERAL PARTICLES
When independent particles move along the same
line, independent equations exist for each.
Then one should use the same origin and time.
Engineering Mechanics – Dynamics 55
Relative motion of two particles.
The relative position of B with respect to A
xB  xB  xA
A
The relative velocity of B with respect to A
vB  vB vA
A
Engineering Mechanics – Dynamics 56
The relative acceleration of B with respect to A
A
Engineering Mechanics – Dynamics 57
A
B B
a  a a
Motion of Several Particles: Relative Motion
• For particles moving along the same
line, displacements should be measured
from the same origin in the same
direction.
xB A  xB  xA  relative position of B
with respect to A
A B A
B
x  x  x
vB A  vB  vA  relative velocity of B
with respect to A
vB  vA  vBA
aB A  aB  aA  relative acceleration of B
with respect to A
15/287/2017
aB  aA  aB A
Engineering Mechanics – Dynamics 58
Engineering Mechanics – Dynamics
Engineering Mechanics – Dynamics 59
Let’s look at some dependent motions.
A
C D
E F
G
System has one degree of
freedom since only one
coordinate can be chosen
independently.
xA
xB
A B
x  2x  constant
v  2v 0
A B
a  2a 0
A B
B
Let’s look at the
relationships.
Engineering Mechanics – Dynamics 60
System has 2 degrees of
freedom.
C
A
B
xA
xC
xB
2x  2x  x  constant
A B C
A B C
2v  2v v 0
2a  2a  a 0
Let’s look at the relationships.
A
Engineering Mechanics – Dynamics
B C
61
Engineering Mechanics – Dynamics
Ball thrown vertically from 12 m
level in elevator shaft with initial
velocity of 18 m/s. At same
instant, open-platform elevator
passes 5 m level moving upward
at 2 m/s.
Determine (a) when and where
ball hits elevator and (b) relative
velocity of ball and elevator at
contact.
Sample Problem 2
16/227/2017 Engineering Mechanics – Dynamics 62
SOLUTION: Sample Problem 2
• Ball: uniformly accelerated motion
(given initial position and velocity).
• Elevator: constant velocity (given
initial position and velocity)
• Write equation for relative position of
ball with respect to elevator and solve
for zero relative position, i.e., impact.
• Substitute impact time into equation
for position of elevator and relative
velocity of ball with respect to
elevator.
16/237/2017 Engineering Mechanics – Dynamics 63
Sample Problem 3
SOLUTION:
• Ball: uniformly accelerated rectilinear motion.
2
2
2
1
0 0
s
B
B 0
s 


m  m 
t  4.905 2 t


s

 

y  y  v t  at 12m  18

 s 
v  v  at 18
m
9.81
m 
2 t
• Elevator: uniform rectilinear motion.
 
16/247/2017 Engineering Mechanics – Dynamics

s

y  y  v t  5m  2
mt
s
vE  2
m
E 0 E
64
Sample Problem 3
• Relative position of ball with respect to elevator:
yB E  1218t  4.905t2 5 2t 0
t  0.39s meaningless
t  3.65s
• Substitute impact time into equations for position of elevator
and relative velocity of ball with respect to elevator.
yE  5 23.65
yE  12.3m
vB E  18 9.81t 2
169.813.65
s
vB E  19.81
m
16/257/2017 Engineering Mechanics – Dynamics 65
Motion of Several Particles: Dependent Motion
• Position of a particle may depend on position of one
or more other particles.
• Position of block B depends on position of block A.
Since rope is of constant length, it follows that sum of
lengths of segments must be constant.
xA  2xB  constant (one degree offreedom)
• Positions of three blocks are dependent.
2xA  2xB  xC  constant (two degrees offreedom)
• For linearly related positions, similar relations hold
between velocities and accelerations.
2
dxA  2
dxB 
dxC  0 or 2vA  2vB  vC  0
dt dt dt
2
dvA  2
dvB 
dvC  0 or 2a A  2aB  aC  0
dt dt dt
16/267/2017 Engineering Mechanics – Dynamics 66
Applications
16/277/2017 Engineering Mechanics – Dynamics 67
Sample Problem 4
Pulley D is attached to a collar which is pulled down at 3 in./s. At t = 0, collarA
starts moving down from K with constant acceleration and zero initial velocity.
Knowing that velocity of collar A is 12 in./s as it passes L, determine the change
in elevation, velocity, and acceleration of block B when block A is at L.
16/287/2017 Engineering Mechanics – Dynamics 68
Sample Problem 4
SOLUTION:
• Define origin at upper horizontal surface with
positive displacement downward.
• Collar A has uniformly accelerated rectilinear
motion. Solve for acceleration and time t to reach L.
2
s
in.
in.
2
12
s

 

A
  aA  9
 2aA 8in.
A2  2aAxA  xA  
0 0
v2 v
s
16/297/2017 Engineering Mechanics – Dynamics
s2
t 1.333s
12
in.
 9
in.
t
vA  vA 0 aAt
69
Sample Problem 4

s

 
D D 0
x x   3
in.1.333s 4in.
• Pulley D has uniform rectilinear motion. Calculate
change of position at time t.
xD  xD 0 vDt
• Block B motion is dependent on motions of collar
A and pulley D. Write motion relationship and
solve for change of block B position at time t.
Total length of cable remains constant,
xA  2xD  xB  xA 0 2xD 0 xB 0
xA xA 02xD  xD 0xB xB 0 0
8in. 24in.xB  xB 0 0
xB  xB 0 16in.
17/207/2017 Engineering Mechanics – Dynamics 70
Sample Problem 4
  

s
 
s


B
12
in.  23
in.  v  0
• Differentiate motion relation twice to develop
equations for velocity and acceleration of block B.
xA  2xD  xB  constant
vA  2vD  vB  0
s
B
v  18
in.
2
9
s
aA  2aD  aB 0
 in.
 a  0
  B
 
s2
aB  9
in.
17/217/2017 Engineering Mechanics – Dynamics 71
Curvilinear Motion
http://news.yahoo.com/photos/ss/441/im:/070123/ids_photos_wl/r2207709100.jpg
17/227/2017 Engineering Mechanics – Dynamics
A particle moving along a curve other than a straight line is said
to be in curvilinear motion.
72
CURVILINEAR MOTION OF PARTICLES
POSITION VECTOR, VELOCITY, AND
ACCELERATION
x
z
y
r

r

v

 r

t
s s
P’
 s
r

P
dt
 
v

t
lim r  dr
t 0 t
dt
v 
ds
Let’s find the instantaneous velocity.
1/27/2017
73 Engineering Mechanics – Dynamics
73
Engineering Mechanics – Dynamics
P
P’
r

r

v

v
'
x
y
t
Engineering Mechanics – Dynamics 1/27/2017
74
z
a

 v

v

74
Engineering Mechanics – Dynamics
P
P’
r

r

dt

v

v
'
x
y
x
z
y
t
a

 v


v
a  lim v  dv


t 0 t
Note that the
acceleration is not
necessarily along the
direction of
the velocity.
Engineering Mechanics – Dynamics 1/27/2017
75
z 75
Engineering Mechanics – Dynamics
DERIVATIVES OF VECTOR
FUNCTIONS
du
dP  lim P


u0 u 

u
 lim
P(u  u ) P(u )

u0


 
du

du

du

 
d( P  Q )  dP  dQ
 f dP

df P
du

d( fP )
du

1/27/2017
76 Engineering Mech
d
aniu
cs – Dynamics
76
Engineering Mechanics – Dynamics
du
 
du


du


d( PQ )  dP Q P dQ

du du

 
du
 
d( PQ )  dP Q  P dQ
dP
ˆ
dPx
du
 ˆj  z
kˆ
du
Engineering Mechanics – Dynamics 1/27/2017
77
du
dPy
i 
dP
du

77
Engineering Mechanics – Dynamics
Engineering Mechanics – Dynamics 1/27/2017
78
Rate of Change of a Vector

P  P
ˆi P
ˆj P
kˆ
x y z
The rate of change of a vector is the
same with respect to a fixed frame and
with respect to a frame in translation.
78
Engineering Mechanics – Dynamics
RECTANGULAR COMPONENTS OF
VELOCITY AND ACCELERATION
r

 xˆi yˆj zkˆ
v

 xˆi yˆj zkˆ
a

 xiˆyˆjzkˆ
1/27/2017 79
Engineering Mechanics – Dynamics 79
Engineering Mechanics – Dynamics
x
y
r

yˆ
j
xî
x
z
y
P
v

v ˆi
x
v ˆj
y
v kˆ
z
a

1/27/2017
zk̂
80
z
Engineering Mechanics – Dynamics
80
Engineering Mechanics – Dynamics
z
y
a ˆj
y
ˆ
a k
z
a ˆi
x
x
a

1/27/2017
81 Engineering Mechanics – Dynamics
81
Engineering Mechanics – Dynamics
Velocity Components in Projectile Motion
ax
 
x
 0
vx
 x
  vxo
Engineering Mechanics – Dynamics 82
xo
x  v t
a  z0
z
v  z v 0
z zo
z  0 1
2
yo
a  y g
y
v  y v  gt
y yo
y  v t  gt2
x
z
y
x’
z’
y’
O
A
B
r

 r

 r

B A B /A
MOTION RELATIVE TO A FRAME IN
TRANSLATION
Engineering Mechanics – Dynamics 83
B
r
 B / A
r

A
r

Engineering Mechanics – Dynamics 84
B A B / A
r

 r

r

r

  r

  r


B A B / A
v

 v

v

B A B / A
v

  v

 v


B A B / A
B / A
a

 a

a

B A
Engineering Mechanics – Dynamics 85

r


 
r



r


B A B / A
A B / A
a

B
 a

a

Velocity is tangent to the path of a particle.
Acceleration is not necessarily in the same direction.
It is often convenient to express the acceleration in
terms of components tangent and normal to the path
of the particle.
TANGENTIAL AND NORMAL
COMPONENTS
Engineering Mechanics – Dynamics 86
O x
y
t
v

 veˆ
t
Engineering Mechanics – Dynamics 87
ê
t
Plane Motion of a Particle
ê'
t
ê

e
ˆn
n
ê' P’
P
lim
êt
 0  
n  0
 ê lim
êt



lim  2sin 2
 e
ˆn 0 

t
e
ˆ 
deˆ
n
ˆ
 e






 ê lim
n
 2
sin 2
0
t
ê
t
ê'
eˆ
t

1/27/2017 88
Engineerin
n
g Mechan
d
ics

– Dynamics 88
Engineering Mechanics – Dynamics

d
t
n
e
ˆ 
deˆ
v

 veˆ
t
t
e
ˆ
 dv dv
dt dt
a  
dt
Engineering Mechanics – Dynamics 89
ˆ
d
e t
 v
n

O x
y
e
ˆt
t
ê'
P
 P’
 s
s  
s ds
d

  lim
0 
t
ˆ
dt
 dv
dt
ˆ
d
e
v t
a  e 
v

v
e
ˆ
dt d ds dt d 
deˆt

deˆt d ds

deˆt
a


dv ˆ
v2
ˆ
Engineering Mechanics – Dynamics 90
e  e
dt t  n
a


dv ˆ
v2
ˆ
e  e
dt t  n
a

 a e
ˆ  a e
ˆ
t t n n
dv
at 
dt
v2
an  
Discuss changing radius of curvature for highway cur
Engineering Mechanics – Dynamics 91
Motion of a Particle in Space
The equations are the same.
O x
y
t
ê
t
ê'
n
ê
n
ê' P’
P
z
Engineering Mechanics – Dynamics 92
RADIAL AND TRANSVERSE
COMPONENTS
x
y
P
r
Engineering Mechanics – Dynamics 93
ê
Plane Motion
ê
r


êr
 êr
eˆr
ê
ê
eˆ


dêr
d
 e
ˆ r
 eˆ
dê
d
dt d dt
deˆr

deˆr

d  e
ˆ
dt d dt
Engineering Mechanics – Dynamics 94
deˆ

deˆ
r
d
  e
ˆ
vr  r v  r

v


dr
dt dt
Engineering Mechanics – Dynamics 95
r r r

d
( reˆ )  reˆ  r
eˆ
v

 reˆr
 reˆ
 vr eˆrveˆ
y
r
ê
ê
r


x
eˆr ˆicos  ˆjsin

deˆr
d
 ˆisin   ˆjcos  e
ˆ
r
 ˆicos  ˆjsin  eˆ
dê
d

Engineering Mechanics – Dynamics 96
v

 reˆr
 reˆ
a

 reˆr  reˆr  reˆ  reˆ reˆ
a

 
rêr  r

 ê  r

ê  r
ê r
 êr
2
a

 ( rr2
)eˆ (r 2r)eˆ
r 
dt
dvr
r
a 
dt
Engineering Mechanics – Dynamics 97
a

dv
2
r



r r
a  
a  r 2r
Note
Extension to the Motion of a Particle in Space:
Cylindrical Coordinates
r

 Reˆ  zkˆ
r
v

 R
eˆ  Reˆ  zkˆ
R 
a

 (R

 R2
)eˆ  (R2R)eˆ 
z

k
ˆ
R 
Engineering Mechanics – Dynamics 98
Curvilinear Motion: Position, Velocity & Acceleration
• Position vector of a particle at time t is defined by a
vector between origin O of a fixed reference frameand
the position occupied by particle.
• Consider particle which occupies position Pdefined
by r at time t and P’defined by r
at t + t,

dr
t0 t dt
 
v lim
r
 instantaneous velocity (vector)
v  lim
s

ds
t0 t dt
 instantaneous speed (scalar)
19/297/2017 E
ng
in
e
e
r
iVng
eMloe
c
cha
in
tyic
si–
sDty
an
a
nm
gi
c
esnt to path 99
Engineering Mechanics – Dynamics
Curvilinear Motion: Position, Velocity & Acceleration

dv
 
t0 t dt
a lim
v
• Consider velocity v
of particle at time t and velocity
vat t + t,
 instantaneous acceleration(vector)
• In general, acceleration vector is not tangent to
particle path and velocity vector.
1
1
/2070/20
17
Engineering Mechanics – Dynamics 10
0
Rectangular Components of Velocity & Acceleration

• Position vector of particle P given by its
rectangular components:
r xi

 y

j zk
• Velocity vector,
zk
k
dt dt dt
z

 vx i

 v y

jv k
v
dx
i


dy 
j
dz 
 xi

 y

j 

• Acceleration vector,
z
1
1
/2071/20
17
Engineering Mechanics – Dynamics


 
 ax i

 a y

j ak
a  i  j  k  xi yj  zk
dt2 dt2 dt2
 d 2x d 2y d2z
10
1
   
0 0
x y
x0  y0  z0  0 v  v  given
Rectangular Components of Velocity & Acceleration
• Rectangular components are useful when
acceleration components can be integrated
independently, ex: motion of a projectile.
ax  x 0 ay  y g az  z 0
with initial conditions,
Therefore:
• Motion in horizontal direction is uniform.
• Motion in vertical direction is uniformly accelerated.
• Motion of projectile could be replaced by two
independent rectilinear motions.
1
1
/2072/20
17
Engineering Mechanics – Dynamics
 
0 0
2
0 0
1
2
x y
vx  vx  vy  vy  gt
x  v  t y  v t  gt
10
2
x
v  v0  at
0 0 2
x  x  v t  1 at2
 
1
1
/2073/20
17
Engineering Mechanics – Dynamics
2 2
0 0
v  v  2a x x
Example
A projectile is fired from the edge of a 150-m cliff with an initial
velocity of 180 m/s at an angle of 30° with the horizontal. Find (a)the
range, and (b) maximum height.
y
Remember:
10
3
Example
Car A is traveling at a constant speed of 36 km/h. As A crosses
intersection, B starts from rest 35 m north of intersection and moves
with a constant acceleration of 1.2 m/s2. Determine the speed, velocity
and acceleration of B relative to A 5 seconds after A crosses
intersection.
1
1
/2074/20
17
Engineering Mechanics – Dynamics 10
4
Tangential and Normal Components
• Velocity vector of particle is tangent to path of
particle. In general, acceleration vector is not.
Wish to express acceleration vector in terms of
tangential and normal components.
•
particle path at P and P’.
respect to the same origin,
t t
e and e are tangential unit vectors for the
When drawn with
det  et et
et et  det
det d
From geometry:
t n
de  de
n
det
d
 e
d
det
1
1
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Engineering Mechanics – Dynamics 10
5
106
t n t n
dv
dt
dv v2
dt 
v2

a  e  e a  a 
Tangential and Normal Components
t
• With the velocity vector expressed as v ve
t t
dt dt dt dt
the particle acceleration may be written as
d ds
d ds dt
a 
dv

dv
e  v
det

dv
e  v
det
ds
dt
n  v
 d  ds
d
t  e
but
de

After substituting,
• Tangential component of acceleration reflects
1/27/2017
change of speed and normal component reflects
change of direction.
• Tangential component may be positive or
negative. Normal component always points
toward center of path curvature.
Engineering Mechanics – Dynamics 10
6
Engineering Mechanics – Dynamics
r  rer
Radial and Transverse Components
• If particle position is given in polar coordinates, wecan
express velocity and acceleration with components
parallel and perpendicular to OP.

de

de


d
d
  er
r  e
dt d  dt
 e
r  r
dt
dt d
de de d d
dt
d 
d
dt
de
 de

 er
  
  r
r r
d dr de
dt dt dt
v  re  e  r
• Particle velocity vector:
 
r
• Similarly, particle acceleration:
d
dt
de
dt dt
r 

 
d d
dt
a  re  r e
 re  r
der
 re e 
 r r
 rer  re
dt
 r e r erer
r

 re

r
• Particle position vector:
r
dt dt
 r 
v 
dr
e  r
d e  re  re
   
2
r 
a  r  r e  r  2r e
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7
Engineering Mechanics – Dynamics
Sample Problem
A motorist is traveling on curved section of highway at 60 mph. Themotorist
applies brakes causing a constant deceleration.
Knowing that after 8 s the speed has been reduced to 45 mph, determinethe
acceleration of the automobile immediately after the brakes are applied.
1
1
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17
Engineering Mechanics – Dynamics 10
8
Sample Problem
60 mph  88ft/s
45mph  66ft/s
ft
2500ft
s2
8s
88 ft s2
 3.10
s2
v2
t
SOLUTION:
• Calculate tangential and normal components of
acceleration.
a 
v

66  88ft s
 2.75
ft
an 


t
• Determine acceleration magnitude and direction
with respect to tangent to curve.
a  a2  a2   2.752  3.102
t n s2
a  4.14
ft
  tan 1 an  tan 13.10
at 2.75
  48.4
1
1
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Engineering Mechanics – Dynamics 10
9
Sample Problem
Determine the minimum radius of curvature of the trajectory
described by the projectile.
v2
an 

Recall:
2
 
v
an
Minimum r, occurs for small v and large an
155.92
9.81
   2480m
v is min and an ismax
an
a
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0
Sample Problem
Rotation of the arm about O is defined by  = 0.15t2 where  is in radians and
t in seconds. Collar B slides along the arm such that r = 0.9 - 0.12t2 where r
is in meters.
After the arm has rotated through 30o, determine (a) the total velocity of the
collar, (b) the total acceleration of the collar, and (c) the relative acceleration
of the collar with respect to the arm.
11/1217/2017 Engineering Mechanics – Dynamics 11
1
Sample Problem
SOLUTION:
• Evaluate time t for  = 30o.
  0.15t 2
 30  0.524rad t 1.869s
• Evaluate radial and angular positions, and first
and second derivatives at time t.
r  0.9 0.12t2  0.481m
r 0.24 t  0.449 ms
r 0.24 m s2
  0.15t 2 0.524rad
 0.30 t  0.561rad s
 0.30 rad s2
1
1
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Engineering Mechanics – Dynamics 11
2
Sample Problem
  tan1 v
vr
v  v2  v2
r 
• Calculate velocity and acceleration.
vr  r 0.449 m s
v r 0.481m0.561rad s  0.270 ms
v  0.524m s   31.0
  tan1a
ar
a  a2  a2
r 
ar  rr2
 0.240 m s2  0.481m0.561rads2
 0.391m s2
a r2r
 0.481m0.3rad s2 2 0.449 m s0.561rad s
 0.359 m s2
a  0.531m s  42.6
1
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Engineering Mechanics – Dynamics 11
3
Sample Problem
• Evaluate acceleration with respect to arm.
Motion of collar with respect to arm is rectilinear
and defined by coordinate r.
aB OA  r 0.240 m s2
1
1
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Engineering Mechanics – Dynamics 11
4
UNIT-II
KINETICS OF PARTICLE
Introduction, definitions of matter, body, particle, mass, weight, inertia,
momentum, Newton’s law of motion, relation between force and mass,
motion of a particle in rectangular coordinates, D’Alembert’s principle,
motion of lift, motion of body on an inclined plane, motion of
connected bodies.
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Engineering Mechanics – Dynamics
11
5
Engineering Mechanics – Dynamics
Newton’s Second Law of Motion
• If the resultant force acting on a particle is not
zero, the particle will have an acceleration
proportional to the magnitude of resultant and in
the direction of the resultant.
F  ma
• If particle is subjected to several forces:
F  ma
• We must use a Newtonian frame of reference, i.e., one that is not
accelerating or rotating.
• If no force acts on particle, particle will not accelerate, i.e., it will
remain stationary or continue on a straight line at constant velocity.
Engineering Mechanics – Dynamics 116
11
6
Linear Momentum of a Particle
dt

d
mv 
d
L
dt dt
F  ma  m
dv
L mv Linear momentum
F  L
Sum of forces = rate of change of linear momentum
If F  0 linear momentum is constant
Principle of conservation of linear momentum
Engineering Mechanics – Dynamics 117
11
7
Equations of Motion
• Newton’s second law


F  m
a

• Convenient to resolve into components:
x y z
z

 

a i  a j  a k
 Fz maz
 Fz mz
 Fy  may
 Fy  my
 Fx  max
 Fx  mx
Fxi

 Fy

j  F k  m
• For tangential and normal components:
t
dv v2
dt
F  m
F t mat

F n man
F n  m

Engineering Mechanics – Dynamics 118
11
8
Dynamic Equilibrium
ma
• Alternate expression of Newton’s law:
F  ma  0
• If we include inertia vector, the system of
forces acting on particle is equivalent to zero.
The particle is said to be in dynamic
equilibrium.
• Inertia vectors are often called inertia
forces as they measure the resistance that
particles offer to changes in motion.
inertia vector
Engineering Mechanics – Dynamics 119
11
9
Sample Problem 1
An 80-kg block rests on a horizontal plane. Find the
magnitude of the force P required to give the block an
acceleration of 2.5 m/s2 to the right. The coefficient of
kinetic friction between the block and plane is mk =
0.25.
Engineering Mechanics – Dynamics 120
SOLUTION:
• Draw a free body diagram
• Apply Newton’s law. Resolve
into rectangular components
12
0
W  mg  809.81 785N
F  k N  0.25N
Sample Problem 12.2
Fx  ma:
Pcos30  0.25N  802.5
 200
Fy  0:
N  Psin30  785
Pcos30  0.25Psin30  785 200
Pcos30
Psin30
N  Psin30  785  0
Solve for P and N
12N
1
P  534.7 N
N 1052.4
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1
Engineering Mechanics – Dynamics
122
Sample Problem 12.3
The two blocks shown start from rest. The
horizontal plane and the pulley are
frictionless, and the pulley is assumed to be
of negligible mass. Determine the
acceleration of each block and the tension in
the1
/
c2
7
o/
2
r0
1
d7
. Engineering Mechanics – Dynamics 12
2
Engineering Mechanics – Dynamics
Fx  mAaA
Fy  mBaB
O
x
y
Sample Problem 2
• Kinematic relationship: If A moves xAto
the right, B moves down 0.5 xA
1
1
B 2 A B 2 A
x  x a  a
Draw free body diagrams & apply Newton’s law:
Fy  mCaC
2940-300aB  2T1  0
T1  100aA
mB g  T2 mBaB
3009.81T2  300aB
T2  2940-300aB
T2  2T1  0
2940-300aB  200aA  0
2940-300aB  2 200aB  0
B
a  4.2 m/ s2
A
a  8.4 m/s2
T1 840 N
Engineering Mechanics – Dynamics 123
T2 1680 N
12
3
Sample Problem 3
The 12-lb block B starts from rest and slides on
the 30-lb wedge A, which is supported by a
horizontal surface.
Neglecting friction, determine (a) the acceleration
of the wedge, and (b) the acceleration of the
block relative to the wedge.
Engineering Mechanics – Dynamics 124
Block
Wedge
12
4
125
N1
WBcosq
WBsinq
N1
aBn
aBt WB
1
N cosq
WB sin  mBaBt
32.2
Bt Bt
120.5 
12
a  a 16.1 ft / s2
aA
1
32.2
A
0.5N 
30
a
N1 sin  mAaA
N1 cos WA N2
N1 WB cos  mBaBn
But aBn  aA sin Same normal acceleration (to maintain contact)
N1 WB cos  mBaA sin 1
32.2
A
N 10.39  
120.5
a
a 5.08 ft / s2
a  2.54 ft /s2
Draw free body diagrams for block & wedge
N1sinq
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2017 EngineerBinngMechanics – Dynamics 12
5
Engineering Mechanics – Dynamics
N1
aBn
aBt WBcosq
WBsinq
N1
WB
1
N cosq
N1sinq
Bx Bt Bn
a  a cos  a
aA
By Bt Bn
a  a sin  a
sin  12.67 ft /s2
cos  10.25 ft /s2
aB / A  aB  aA
aB / A  12.67i 10.25 j  5.08i
 17.75i 10.25 j
30°
20.5
Engineering Mechanics – Dynamics 126
12
6
Sample Problem 4
The bob of a 2-m pendulum describes an arc of a circle in a
vertical plane. If the tension in the cord is 2.5 times the weight of
the bob for the position shown, find the velocity and acceleration
of the bob in that position.
Engineering Mechanics – Dynamics 127
12
7
Sample Problem 5
Resolve into tangential and normal components:
 Ft  mat :
at  g sin 30
mg sin30  mat
at  4.9 m s2
 Fn  man : 2.5mg  mg cos30  man
an  g2.5  cos30
an  16.03m s2
• Solve for velocity in terms of normalacceleration.
2
an  2 m 16.03m s

v2
an v    

v  5.66 ms
mgsin30
Engineering Mechanics – Dynamics 128
mgcos30
12
8
Sample Problem 6
Determine the rated speed of a
highway curve of radius  = 400 ft
banked through an angle  = 18o. The
rated speed of a banked highway curve
is the speed at which a car should
travel if no lateral friction force is to
be exerted at its wheels.
Engineering Mechanics – Dynamics 129
SOLUTION:
• The car travels in a horizontal circular
path with a normal component of
acceleration directed toward the center
of the path.The forces acting on the car
are its weight and a normal reaction
from the road surface.
• Resolve the equation of motion for
the car into vertical and normal
components.
• Solve for the vehicle speed.
12
9
Sample Problem 7
SOLUTION:
• The car travels in a horizontal circular
path with a normal component of
acceleration directed toward the center
of the path.The forces acting on the
car are its weight and a normal
reaction from the road surface.
• Resolve the equation of motion for
the car into vertical and normal
components.
 Fy  0:
W
cos
R 
R cos W  0
 Fn  man :
W v2
g 
W
cos
g
sin 
R sin 
W
an
• Solve for the vehicle speed.
v2  gtan
 32.2ft s2 400fttan18
v  64.7 ft s  44.1mi h
Engineering Mechanics – Dynamics 130
13
0
Derivative of angular momentum with respect to time:
HO  r  mv  r  mv  v  mv  r  ma
 r F
 MO
Sum of moments about O = rate of change of angular momentum
L mv
Angular Momentum
From before, linear momentum:
Now angular momentum is defined as the moment of momentum
HO  r  mv
HO is a vector perpendicular to the plane
containing r and mv
Resolving into radial & transverse components:
2
O 
H  mv r  mr 
about O
Moment of F
Engineering Mechanics – Dynamics 131
13
1
Equations of Motion in Radial & Transverse Components
F  ma  mr2r
Engineering Mechanics – Dynamics 132
Fr  mar  mr r2
13
2
Central Force
When force acting on particle is directed
toward or away from a fixed point O, the
particle is said to be moving under a central
force.
O = center of force
Since line of action of the central force passes through O:
MO  HO  0
r  mv HO  constant
Engineering Mechanics – Dynamics 133
13
3
Sample Problem 8
A block B of mass m can slide freely on
a frictionless arm OA which rotates in a
horizontal plane at a constant rate0.
Engineering Mechanics – Dynamics 134
Knowing that B is released at a distance
r0 from O, express as a function ofr
a) the component vr of the velocity ofB
along OA, and
b) the magnitude of the horizontal force
exerted on B by the arm OA.
SOLUTION:
• Write the radial and transverse
equations of motion for the block.
• Integrate the radial equation to find an
expression for the radial velocity.
• Substitute known information into the
transverse equation to find an
expression for the force on the block.
13
4
Sample Problem 8
Write radial and transverse equationsof
motion:
r r
F  m a
F   m a
r vr 
dvr 
dvr dr
 vr
dvr
 
2 2 2 2
0
r 0
v  r r
 
1 2
2 2 2
0 0
F  2m r  r
0  mr  r2

F  mr  2r 
r  r2
dt dr dt dr
But vr r
2 r
r
dv
dr
r  v 2
r r
r dr  v dv
r
o
r 2
dr
vr dvr 
vr

0

ro
 
1 2
2 2
0
r 0
v  r  r
Engineering Mechanics – Dynamics 135
13
5
UNIT-III
IMPULSE AND
MOMENTUM,VIRTUAL
WORK
Impulse and momentum: Introduction; Impact, momentum, impulse,
impulsive forces, units, law of conservation of momentum, Newton’s
law of collision of elastic bodies.
Coefficient of restitution, recoil of gun, impulse momentum
equation; Virtual work: Introduction, principle of virtual work,
applications, beams, lifting machines, simple framed structures.
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13
6
Engineering Mechanics – Dynamics
Impulse = Momentum
Consider Newton’s 2nd
Law and the
definition of
acceleration
Ns
Kg x m/s
Momentum is defined as “Inertia in Motion”
Units of Impulse:
Units of Momentum:
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Engineering Mechanics – Dynamics 13
7
Engineering Mechanics – Dynamics
Impulse – Momentum Theorem
Ft  mv
IMPULSE CHANGE IN MOMENTUM
This theorem reveals
some interesting
relationships such as the
INVERSE relationship
t
Engineering Mechanics – Dynamics 138
TIMF
E
between F
O
R
mC
E
a
vn
d

Impulse – Momentum Relationships
Engineering Mechanics – Dynamics 139
Impulse – Momentum Relationships
fT mV
Constant
Since TIME is directly related
to the VELOCITY when the
force and mass are constant,
the LONGER the cannonball is
in the barrel the greater the
velocity.
Also, you could say that the
force acts over a larger
ent, thus there is
1/27/2017 140
Engineering Me
c
h
da
n
iic
ss
p
–D
lay
n
ca
m
ei
c
ms 14
0
Engineering Mechanics – Dynamics
How about a collision?
Consider 2 objects speeding
toward each other. When they
collide......
Due to Newton’s 3rd Law the
FORCE they exert on each
other are EQUAL and
OPPOSITE.
The TIMES of impact are also
equal.
Therefore, the IMPULSES of the 2
objects colliding are also
EQUAL
2
1
J1  J2
(Ft)  (Ft)
t1  t2
F1 F2
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Engineering Mechanics – Dynamics 14
1
Engineering Mechanics – Dynamics
How about a collision?
If the Impulses are
equal then the
also equal!
1 J2
m1v1m2v2
m1(v1 vo1)  m2 (v2 vo2 )
m1v1  m1vo1  m2v2 m2vo2
p1 p2
J 
M

OMENTUMSare
 pbefore
 pafter
m1vo1  m2vo2  m1v1m2v2
Engineering Mechanics – Dynamics 142
Momentum is conserved!
The Law of Conservation of Momentum: “In the
absence of an external force (gravity, friction), the
total momentum before the collision is equal to
the total momentum after the collision.”
po(truck)  mvo  (500)(5)  2500kg*m / s
po(car)  (400)(2)  800kg*m / s
po(total)  3300kg*m / s
ptruck  500*3 1500kg*m / s
pcar  400*4.5 1800kg*m / s
ptotal  3300kg*m / s
Engineering Mechanics – Dynamics 143
Types of Collisions
A situation where the objects DO NOT STICK is
one type of collision
Notice that in EACH case, you have TWO objects BEFORE
and AFTER the collision.
Engineering Mechanics – Dynamics 144
A “no stick” type collision
pbefore = pafter
m1vo1  m2vo2  m1v1 m2v2
(1000)(20)  0  (1000)(v1)  (3000)(10)
10000 1000v1
v1  -10 m/s
Engineering Mechanics – Dynamics 145
Types of Collisions
Another type of collision is one where the
objects “STICK” together. Notice you have
TWO objects before the collision and ONE
object after the collision.
Engineering Mechanics – Dynamics 146
A “stick” type of collision
20000  4000vT
vT 
Engineering Mechanics – Dynamics 147
pbefore = pafter
m1vo1  m2vo2  mTvT
(1000)(20)  0  (4000)vT
5 m/s
The “explosion” type
This type is often referred to
as “backwards inelastic”.
Notice you have ONE object
( we treat this as a SYSTEM)
before the explosion and
TWO objects after the
explosion.
Engineering Mechanics – Dynamics 148
Backwards Inelastic - Explosions
0  3 4v2
v2 
Engineering Mechanics – Dynamics 149
Suppose we have a 4-kg rifle
loaded with a 0.010 kg bullet.
When the rifle is fired the
bullet exits the barrel with a
velocity of 300 m/s. How fast
does the gun RECOIL
backwards?
pbefore = pafter
mTvT  m1v1 m2v2
(4.010)(0)  (0.010)(300)  (4)(v2 )
-0.75 m/s
Collision Summary
m1v01  m2v02  m1v1m2v2
m1v01  m2v02  mtotalvtotal
mtotalvo(total)  m1v1  m2v2
Sometimes objects stick together or blow
apart. In this case, momentum is ALWAYS
conserved.
 pbefore
 pafter
When 2 objects collide and DON’
When 2 objects collide and stick to
When 1 object breaks into 2 objec
Engineering Mechanics – Dynamics 150
Elastic Collision = Kinetic Energy is Conserved
Inelastic Collision = Kinetic Energy is NOT Conserved
Elastic Collision
KEcar (Before)  1
2 mv  0.5(1000)(20)  200,000J
2 2
KEtruck (After )  0.5(3000)(10) 150,000J
2
KEcar (After )  0.5(1000)(10)  50,000J
2
Since KINETIC ENERGY is conserved during the collision
we call this an ELASTIC COLLISION.
Engineering Mechanics – Dynamics 151
Inelastic Collision
KEcar (Before)  1
2 mv  0.5(1000)(20)  200,000J
2 2
KEtruck/car (After)  0.5(4000)(5)  50,000J
2
Since KINETIC ENERGY was NOT conserved during the
collision we call this an INELASTIC COLLISION.
Engineering Mechanics – Dynamics 152
Examp
Gl
ra
e
nny (m=80 kg) whizzes
around the rink with a velocity
of 6 m/s. She suddenly collides
with Ambrose (m=40 kg) who
is at rest directly in her path.
Rather than knock him over,
she picks him up and
continues in motion without
"braking." Determine the
velocity of Granny and
Ambrose.
How many objects do I have before the collision?
Engineering Mechanics – Dynamics 153
2  
b a
vT 
p  p
m1vo1  m2vo2  mTvT
How many objec1tsdo I have after the c
(o
8l
l
i
0s
i
)o
(n
6?)  (40)(0) 120vT
4 m/s
Collisions in 2 Dimensions
The figure to the left shows a
collision between two pucks
on an air hockey table. Puck A
has a mass of 0.025-kg and is
moving along the x-axis with a
velocity of +5.5 m/s. It makes
a collision with puck B, which
has a mass of 0.050-kg and is
initially at rest. The collision is
NOT head on. After the
collision, the two pucks fly
vA
Engineering Mechanics – Dynamics 154
A
v sin
vAcos
vBcos
vB
vBsin apart with angles shown in
the drawing. Calculate the
speeds of the pucks after the
collision.
Collisions in 2 dimensions
 pox  px
mAvoxA  mBvoxB  mAvxA  mBvxB
(0.025)(5.5) 0  (.025)(vA cos65) (.050)(vB cos37)
vA
vB
vAcos
A
v sin
B
v cos
B
v sin
0  (0.025)(vA sin 65)  (0.050)(vB sin37)
0.0300vB 0.0227vA
vB  0.757vA
0  mAvyA  mBvyB
0.1375  0.0106vA 0.040vB
 poy  py
Engineering Mechanics – Dynamics 155
Collisions in 2 dimensions
0.1375  0.0106vA 0.040vB
vB  0
vB.
7
0.7
5
577
(2.8
v
4)
A
 2.15m/ s
0.1375  0.0106vA (0.050)(0.757vA )
0.1375  0.0106vA  0.03785vA
0.1375  0.04845vA
vA  2.84m / s
1/27/2017
156 Engineering Mechanics – Dynamics
15
6
Engineering Mechanics – Dynamics
WORK ENERGY
METHOD
UNIT
-IV
1/27/2017 Engineering Mechanics – Dynamics 157
Work energy method: Law of conservation of energy,
application of work energy, method to particle motion
and connected system, work energy applied toconnected
systems, work energy applied to fixed axis rotation.
15
7
Engineering Mechanics – Dynamics
Law of Conservation of Energy
• What you put in is
what you get out
• Total energy is
conserved
15
8
Engineering Mechanics – Dynamics
Practical Applications
 Gasoline converts to energy which moves
the car
 A battery converts stored chemical
energy to electrical energy
 Dams convert the kinetic energy of falling
water into electrical energy
15
9
Engineering Mechanics – Dynamics
CanYouThink of Other Examples?
16
0
Engineering Mechanics – Dynamics
Conservation of Mechanical Energy
1
mv2
 mgh  E
2
Total
Energy
Potential
Energy
Kinetic
Energy
m = mass
v = velocity
g = gravitational acceleration
h = height
ILYA,did you
know thateven
though it wasa
bumpy ride,
our energy
remained
constant!
16
1
Engineering Mechanics – Dynamics
Example of Conservation of
Mechanical Energy
2
1
m v 2
 m g h  E
Constant
16
2
Engineering Mechanics – Dynamics
An Example
16
3
Engineering Mechanics – Dynamics
Another Example
16
4
Engineering Mechanics – Dynamics
Yet Another Example
16
5
Engineering Mechanics – Dynamics
Last Example
16
6
Engineering Mechanics – Dynamics
MECHANICAL
VIBRATIONS
UNIT
-V
1/27/2017 Engineering Mechanics – Dynamics 167
Definitions and concepts, simple harmonic
motion, free vibrations, simple and compound
pendulum, torsion pendulum, free vibrations
without damping, general cases.
16
7
Engineering Mechanics – Dynamics
Simple Harmonic Motion
• Harmonic Motion is any motion that repeats itself.
• Examples of Harmonic Motion.
Engineering Mechanics – Dynamics 168
Engineering Mechanics – Dynamics 169
Engineering Mechanics – Dynamics 170
Engineering Mechanics – Dynamics 171
Engineering Mechanics – Dynamics 172
Engineering Mechanics – Dynamics 173
Period
Displacement
Time for one oscillation
Frequency Number of oscillations in
one second
Amplitude Maximum displacement
Distance from equilibrium
• Simple harmonic motion is a special type of harmonic
motion.
• Consider a mass on a spring.
• The cart is in equilibrium, because the total force is
zero.
• The acceleration is also
(this doesn’t meazneriots.stationary)
Engineering Mechanics – Dynamics 174
Lets look at the forces
force
dispt = -A
Engineering Mechanics – Dynamics 175
force
dispt = -A/2
Engineering Mechanics – Dynamics 176
Force = 0
dispt = 0
Engineering Mechanics – Dynamics 177
force
dispt = A/2
Engineering Mechanics – Dynamics 178
force
dispt = A
Engineering Mechanics – Dynamics 179
force
dispt = A
• Notice that as the displacement increases, the
restoring force increases.
• Notice that the restoring force is always in the
opposite direction to the displacement
Engineering Mechanics – Dynamics 180
Now we’ll look at the acceleration
dispt = -A
acceleration
force
Engineering Mechanics – Dynamics 181
dispt = -A/2
acceleration
force
Engineering Mechanics – Dynamics 182
Force = 0
dispt = 0
Engineering Mechanics – Dynamics 183
Acceleration =0
dispt = A/2
acceleration
force
Engineering Mechanics – Dynamics 184
dispt = A
acceleration
force
Engineering Mechanics – Dynamics 185
acceleration
dispt = A
• Notice that as the displacement increases, the
acceleration increases.
• Notice that the acceleration is always in the
opposite direction to the displacement
Engineering Mechanics – Dynamics 186
Engineering Mechanics – Dynamics 187
• The relation between acceleration and
displacement is …..
• Acceleration is proportional to displacement
• Acceleration is in opposite direction to
displacement.
a   constant  y
a   2
 y T
 
2
Acceleration/position graph
acceleration
Engineering Mechanics – Dynamics 188
position
Acceleration/position graph
acceleration
Engineering Mechanics – Dynamics 189
position
y  mx  c
a  mx
a 2
x
Force/position graph
force
Engineering Mechanics – Dynamics 190
position
a 2
x
F  ma  (m2
)x
Engineering Mechanics – Dynamics 191
Graphs of SHM
• We have looked at simple harmonic motion as
a function of position.
• Now we’ll look at it as a function of time
• raphs
Engineering Mechanics – Dynamics 192
graphical treatment
1/27/2017 Engineering Mechanics – Dynamics
19
3
Engineering Mechanics – Dynamics
•
Engineering Mechanics – Dynamics 194
Engineering Mechanics – Dynamics 195
•
Reference Circle
Engineering Mechanics – Dynamics 196
Reference Circle
Red ball moves in SHM horizontally
Blue ball moves in a circle
Both have same period
Amplitude of SHM equals
radius of circle
Both have same horizontal
displacement
Engineering Mechanics – Dynamics 197
Tofind the position of a swing at a certain time.
The period is 4.0s
The amplitude is 2.0m
Where is the swing 2.0s after release?
Engineering Mechanics – Dynamics 198
The period is 4.0s
The amplitude is 2.0m
Where is the swing 1.0s after release?
Engineering Mechanics – Dynamics 199
Where is the swing 0.5s after release?
4.0
Convert time to angle (1period = 360o)
0.5
3600
 450
450
2.0m
x
2
x
cos450

0.50s  450
Engineering Mechanics – Dynamics 200
Where is the swing 2.5s after release?
Convert time to angle (1period = 360o)
4.0
2.5
3600
 2250
450
2.0m
x
2
cos450

x
2.50s  2250
Engineering Mechanics – Dynamics 201
How long does it take to go 1.4m from the start?
(1) Calculate angle
(2) Convert angle to time
(1period = 360o)
 
600
2.0m
2
cos 
0.59
600

60
of a period
360
600
 1
6  4.0s
1.41m 0.59m
Engineering Mechanics – Dynamics 202
• The top of the sky tower is oscillating with an
amplitude of 2.0 m and a period of 14 s.
• How long is it more than 0.80m from equilibrium each
cycle?
• What is the horizontal acceleration when the
displacement is maximum?
Engineering Mechanics – Dynamics 203
Equations 1
y  Asin   t
y  Asint
v  Acost
a  A2
sint
Engineering Mechanics – Dynamics 204
Equations 2
y  Acost
v  Asint
a  A2
cost
Engineering Mechanics – Dynamics 205
Equations 3
y  Acost
v  Asint
a  A2
cost
Engineering Mechanics – Dynamics 206
Engineering Mechanics – Dynamics 207
y  Asint
v  Acost
a  A2
sint
ymax  A
vmax  A
max
a  A2
a  2
Asint  2
y
a  2
y
Anisha is on a swing. Kate pulls her back 2.0m and lets her go. Her
period is 4.0s.
(a) Calculate her maximum speed. (where is it?)
(b) Calculate her maximum acceleration. (where is it?)
Engineering Mechanics – Dynamics 208
Anisha is on a swing. Kate pulls her back 2.0m and lets her go. Her
period is 4.0s.
(a) Calculate her speed 0.50s after being released
(b) Calculate her acceleration 0.50s after being released
Engineering Mechanics – Dynamics 209
Engineering Mechanics – Dynamics 210
• Nik is bungee jumping. In one oscillation he
travels 12 m and it takes 8.0s.
• Tahi starts videoing him as he passes
through the mid position moving UP.
(a) Calculate his velocity 1.0s after the video
starts
(b) Calculate his acceleration 2.0s after the video
starts.
Engineering Mechanics – Dynamics 211
Mass on a Spring
• As the mass increases, the period… increases
• As the spring stiffness increases the period …
increases
Effect of mass:
decreases
• As the acceleration decreases the period …
increases
A larger mass means a longer period.
(assuming constant force)
m
• As the mass increases, the acceleration…
Engineering Mechanics – Dynamics 212
a 
F
Effect of spring stiffness:
• As the stiffness increases, the restoring force…
• As the acceleration increases the period …
A stiffer spring means a shorter period.
m
Engineering Mechanics – Dynamics 213
a 
F
increases (assuming same displacement)
• As the restoring force increases the acceleration …
increases
decreases
F  kx
m
Engineering Mechanics – Dynamics 214
k
T  2
Summary
• mass ↑ acceln↓ period ↑
• stiffness ↑ force ↑ acceln ↑ period
eq↓
uation
Extension …..derivation of the equation:
consider a mass on a spring.
a 
F
F  -kx
m
m
a 
kx a  
k
x (i.e.
m
a x)
m
a 
k
x a 2
x
k
 2
 (
2 )2
m
Engineering Mechanics – Dynamics 215
m T k
m T
k

2
T  2
energy of motion
1/27/2017 Engineering Mechanics – Dynamics
21
6
Engineering Mechanics – Dynamics
Simple Pendulum
• This is where all the mass is concentrated in
one point.
Engineering Mechanics – Dynamics 217
What provides the restoring force?
the restoring force is
the Tension plus
Gravity
Engineering Mechanics – Dynamics 218
Why is the motion SHM?
As the displacement increases,
the restoring force. increases.
the restoring force is always
towards equilibrium
Engineering Mechanics – Dynamics 219
Engineering Mechanics – Dynamics 220
Engineering Mechanics – Dynamics 221
• This next bit is very important
Why does length affect period?
For the same amplitude, if the pendulum is shorter,
the angle of the string to the vertical is greater.
The restoring force is greater.
The acceleration is greater
So the period is shorter
Engineering Mechanics – Dynamics 222
period of a pendulum
l
g
T  2
How is lengthmeasured?
Engineering Mechanics – Dynamics 223
As the pendulum expands
down,
Engineering Mechanics – Dynamics 224
The mercury expands up
This keeps the center of
mass in the same place
Same length same period.
Engineering Mechanics – Dynamics 225
Energy of SHM
energy of motion
1/27/2017 Engineering Mechanics – Dynamics
22
6
Engineering Mechanics – Dynamics
a sprung system
1/27/2017 Engineering Mechanics – Dynamics 227
22
7
Engineering Mechanics – Dynamics
dampers
1/27/2017 Engineering Mechanics – Dynamics 228
22
8
Engineering Mechanics – Dynamics
energy dissipation
plunger
hydraulic oil
dividing
piston
high pressure
nitrogen gas
1/27/2017 Engineering Mechanics – Dynamics 229
22
9
Engineering Mechanics – Dynamics
bridge dampers
1/27/2017 Engineering Mechanics – Dynamics 230
23
0
Engineering Mechanics – Dynamics
Resonance
1/27/2017 Engineering Mechanics – Dynamics 231
 Any elastic system has a natural period of
oscillation.
 If bursts of energy (pushes) are supplied
at the natural period, the amplitude will
increase.
 This is called resonance
23
1
Engineering Mechanics – Dynamics
1/27/2017 Engineering Mechanics – Dynamics 232
23
2
Engineering Mechanics – Dynamics
Examples of resonance
1/27/2017 Engineering Mechanics – Dynamics 233
23
3
Engineering Mechanics – Dynamics
 The glass has a natural frequency of
vibration.
 If you tap the glass, it vibrates at the
natural frequency causing sound.
 If you put energy in at the natural
frequency,the amplitude increases.
This is resonance.
 If the amplitude gets high enough,the
glass can break.
1/27/2017 Engineering Mechanics – Dynamics 234
23
4
Engineering Mechanics – Dynamics
Bay of Fundy
1/27/2017 Engineering Mechanics – Dynamics 235
23
5
Engineering Mechanics – Dynamics
Bay of Fundy
1/27/2017 Engineering Mechanics – Dynamics 236
The period of the tide is 12 hours.
The time for a wave to move up the bay and
back is 12 hours
23
6
Engineering Mechanics – Dynamics
What is vibration?
 Vibrations are oscillations of a system about
an equilbrium position.
23
7
Engineering Mechanics – Dynamics
Vibration…
It is also an
everyday
phenomenon we
meet on
everyday life
23
8
Engineering Mechanics – Dynamics
Vibration …
Useful Vibration Harmful vibration
Noise
Destruction
Compressor
Ultrasonic
cleaning
Testing
Wear
Fatigue
23
9
Engineering Mechanics – Dynamics
Vibration parameters
All mechanical systems
can be modeled by
containing three basic
components:
spring, damper, mass
When these components are subjected to constant force, they
react with a constant
displacement, velocity and acceleration
24
0
Engineering Mechanics – Dynamics
Free vibration
Equilibrium pos.
 When a system is initially disturbed by a displacement,
velocity or acceleration, the system begins to vibrate with a
constant amplitude and frequency depend on its stiffness and
mass.
 This frequency is called as natural frequency,and the form
of the vibration is called as mode shapes
24
1
Engineering Mechanics – Dynamics
ForcedVibration
If an external force applied to a
system, the system will follow the
force with the same frequency.
However, when the force frequency
is increased to the system’s natural
frequency, amplitudes will
dangerously increase in this region.
This phenomenon called as
“Resonance”
’
24
2
Engineering Mechanics – Dynamics
Bridge collapse:
http://www.youtube.com/watch?v=j-zczJXSxnw
Hellicopter resonance:
http://www.youtube.com/watch?v=0FeXjhUEXlc
Resonance vibration test:
http://www.youtube.com/watch?v=LV_UuzEznHs
Flutter (Aeordynamically induced vibration) :
http://www.youtube.com/watch?v=OhwLojNerMU
Watch these …
24
3
Engineering Mechanics – Dynamics
Lumped (Rigid) Modelling Numerical Modelling
Element-based
methods
(FEM, BEM)
Statistical and Energy-based
methods
(SEA, EFA, etc.)
Modelling of vibrating systems
24
4
Engineering Mechanics – Dynamics
•Mathematical modeling of a physical system requires the
selection of a set of variables that describes the behavior of the
system.
•The number of degrees of freedom for a system is the number
of kinematically independent variables necessary to completely
describe the motion of every particle in the
system
DOF=1
Single degree of freedom
(SDOF)
DOF=2
Multi degree of freedom
(MDOF)
Degree of Freedom (DOF)
24
5
Engineering Mechanics – Dynamics
Equivalent model of systems
Example
1:
Example
2:
SDOF
DOF=1
MDOF
DOF=2
24
6
Engineering Mechanics – Dynamics
Equivalent model of systems
Example
3:
SDOF
MDOF
DOF=2
DOF= 3 if body 1 has no
rotation
DOF= b4odiyf1body1has
rotation
24
7
Engineering Mechanics – Dynamics
SDOF systems
 Helical springs
F: Force, D: Diameter, G: Shear modulus of the rod,
Shear
stress:
Stiffness
coefficient:
N: Number of turns, r : Radius
 Springs in combinations:
Parallel combination Series combination
24
8
Engineering Mechanics – Dynamics
Elastic elements as springs
24
9
Engineering Mechanics – Dynamics
Moment of Inertia
25
0
Engineering Mechanics – Dynamics
What are the equivalent stiffnesses?
25
1
Engineering Mechanics – Dynamics

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  • 1. INSTITUTE OFAERONAUTICAL ENGINEERING (Autonomous) Dundigal, Hyderabad - 500043 Course : ENGINEERING MECHANICS (AME002) Prepared by : Mr. B.D.Y.Sunil Assistant Professor 1 Engineering Mechanics – Dynamics
  • 2. Subject Engineering Mechanics – Dynamics 2 30% 70%  Graduates: ◦ Midterm exam ◦ Final exam  Course Materials ◦ Lecture notes  Power points slides  Class notes ◦ Textbooks  Engineering Mechanics: Statics 10th Edition by R.C. Hibbeler 2 Engineering Mechanics – Dynamics
  • 3. COURSE OBJECTIVES Engineering Mechanics – Dynamics 3 The course should enable the students to: III. I. Develop the ability to work comfortably with basic engineering mechanics concepts required for analysing static structures. II. Identify an appropriate structural system to studying a given problem and isolate it from its environment, model the problem using good free body diagrams and accurate equilibrium equations. Identify and model various types of loading and support conditions that act on structural systems, apply pertinent mathematical, physical and engineering mechanical principles to the system to solve and analyze the problem. IV. Solve the problem of equilibrium by using the principle of work and energy in mechanical design and structural analysis. V. Apply the concepts of vibrations to the problems associated with dynamic behavior. 3 Engineering Mechanics – Dynamics
  • 4. COURSE OUTCOMES Engineering Mechanics – Dynamics 4 After completing this course the student must demonstrate the knowledge and ability to: 1.Classifying different types of motions in kinematics. 2.Categorizing the bodies in kinetics as a particle,rigid body in translation and rotation. 3.Choosing principle of impulse momentum and virtual work for equilibrium of ideal systems, stableand unstable equilibriums 4.Appraising work and energy method for particle motion and plane motion. 5.Apply the concepts of vibrations. 4 Engineering Mechanics – Dynamics
  • 5. KINEMATICS KINETICS NEWTON’S LAW KINETICS ENERGY & MOMENTUM PARTICLE SYSTEM OF PARTICLES RIGID BODIES Chapter 1 Chapter 2 Chapter 3 Chapter 4 Chapter 3 Chapter 4 Chapter 5 Course Outline Engineering Mechanics – Dynami5cs 5 Engineering Mechanics – Dynamics
  • 6. Introduction to Mechanics Mechanics Statics Dynamics Kinematics Kinetics Engineering Mechanics – Dynamics 6  What is mechanics? Physical science deals with the state of rest or motion of bodies under the action of force  Why we study mechanics? This science form the groundwork for further study in the design and analysis of structures 6 Engineering Mechanics – Dynamics
  • 7. BasicTerms Engineering Mechanics – Dynamics 7  Essential basic terms to be understood ◦ Statics: dealing with the equilibrium of a rigid-body at rest ◦ Rigid body: the relative movement between its parts are negligible ◦ Dynamics: dealing with a rigid-body in motion ◦ Length: applied to the linear dimension of a straight line or curved line ◦ Area: the two dimensional size of shape or surface ◦ Volume: the three dimensional size of the space occupied by substance ◦ Force: the action of one body on another whether it’s a push or a pull force ◦ Mass: the amount of matter in a body ◦ Weight:the force with which a body is attracted toward the centre of the Earth ◦ Particle:a body of negligible dimension 7 Engineering Mechanics – Dynamics
  • 8. Units of Measurement 1/27/2017 Engineering Mechanics – Dynamics 8  Four fundamental quantities in mechanics ◦ Mass ◦ Length ◦ Time ◦ Force  Two different systems of units we dealing with during the course ◦ Units (CGS)  Length in centimeter(cm)  Time in Seconds (s)  Force in kilograms (kg) ◦ International System of Units or Metric Units (SI)  Length in metre (m)  Time in Seconds (s)  Force in Newton (N) 8 Engineering Mechanics – Dynamics
  • 9. Units of Measurement Engineering Mechanics – Dynamics 9 Quantity SI Units US Units Unit Symbol Unit Symbol Mass kilogram kg slug - Length meter m foot ft Time second s second sec Force newton N pound lb Summery of the four fundamental quantities in the two system 9 Engineering Mechanics – Dynamics
  • 10. Units of Measurement Engineering Mechanics – Dynamics 10  Metric System (SI) ◦ SI System offers major advantages relative to the FPS system  Widely used throughout the world  Use one basic unit for length  meter; while FPS uses many basic units  inch,foot,yard,mile  SI based on multiples of 10, which makes it easier to use & learn whereas FPS is complicated,for example  SI system 1 meter = 100 centimeters,1 kilometer = 1000 meters,etc  FPS system 1 foot = 12 inches,1 yard = 3 feet,1 mile = 5280 feet,etc  Metric System (SI) ◦ Newton’s second law F = m.a  Thus the force (N) = mass (kg)  acceleration (m/s2) ◦ Therefore 1 Newton is the force required to give a mass of 1 kg an acceleration of 1 m/s2 10 Engineering Mechanics – Dynamics
  • 11. Units of Measurement  U.S. Customary System (FPS) ◦ Force (lb) = mass (slugs)  acceleration (ft/sec2 )  Thus (slugs) = lb.sec2/ft ◦ Therefore 1 slug is the mass which is given an acceleration of 1 ft/sec2 when acted upon by a force of 1 lb  Conversion of Units ◦ Converting from one system of unit to another;  The standard value of g (gravitational acceleration) ◦ SI units g = 9.806 m/s2 ◦ FPS units g = 32.174 ft/sec2 Quantity FPS Equals SI Force 1 lb 4.448 N Mass 1 slug 14.593 kg Length 1 ft 0.304 m Engineering Mechanics – Dynamics 11 11 Engineering Mechanics – Dynamics
  • 12. Objectives Engineering Mechanics – Dynamics 12 T oprovide an introductionof: ※ Fundamental concepts, ※ General principles, ※ Analysis methods, ※ Future Studies in Engineering Mechanics. 12 Engineering Mechanics – Dynamics
  • 13. Outline Engineering Mechanics – Dynamics 13  1. EngineeringMechanics  2. FundamentalConcepts  3. GeneralPrinciples  4. StaticAnalysis  5. DynamicAnalysis  6. FutureStudies 13 Engineering Mechanics – Dynamics
  • 14. 1. Engineering Mechanics Engineering Mechanics – Dynamics 14  Mechanics : - Rigid-body Mechanics - Deformable-body Mechanics - Fluid Mechanics  Rigid-body Mechanics : - Statics - Dynamics 14 Engineering Mechanics – Dynamics
  • 15.  Statics – Equilibrium Analysis of particles and bodies  Dynamics – Accelerated motion of particles and bodies Kinematics and Kinetics  Mechanics of Materials…  Theory ofVibration… 1. Engineering Mechanics Engineering Mechanics – Dynamics 15 15 Engineering Mechanics – Dynamics
  • 16. 2. Fundamentals Concepts Engineering Mechanics – Dynamics 16 Basic Quantities  Length, Mass,Time,Force Units of Measurement  m, kg,s,N… (SI, Int.System of Units) - Dimensional Homogeneity - Significant Figures 16 Engineering Mechanics – Dynamics
  • 17. 2. Fundamentals Concepts Engineering Mechanics – Dynamics 17 Idealizations  Particles – Consider mass but neglect size  Rigid Body – Neglect material properties  Concentrated Force  Supports and Reactions 17 Engineering Mechanics – Dynamics
  • 18. 3. General Principles Engineering Mechanics – Dynamics 18 - Newton’s Laws of Motion  First Law, Second Law,Third Law  Law of GravitationalAttraction - D’Alembert Principle :F+(-ma)=0 - Impulse and Momentum - Work and Energy - Principle ofVirtualWork (Equilibrium) 18 Engineering Mechanics – Dynamics
  • 19. 4. StaticAnalysis Engineering Mechanics – Dynamics 19  Force and Equilibrium  Force System Resultants  StructuralAnalysis  Internal forces  Friction  Centroid and Moments of Inertia  VirtualWork andStability 19 Engineering Mechanics – Dynamics
  • 20. 5. DynamicAnalysis Engineering Mechanics – Dynamics 20  Kinematics of a Particle  Kinetics: Force andAcceleration  Work and Energy  Impulse and Momentum (Impact)  Planar Kinematics and Kinetics  3-D Kinematics and Kinetics  Vibrations 20 Engineering Mechanics – Dynamics
  • 21. UNIT-I KINEMATICS OF PARTICLES IN Engineering Mechanics – Dynamics 21 RECTILINEAR MOTION Motion of a particle, rectilinear motion, motion curves, rectangular components of curvilinear motion, kinematics of rigid body, types of rigid body motion, angular motion, fixed axis rotation. 21 Engineering Mechanics – Dynamics
  • 22. INTRODUCTION TODYNAMICS Engineering Mechanics – Dynamics 22  Galileo and Newton (Galileo’s experiments led to Newton’s laws)  Kinematics – study of motion  Kinetics – the study of what causes changes in motion  Dynamics is composed of kinematics and kinetics 22 Engineering Mechanics – Dynamics
  • 23. Engineering Mechanics – Dynamics 23 Introduction • Dynamics includes: - Kinematics: study of the motion (displacement, velocity, acceleration, & time) without reference to the cause of motion (i.e. regardless of forces). - Kinetics: study of the forces acting on a body, and the resulting motion caused by the given forces. • Rectilinear motion: position, velocity, and acceleration of a particle as it moves along a straight line. • Curvilinear motion: position, velocity, and acceleration of a particle as it moves along a curved line. 23
  • 24. Engineering Mechanics – Dynamics 24 RECTILINEAR MOTION OF PARTICLES 24
  • 25. Rectilinear Motion: Position, Velocity & Acceleration Engineering Mechanics – Dynamics 25
  • 26. Acceleration MECHANICS Kinematics of Particles Motion in One Dimension 26 Engineering Mechanics – Dynamics
  • 27. Summary of properties of vectors 27 Engineering Mechanics – Dynamics
  • 28. POSITION, VELOCITY, AND ACCELERATION For linear motion x marks the position of an object. Position units would be m, ft, etc. Average velocity is t Velocity units would be in m/s, ft/s, etc. The instantaneous velocity is v  x dt v  lim x  dx 28 En  gin te ering0 Mech  anict s – Dynamics 28 Engineering Mechanics – Dynamics
  • 29. The average acceleration is a  v t The units of acceleration would be m/s2, ft/s2, etc. The instantaneous acceleration is t0 t a  lim 2 Engineering Mechanics – Dynamics 29 dt dt dt dt v  dv  d dx  d 2 x
  • 30. dt dx dt dx a  dv  dv dx  v dv One more derivative dt da  Jerk Notice If v is a function of x, then Engineering Mechanics – Dynamics 30
  • 31. Consider the function x  t3  6t2 v  3t2 12t a  6t 12 x(m) 0 16 32 2 4 t(s) 6 t(s) Plotted a(m/s2) 12 0 -12 -24 2 4 6 0 v(m/s) 12 -12 -24 -36 2 4 Engineering Mechanics – Dynamics 31 t(s) 6
  • 32. Rectilinear Motion: Position, Velocity & Acceleration • Particle moving along a straight line is said to be in rectilinear motion. • Position coordinate of a particle is defined by (+ or -) distance of particle from a fixed origin on the line. • The motion of a particle is known if the position coordinate for particle is known for every value of time t. Motion of the particle may be expressed in the form of a function, e.g., 3 x  6t2 t or in the form of a graph x vs. t. Engineering Mechanics – Dynamics 32
  • 33. Rectilinear Motion: Position, Velocity & Acceleration • Consider particle which occupies position P at time t and P’at t+t, t Average velocity  x Instantaneous velocity  v  lim x t0 t • Instantaneous velocity may be positive or negative. Magnitude of velocity is referred to as particle speed. • From the definition of a derivative, dt Engineering Mechanics – Dynamics v  dx 12t 3t2 v  lim x  dx t0 t dt e.g., x  6t2 t3 33
  • 34. Rectilinear Motion: Position, Velocity & Acceleration dt dt2 a  dv 12  6t e.g. v 12t 3t2 t dt v dv d2x a  lim   t0 • Consider particle with velocity v at time t and v’at t+t, Instantaneous acceleration a  lim v t0 t • From the definition of a derivative, Engineering Mechanics – Dynamics 34
  • 35. Rectilinear Motion: Position, Velocity & Acceleration • Consider particle with motion given by x  6t2 t3 dt v  dx 12t 3t2 dv d2x Engineering Mechanics – Dynamics a   126t dt dt2 • at t = 0, x = 0, v = 0, a = 12 m/s2 • at t = 2 s, x = 16 m, v = vmax = 12 m/s, a = 0 • at t = 4 s, x = xmax = 32 m, v = 0, a = -12m/s2 • at t = 6 s, x = 0, v = -36 m/s, a = -24 m/s2 35
  • 36. Engineering Mechanics – Dynamics 36 DETERMINATION OF THE MOTION OF A PARTICLE Three common classes of motion
  • 37. Engineering Mechanics – Dynamics 37  0 0 v v  dt dv  adt  f (t )dt t 1. a  f (t )  dv 0 dt f ( t )dt  dx v t  0 0 f (t )dt dt dx  v 
  • 38. Engineering Mechanics – Dynamics 38 t  0 0 f (t )dt dt dx  v    t t 0 0 x  x0  v0 t   f (t )dt dt   t 0 dx  v0 dt   f (t )dtdt
  • 39. Engineering Mechanics – Dynamics 39   0 0 t t x  x0  v0t   f (t )dtdt
  • 40. x  xo f (x)dx 0 2 1 (v2  v2 ) dt dx with v  then get x  x(t) 2. a  f ( x )  v dv Engineering Mechanics – Dynamics 40 dx vdv adx  f ( x)dx
  • 41. v t dv v0 0 x v x0 v0 vdv dx   f (v ) Both can lead to x  x( t ) or dt dx Engineering Mechanics – Dynamics 41 3. a  f ( v )  dv  v dv  f (v )  dt  t
  • 42. 1/27/2017 42 UNIFORM RECTILINEAR MOTION v  constant a 0 v  dx dt x  x0  vdt  vt x  Engineeri x ng M 0 echani  cs – Dyn v amics t 42 Engineering Mechanics – Dynamics
  • 43. Also dx v dv  a UNIFORMLY ACCELERATED RECTILINEAR MOTION a  constant v  v0  at 2 o 0 x  x  v t  1 at 2 1/27/2017 43 v2  v2  2a( x  x ) En 0 gineering Mechanics – Dynamics 0 43 Engineering Mechanics – Dynamics
  • 44. Determining the Motion of a Particle • Recall, motion is defined if position x is known for all time t. • If the acceleration is given, we can determine velocity and position by two successive integrations. • Three classes of motion may be defined for: - acceleration given as a function of time, a = f(t) - acceleration given as a function of position, a = f(x) - acceleration given as a function of velocity, a = f(v) v  dx a  dv dt dt d2 x dt2 a  a  dv  dv dx  v dv dt dx dt dx 14/247/2017 Engineering Mechanics – Dynamics 44
  • 45. Determining the Motion of a Particle • Acceleration given as a function of time, a = f(t): a  f (t)  dv  dv dt v  f (t)dt   v0 t dv   f (t)dt  0 t v  v0   f (t)dt 0 v  dx dt  dx vdt x t  dx  vdt x0 0 t  x  x0 vdt 0 2 2 0 1 1 2 2 v x x v0 x0 x0 dv a  f (x)  v dx  v  v  f (x)dx  vdv  f (x)dx  vdv   f (x)dx  •Acceleration given as a function of position, a = f(x): 0 14/257/2017 Engineering Mechanics – Dynamics x x dx dx dt dx v v v    dt   t  dt 0 45
  • 46. Determining the Motion of a Particle v dv dt dv f (v) dv f (v) dv f (v) a  f (v)   t v  dt   0 t v  dt   0 v0 x v 14/267/2017 Engineering Mechanics – Dynamics x0 v0 v dv dx vdv f (v) vdv f (v) vdv f (v) a  f (v)  v  dx  dx   v  x  x0  0 • Acceleration given as a function of velocity, a = f(v): 46
  • 47. Summary Procedure: 1. Establish a coordinate system & specify an origin 2. Remember: x,v,a,t are related by: 3. When integrating, either use limits (if integration dt dt v  dx a  dv d2 x dt2 a  dt dx dt dx known) or add a constant of a  dv  dv dx  v dv 14/277/2017 Engineering Mechanics – Dynamics 47
  • 48. Sample Problem 1 Ball tossed with 10 m/s vertical velocity from window 20 m above ground. Determine: • velocity and elevation above ground at time t, • highest elevation reached by ball and corresponding time, and • time when ball will hit the ground and corresponding velocity. 14/287/2017 Engineering Mechanics – Dynamics 48
  • 49. Sample Problem 1 dt t vt v0 0 vt  v0  9.81t dv  a  9.81m s2 dv  9.81dt    s2  s vt10 m 9.81 m t 2 dt t yt y0 0 yt y0 10t  1 9.81t2 dy  v 109.81t dy  109.81tdt 2 s  m    m  t  4.905 2 t   s     yt 20m  10 SOLUTION: • Integrate twice to find v(t) and y(t). 14/297/2017 Engineering Mechanics – Dynamics 49
  • 50. Sample Problem 1 • Solve for t at which velocity equals zero and evaluate corresponding altitude. s s   2   vt10 m 9.81 m t  0 t 1.019s 2 2 1.019s m m 2  s      1.019s 4.905   s       s  m  m    s     y  20m  10 t  4.905 2 t yt 20m  10 y  25.1m 15/207/2017 Engineering Mechanics – Dynamics 50
  • 51. Sample Problem 1 • Solve for t at which altitude equals zero and evaluate corresponding velocity. 2   s  m  m    s     t  4.905 2 t  0 yt 20m  10 t  1.243s meaningless t  3.28s s s  2   s   2   s  v3.28s10 m 9.81 m 3.28s vt10 m 9.81 m t s v  22.2 m 15/217/2017 Engineering Mechanics – Dynamics 51
  • 52. What if the ball is tossed downwards with the same speed? (The audience is thinking …) vo= - 10 m/s 15/227/2017 Engineering Mechanics – Dynamics 52
  • 53. Uniform Rectilinear Motion Uniform rectilinear motion acceleration = 0 velocity = constant dt x t dx  v dt x0 0 x  x0  vt x  x0 vt dx  v  constant 15/237/2017 Engineering Mechanics – Dynamics 53
  • 54. Uniformly Accelerated Rectilinear Motion Uniformly accelerated motion acceleration = constant v  v  at t  dt v  v0  at 0 dv  a dt 0 v  v0 dv  a  constant 2 2 0 0 0 0 dt t x  x0  v0t  1 at2 x  x  v t  1 at 2 v  atdt dx    at dx  v  0 x  x0 0 0 2 2 1 2 dx v2  v2  2ax  x  0 0 ax  x  v  v  vdv  a dx x0 v dv  a  constant x  v  v0 Also: 15/247/2017 Engineering Me c haAnic sp–pD y ln ia m ci ac s tion:free fall 54 Engineering Mechanics – Dynamics
  • 55. MOTION OF SEVERAL PARTICLES When independent particles move along the same line, independent equations exist for each. Then one should use the same origin and time. Engineering Mechanics – Dynamics 55
  • 56. Relative motion of two particles. The relative position of B with respect to A xB  xB  xA A The relative velocity of B with respect to A vB  vB vA A Engineering Mechanics – Dynamics 56
  • 57. The relative acceleration of B with respect to A A Engineering Mechanics – Dynamics 57 A B B a  a a
  • 58. Motion of Several Particles: Relative Motion • For particles moving along the same line, displacements should be measured from the same origin in the same direction. xB A  xB  xA  relative position of B with respect to A A B A B x  x  x vB A  vB  vA  relative velocity of B with respect to A vB  vA  vBA aB A  aB  aA  relative acceleration of B with respect to A 15/287/2017 aB  aA  aB A Engineering Mechanics – Dynamics 58 Engineering Mechanics – Dynamics
  • 59. Engineering Mechanics – Dynamics 59 Let’s look at some dependent motions.
  • 60. A C D E F G System has one degree of freedom since only one coordinate can be chosen independently. xA xB A B x  2x  constant v  2v 0 A B a  2a 0 A B B Let’s look at the relationships. Engineering Mechanics – Dynamics 60
  • 61. System has 2 degrees of freedom. C A B xA xC xB 2x  2x  x  constant A B C A B C 2v  2v v 0 2a  2a  a 0 Let’s look at the relationships. A Engineering Mechanics – Dynamics B C 61 Engineering Mechanics – Dynamics
  • 62. Ball thrown vertically from 12 m level in elevator shaft with initial velocity of 18 m/s. At same instant, open-platform elevator passes 5 m level moving upward at 2 m/s. Determine (a) when and where ball hits elevator and (b) relative velocity of ball and elevator at contact. Sample Problem 2 16/227/2017 Engineering Mechanics – Dynamics 62
  • 63. SOLUTION: Sample Problem 2 • Ball: uniformly accelerated motion (given initial position and velocity). • Elevator: constant velocity (given initial position and velocity) • Write equation for relative position of ball with respect to elevator and solve for zero relative position, i.e., impact. • Substitute impact time into equation for position of elevator and relative velocity of ball with respect to elevator. 16/237/2017 Engineering Mechanics – Dynamics 63
  • 64. Sample Problem 3 SOLUTION: • Ball: uniformly accelerated rectilinear motion. 2 2 2 1 0 0 s B B 0 s    m  m  t  4.905 2 t   s     y  y  v t  at 12m  18   s  v  v  at 18 m 9.81 m  2 t • Elevator: uniform rectilinear motion.   16/247/2017 Engineering Mechanics – Dynamics  s  y  y  v t  5m  2 mt s vE  2 m E 0 E 64
  • 65. Sample Problem 3 • Relative position of ball with respect to elevator: yB E  1218t  4.905t2 5 2t 0 t  0.39s meaningless t  3.65s • Substitute impact time into equations for position of elevator and relative velocity of ball with respect to elevator. yE  5 23.65 yE  12.3m vB E  18 9.81t 2 169.813.65 s vB E  19.81 m 16/257/2017 Engineering Mechanics – Dynamics 65
  • 66. Motion of Several Particles: Dependent Motion • Position of a particle may depend on position of one or more other particles. • Position of block B depends on position of block A. Since rope is of constant length, it follows that sum of lengths of segments must be constant. xA  2xB  constant (one degree offreedom) • Positions of three blocks are dependent. 2xA  2xB  xC  constant (two degrees offreedom) • For linearly related positions, similar relations hold between velocities and accelerations. 2 dxA  2 dxB  dxC  0 or 2vA  2vB  vC  0 dt dt dt 2 dvA  2 dvB  dvC  0 or 2a A  2aB  aC  0 dt dt dt 16/267/2017 Engineering Mechanics – Dynamics 66
  • 68. Sample Problem 4 Pulley D is attached to a collar which is pulled down at 3 in./s. At t = 0, collarA starts moving down from K with constant acceleration and zero initial velocity. Knowing that velocity of collar A is 12 in./s as it passes L, determine the change in elevation, velocity, and acceleration of block B when block A is at L. 16/287/2017 Engineering Mechanics – Dynamics 68
  • 69. Sample Problem 4 SOLUTION: • Define origin at upper horizontal surface with positive displacement downward. • Collar A has uniformly accelerated rectilinear motion. Solve for acceleration and time t to reach L. 2 s in. in. 2 12 s     A   aA  9  2aA 8in. A2  2aAxA  xA   0 0 v2 v s 16/297/2017 Engineering Mechanics – Dynamics s2 t 1.333s 12 in.  9 in. t vA  vA 0 aAt 69
  • 70. Sample Problem 4  s    D D 0 x x   3 in.1.333s 4in. • Pulley D has uniform rectilinear motion. Calculate change of position at time t. xD  xD 0 vDt • Block B motion is dependent on motions of collar A and pulley D. Write motion relationship and solve for change of block B position at time t. Total length of cable remains constant, xA  2xD  xB  xA 0 2xD 0 xB 0 xA xA 02xD  xD 0xB xB 0 0 8in. 24in.xB  xB 0 0 xB  xB 0 16in. 17/207/2017 Engineering Mechanics – Dynamics 70
  • 71. Sample Problem 4     s   s   B 12 in.  23 in.  v  0 • Differentiate motion relation twice to develop equations for velocity and acceleration of block B. xA  2xD  xB  constant vA  2vD  vB  0 s B v  18 in. 2 9 s aA  2aD  aB 0  in.  a  0   B   s2 aB  9 in. 17/217/2017 Engineering Mechanics – Dynamics 71
  • 72. Curvilinear Motion http://news.yahoo.com/photos/ss/441/im:/070123/ids_photos_wl/r2207709100.jpg 17/227/2017 Engineering Mechanics – Dynamics A particle moving along a curve other than a straight line is said to be in curvilinear motion. 72
  • 73. CURVILINEAR MOTION OF PARTICLES POSITION VECTOR, VELOCITY, AND ACCELERATION x z y r  r  v   r  t s s P’  s r  P dt   v  t lim r  dr t 0 t dt v  ds Let’s find the instantaneous velocity. 1/27/2017 73 Engineering Mechanics – Dynamics 73 Engineering Mechanics – Dynamics
  • 74. P P’ r  r  v  v ' x y t Engineering Mechanics – Dynamics 1/27/2017 74 z a   v  v  74 Engineering Mechanics – Dynamics
  • 75. P P’ r  r  dt  v  v ' x y x z y t a   v   v a  lim v  dv   t 0 t Note that the acceleration is not necessarily along the direction of the velocity. Engineering Mechanics – Dynamics 1/27/2017 75 z 75 Engineering Mechanics – Dynamics
  • 76. DERIVATIVES OF VECTOR FUNCTIONS du dP  lim P   u0 u   u  lim P(u  u ) P(u )  u0     du  du  du    d( P  Q )  dP  dQ  f dP  df P du  d( fP ) du  1/27/2017 76 Engineering Mech d aniu cs – Dynamics 76 Engineering Mechanics – Dynamics
  • 77. du   du   du   d( PQ )  dP Q P dQ  du du    du   d( PQ )  dP Q  P dQ dP ˆ dPx du  ˆj  z kˆ du Engineering Mechanics – Dynamics 1/27/2017 77 du dPy i  dP du  77 Engineering Mechanics – Dynamics
  • 78. Engineering Mechanics – Dynamics 1/27/2017 78 Rate of Change of a Vector  P  P ˆi P ˆj P kˆ x y z The rate of change of a vector is the same with respect to a fixed frame and with respect to a frame in translation. 78 Engineering Mechanics – Dynamics
  • 79. RECTANGULAR COMPONENTS OF VELOCITY AND ACCELERATION r   xˆi yˆj zkˆ v   xˆi yˆj zkˆ a   xiˆyˆjzkˆ 1/27/2017 79 Engineering Mechanics – Dynamics 79 Engineering Mechanics – Dynamics
  • 80. x y r  yˆ j xî x z y P v  v ˆi x v ˆj y v kˆ z a  1/27/2017 zk̂ 80 z Engineering Mechanics – Dynamics 80 Engineering Mechanics – Dynamics
  • 81. z y a ˆj y ˆ a k z a ˆi x x a  1/27/2017 81 Engineering Mechanics – Dynamics 81 Engineering Mechanics – Dynamics
  • 82. Velocity Components in Projectile Motion ax   x  0 vx  x   vxo Engineering Mechanics – Dynamics 82 xo x  v t a  z0 z v  z v 0 z zo z  0 1 2 yo a  y g y v  y v  gt y yo y  v t  gt2
  • 83. x z y x’ z’ y’ O A B r   r   r  B A B /A MOTION RELATIVE TO A FRAME IN TRANSLATION Engineering Mechanics – Dynamics 83 B r  B / A r  A r 
  • 84. Engineering Mechanics – Dynamics 84 B A B / A r   r  r  r    r    r   B A B / A v   v  v  B A B / A v    v   v   B A B / A B / A a   a  a  B A
  • 85. Engineering Mechanics – Dynamics 85  r     r    r   B A B / A A B / A a  B  a  a 
  • 86. Velocity is tangent to the path of a particle. Acceleration is not necessarily in the same direction. It is often convenient to express the acceleration in terms of components tangent and normal to the path of the particle. TANGENTIAL AND NORMAL COMPONENTS Engineering Mechanics – Dynamics 86
  • 87. O x y t v   veˆ t Engineering Mechanics – Dynamics 87 ê t Plane Motion of a Particle ê' t ê  e ˆn n ê' P’ P
  • 88. lim êt  0   n  0  ê lim êt    lim  2sin 2  e ˆn 0   t e ˆ  deˆ n ˆ  e        ê lim n  2 sin 2 0 t ê t ê' eˆ t  1/27/2017 88 Engineerin n g Mechan d ics  – Dynamics 88 Engineering Mechanics – Dynamics
  • 89.  d t n e ˆ  deˆ v   veˆ t t e ˆ  dv dv dt dt a   dt Engineering Mechanics – Dynamics 89 ˆ d e t  v
  • 90. n  O x y e ˆt t ê' P  P’  s s   s ds d    lim 0  t ˆ dt  dv dt ˆ d e v t a  e  v  v e ˆ dt d ds dt d  deˆt  deˆt d ds  deˆt a   dv ˆ v2 ˆ Engineering Mechanics – Dynamics 90 e  e dt t  n
  • 91. a   dv ˆ v2 ˆ e  e dt t  n a   a e ˆ  a e ˆ t t n n dv at  dt v2 an   Discuss changing radius of curvature for highway cur Engineering Mechanics – Dynamics 91
  • 92. Motion of a Particle in Space The equations are the same. O x y t ê t ê' n ê n ê' P’ P z Engineering Mechanics – Dynamics 92
  • 93. RADIAL AND TRANSVERSE COMPONENTS x y P r Engineering Mechanics – Dynamics 93 ê Plane Motion ê r  
  • 94. êr  êr eˆr ê ê eˆ   dêr d  e ˆ r  eˆ dê d dt d dt deˆr  deˆr  d  e ˆ dt d dt Engineering Mechanics – Dynamics 94 deˆ  deˆ r d   e ˆ
  • 95. vr  r v  r  v   dr dt dt Engineering Mechanics – Dynamics 95 r r r  d ( reˆ )  reˆ  r eˆ v   reˆr  reˆ  vr eˆrveˆ
  • 96. y r ê ê r   x eˆr ˆicos  ˆjsin  deˆr d  ˆisin   ˆjcos  e ˆ r  ˆicos  ˆjsin  eˆ dê d  Engineering Mechanics – Dynamics 96
  • 97. v   reˆr  reˆ a   reˆr  reˆr  reˆ  reˆ reˆ a    rêr  r   ê  r  ê  r ê r  êr 2 a   ( rr2 )eˆ (r 2r)eˆ r  dt dvr r a  dt Engineering Mechanics – Dynamics 97 a  dv 2 r    r r a   a  r 2r Note
  • 98. Extension to the Motion of a Particle in Space: Cylindrical Coordinates r   Reˆ  zkˆ r v   R eˆ  Reˆ  zkˆ R  a   (R   R2 )eˆ  (R2R)eˆ  z  k ˆ R  Engineering Mechanics – Dynamics 98
  • 99. Curvilinear Motion: Position, Velocity & Acceleration • Position vector of a particle at time t is defined by a vector between origin O of a fixed reference frameand the position occupied by particle. • Consider particle which occupies position Pdefined by r at time t and P’defined by r at t + t,  dr t0 t dt   v lim r  instantaneous velocity (vector) v  lim s  ds t0 t dt  instantaneous speed (scalar) 19/297/2017 E ng in e e r iVng eMloe c cha in tyic si– sDty an a nm gi c esnt to path 99 Engineering Mechanics – Dynamics
  • 100. Curvilinear Motion: Position, Velocity & Acceleration  dv   t0 t dt a lim v • Consider velocity v of particle at time t and velocity vat t + t,  instantaneous acceleration(vector) • In general, acceleration vector is not tangent to particle path and velocity vector. 1 1 /2070/20 17 Engineering Mechanics – Dynamics 10 0
  • 101. Rectangular Components of Velocity & Acceleration  • Position vector of particle P given by its rectangular components: r xi   y  j zk • Velocity vector, zk k dt dt dt z   vx i   v y  jv k v dx i   dy  j dz   xi   y  j   • Acceleration vector, z 1 1 /2071/20 17 Engineering Mechanics – Dynamics      ax i   a y  j ak a  i  j  k  xi yj  zk dt2 dt2 dt2  d 2x d 2y d2z 10 1
  • 102.     0 0 x y x0  y0  z0  0 v  v  given Rectangular Components of Velocity & Acceleration • Rectangular components are useful when acceleration components can be integrated independently, ex: motion of a projectile. ax  x 0 ay  y g az  z 0 with initial conditions, Therefore: • Motion in horizontal direction is uniform. • Motion in vertical direction is uniformly accelerated. • Motion of projectile could be replaced by two independent rectilinear motions. 1 1 /2072/20 17 Engineering Mechanics – Dynamics   0 0 2 0 0 1 2 x y vx  vx  vy  vy  gt x  v  t y  v t  gt 10 2
  • 103. x v  v0  at 0 0 2 x  x  v t  1 at2   1 1 /2073/20 17 Engineering Mechanics – Dynamics 2 2 0 0 v  v  2a x x Example A projectile is fired from the edge of a 150-m cliff with an initial velocity of 180 m/s at an angle of 30° with the horizontal. Find (a)the range, and (b) maximum height. y Remember: 10 3
  • 104. Example Car A is traveling at a constant speed of 36 km/h. As A crosses intersection, B starts from rest 35 m north of intersection and moves with a constant acceleration of 1.2 m/s2. Determine the speed, velocity and acceleration of B relative to A 5 seconds after A crosses intersection. 1 1 /2074/20 17 Engineering Mechanics – Dynamics 10 4
  • 105. Tangential and Normal Components • Velocity vector of particle is tangent to path of particle. In general, acceleration vector is not. Wish to express acceleration vector in terms of tangential and normal components. • particle path at P and P’. respect to the same origin, t t e and e are tangential unit vectors for the When drawn with det  et et et et  det det d From geometry: t n de  de n det d  e d det 1 1 /2075/20 17 Engineering Mechanics – Dynamics 10 5
  • 106. 106 t n t n dv dt dv v2 dt  v2  a  e  e a  a  Tangential and Normal Components t • With the velocity vector expressed as v ve t t dt dt dt dt the particle acceleration may be written as d ds d ds dt a  dv  dv e  v det  dv e  v det ds dt n  v  d  ds d t  e but de  After substituting, • Tangential component of acceleration reflects 1/27/2017 change of speed and normal component reflects change of direction. • Tangential component may be positive or negative. Normal component always points toward center of path curvature. Engineering Mechanics – Dynamics 10 6 Engineering Mechanics – Dynamics
  • 107. r  rer Radial and Transverse Components • If particle position is given in polar coordinates, wecan express velocity and acceleration with components parallel and perpendicular to OP.  de  de   d d   er r  e dt d  dt  e r  r dt dt d de de d d dt d  d dt de  de   er      r r r d dr de dt dt dt v  re  e  r • Particle velocity vector:   r • Similarly, particle acceleration: d dt de dt dt r     d d dt a  re  r e  re  r der  re e   r r  rer  re dt  r e r erer r   re  r • Particle position vector: r dt dt  r  v  dr e  r d e  re  re     2 r  a  r  r e  r  2r e 11/2077/2017 Engineering Mechanics – Dynamics 10 7 Engineering Mechanics – Dynamics
  • 108. Sample Problem A motorist is traveling on curved section of highway at 60 mph. Themotorist applies brakes causing a constant deceleration. Knowing that after 8 s the speed has been reduced to 45 mph, determinethe acceleration of the automobile immediately after the brakes are applied. 1 1 /2078/20 17 Engineering Mechanics – Dynamics 10 8
  • 109. Sample Problem 60 mph  88ft/s 45mph  66ft/s ft 2500ft s2 8s 88 ft s2  3.10 s2 v2 t SOLUTION: • Calculate tangential and normal components of acceleration. a  v  66  88ft s  2.75 ft an    t • Determine acceleration magnitude and direction with respect to tangent to curve. a  a2  a2   2.752  3.102 t n s2 a  4.14 ft   tan 1 an  tan 13.10 at 2.75   48.4 1 1 /2079/20 17 Engineering Mechanics – Dynamics 10 9
  • 110. Sample Problem Determine the minimum radius of curvature of the trajectory described by the projectile. v2 an   Recall: 2   v an Minimum r, occurs for small v and large an 155.92 9.81    2480m v is min and an ismax an a 11/1270/2017 Engineering Mechanics – Dynamics 11 0
  • 111. Sample Problem Rotation of the arm about O is defined by  = 0.15t2 where  is in radians and t in seconds. Collar B slides along the arm such that r = 0.9 - 0.12t2 where r is in meters. After the arm has rotated through 30o, determine (a) the total velocity of the collar, (b) the total acceleration of the collar, and (c) the relative acceleration of the collar with respect to the arm. 11/1217/2017 Engineering Mechanics – Dynamics 11 1
  • 112. Sample Problem SOLUTION: • Evaluate time t for  = 30o.   0.15t 2  30  0.524rad t 1.869s • Evaluate radial and angular positions, and first and second derivatives at time t. r  0.9 0.12t2  0.481m r 0.24 t  0.449 ms r 0.24 m s2   0.15t 2 0.524rad  0.30 t  0.561rad s  0.30 rad s2 1 1 /1272/2 017 Engineering Mechanics – Dynamics 11 2
  • 113. Sample Problem   tan1 v vr v  v2  v2 r  • Calculate velocity and acceleration. vr  r 0.449 m s v r 0.481m0.561rad s  0.270 ms v  0.524m s   31.0   tan1a ar a  a2  a2 r  ar  rr2  0.240 m s2  0.481m0.561rads2  0.391m s2 a r2r  0.481m0.3rad s2 2 0.449 m s0.561rad s  0.359 m s2 a  0.531m s  42.6 1 1 /1273/2 017 Engineering Mechanics – Dynamics 11 3
  • 114. Sample Problem • Evaluate acceleration with respect to arm. Motion of collar with respect to arm is rectilinear and defined by coordinate r. aB OA  r 0.240 m s2 1 1 /1274/2 017 Engineering Mechanics – Dynamics 11 4
  • 115. UNIT-II KINETICS OF PARTICLE Introduction, definitions of matter, body, particle, mass, weight, inertia, momentum, Newton’s law of motion, relation between force and mass, motion of a particle in rectangular coordinates, D’Alembert’s principle, motion of lift, motion of body on an inclined plane, motion of connected bodies. 1/27/2017 115 Engineering Mechanics – Dynamics 11 5 Engineering Mechanics – Dynamics
  • 116. Newton’s Second Law of Motion • If the resultant force acting on a particle is not zero, the particle will have an acceleration proportional to the magnitude of resultant and in the direction of the resultant. F  ma • If particle is subjected to several forces: F  ma • We must use a Newtonian frame of reference, i.e., one that is not accelerating or rotating. • If no force acts on particle, particle will not accelerate, i.e., it will remain stationary or continue on a straight line at constant velocity. Engineering Mechanics – Dynamics 116 11 6
  • 117. Linear Momentum of a Particle dt  d mv  d L dt dt F  ma  m dv L mv Linear momentum F  L Sum of forces = rate of change of linear momentum If F  0 linear momentum is constant Principle of conservation of linear momentum Engineering Mechanics – Dynamics 117 11 7
  • 118. Equations of Motion • Newton’s second law   F  m a  • Convenient to resolve into components: x y z z     a i  a j  a k  Fz maz  Fz mz  Fy  may  Fy  my  Fx  max  Fx  mx Fxi   Fy  j  F k  m • For tangential and normal components: t dv v2 dt F  m F t mat  F n man F n  m  Engineering Mechanics – Dynamics 118 11 8
  • 119. Dynamic Equilibrium ma • Alternate expression of Newton’s law: F  ma  0 • If we include inertia vector, the system of forces acting on particle is equivalent to zero. The particle is said to be in dynamic equilibrium. • Inertia vectors are often called inertia forces as they measure the resistance that particles offer to changes in motion. inertia vector Engineering Mechanics – Dynamics 119 11 9
  • 120. Sample Problem 1 An 80-kg block rests on a horizontal plane. Find the magnitude of the force P required to give the block an acceleration of 2.5 m/s2 to the right. The coefficient of kinetic friction between the block and plane is mk = 0.25. Engineering Mechanics – Dynamics 120 SOLUTION: • Draw a free body diagram • Apply Newton’s law. Resolve into rectangular components 12 0
  • 121. W  mg  809.81 785N F  k N  0.25N Sample Problem 12.2 Fx  ma: Pcos30  0.25N  802.5  200 Fy  0: N  Psin30  785 Pcos30  0.25Psin30  785 200 Pcos30 Psin30 N  Psin30  785  0 Solve for P and N 12N 1 P  534.7 N N 1052.4 1/27/2017 Engineering Mechanics – Dynamics 12 1 Engineering Mechanics – Dynamics
  • 122. 122 Sample Problem 12.3 The two blocks shown start from rest. The horizontal plane and the pulley are frictionless, and the pulley is assumed to be of negligible mass. Determine the acceleration of each block and the tension in the1 / c2 7 o/ 2 r0 1 d7 . Engineering Mechanics – Dynamics 12 2 Engineering Mechanics – Dynamics
  • 123. Fx  mAaA Fy  mBaB O x y Sample Problem 2 • Kinematic relationship: If A moves xAto the right, B moves down 0.5 xA 1 1 B 2 A B 2 A x  x a  a Draw free body diagrams & apply Newton’s law: Fy  mCaC 2940-300aB  2T1  0 T1  100aA mB g  T2 mBaB 3009.81T2  300aB T2  2940-300aB T2  2T1  0 2940-300aB  200aA  0 2940-300aB  2 200aB  0 B a  4.2 m/ s2 A a  8.4 m/s2 T1 840 N Engineering Mechanics – Dynamics 123 T2 1680 N 12 3
  • 124. Sample Problem 3 The 12-lb block B starts from rest and slides on the 30-lb wedge A, which is supported by a horizontal surface. Neglecting friction, determine (a) the acceleration of the wedge, and (b) the acceleration of the block relative to the wedge. Engineering Mechanics – Dynamics 124 Block Wedge 12 4
  • 125. 125 N1 WBcosq WBsinq N1 aBn aBt WB 1 N cosq WB sin  mBaBt 32.2 Bt Bt 120.5  12 a  a 16.1 ft / s2 aA 1 32.2 A 0.5N  30 a N1 sin  mAaA N1 cos WA N2 N1 WB cos  mBaBn But aBn  aA sin Same normal acceleration (to maintain contact) N1 WB cos  mBaA sin 1 32.2 A N 10.39   120.5 a a 5.08 ft / s2 a  2.54 ft /s2 Draw free body diagrams for block & wedge N1sinq 1/27/A 2017 EngineerBinngMechanics – Dynamics 12 5 Engineering Mechanics – Dynamics
  • 126. N1 aBn aBt WBcosq WBsinq N1 WB 1 N cosq N1sinq Bx Bt Bn a  a cos  a aA By Bt Bn a  a sin  a sin  12.67 ft /s2 cos  10.25 ft /s2 aB / A  aB  aA aB / A  12.67i 10.25 j  5.08i  17.75i 10.25 j 30° 20.5 Engineering Mechanics – Dynamics 126 12 6
  • 127. Sample Problem 4 The bob of a 2-m pendulum describes an arc of a circle in a vertical plane. If the tension in the cord is 2.5 times the weight of the bob for the position shown, find the velocity and acceleration of the bob in that position. Engineering Mechanics – Dynamics 127 12 7
  • 128. Sample Problem 5 Resolve into tangential and normal components:  Ft  mat : at  g sin 30 mg sin30  mat at  4.9 m s2  Fn  man : 2.5mg  mg cos30  man an  g2.5  cos30 an  16.03m s2 • Solve for velocity in terms of normalacceleration. 2 an  2 m 16.03m s  v2 an v      v  5.66 ms mgsin30 Engineering Mechanics – Dynamics 128 mgcos30 12 8
  • 129. Sample Problem 6 Determine the rated speed of a highway curve of radius  = 400 ft banked through an angle  = 18o. The rated speed of a banked highway curve is the speed at which a car should travel if no lateral friction force is to be exerted at its wheels. Engineering Mechanics – Dynamics 129 SOLUTION: • The car travels in a horizontal circular path with a normal component of acceleration directed toward the center of the path.The forces acting on the car are its weight and a normal reaction from the road surface. • Resolve the equation of motion for the car into vertical and normal components. • Solve for the vehicle speed. 12 9
  • 130. Sample Problem 7 SOLUTION: • The car travels in a horizontal circular path with a normal component of acceleration directed toward the center of the path.The forces acting on the car are its weight and a normal reaction from the road surface. • Resolve the equation of motion for the car into vertical and normal components.  Fy  0: W cos R  R cos W  0  Fn  man : W v2 g  W cos g sin  R sin  W an • Solve for the vehicle speed. v2  gtan  32.2ft s2 400fttan18 v  64.7 ft s  44.1mi h Engineering Mechanics – Dynamics 130 13 0
  • 131. Derivative of angular momentum with respect to time: HO  r  mv  r  mv  v  mv  r  ma  r F  MO Sum of moments about O = rate of change of angular momentum L mv Angular Momentum From before, linear momentum: Now angular momentum is defined as the moment of momentum HO  r  mv HO is a vector perpendicular to the plane containing r and mv Resolving into radial & transverse components: 2 O  H  mv r  mr  about O Moment of F Engineering Mechanics – Dynamics 131 13 1
  • 132. Equations of Motion in Radial & Transverse Components F  ma  mr2r Engineering Mechanics – Dynamics 132 Fr  mar  mr r2 13 2
  • 133. Central Force When force acting on particle is directed toward or away from a fixed point O, the particle is said to be moving under a central force. O = center of force Since line of action of the central force passes through O: MO  HO  0 r  mv HO  constant Engineering Mechanics – Dynamics 133 13 3
  • 134. Sample Problem 8 A block B of mass m can slide freely on a frictionless arm OA which rotates in a horizontal plane at a constant rate0. Engineering Mechanics – Dynamics 134 Knowing that B is released at a distance r0 from O, express as a function ofr a) the component vr of the velocity ofB along OA, and b) the magnitude of the horizontal force exerted on B by the arm OA. SOLUTION: • Write the radial and transverse equations of motion for the block. • Integrate the radial equation to find an expression for the radial velocity. • Substitute known information into the transverse equation to find an expression for the force on the block. 13 4
  • 135. Sample Problem 8 Write radial and transverse equationsof motion: r r F  m a F   m a r vr  dvr  dvr dr  vr dvr   2 2 2 2 0 r 0 v  r r   1 2 2 2 2 0 0 F  2m r  r 0  mr  r2  F  mr  2r  r  r2 dt dr dt dr But vr r 2 r r dv dr r  v 2 r r r dr  v dv r o r 2 dr vr dvr  vr  0  ro   1 2 2 2 0 r 0 v  r  r Engineering Mechanics – Dynamics 135 13 5
  • 136. UNIT-III IMPULSE AND MOMENTUM,VIRTUAL WORK Impulse and momentum: Introduction; Impact, momentum, impulse, impulsive forces, units, law of conservation of momentum, Newton’s law of collision of elastic bodies. Coefficient of restitution, recoil of gun, impulse momentum equation; Virtual work: Introduction, principle of virtual work, applications, beams, lifting machines, simple framed structures. 1/27/2017 136 Engineering Mechanics – Dynamics 13 6 Engineering Mechanics – Dynamics
  • 137. Impulse = Momentum Consider Newton’s 2nd Law and the definition of acceleration Ns Kg x m/s Momentum is defined as “Inertia in Motion” Units of Impulse: Units of Momentum: 1/27/2017 137 Engineering Mechanics – Dynamics 13 7 Engineering Mechanics – Dynamics
  • 138. Impulse – Momentum Theorem Ft  mv IMPULSE CHANGE IN MOMENTUM This theorem reveals some interesting relationships such as the INVERSE relationship t Engineering Mechanics – Dynamics 138 TIMF E between F O R mC E a vn d 
  • 139. Impulse – Momentum Relationships Engineering Mechanics – Dynamics 139
  • 140. Impulse – Momentum Relationships fT mV Constant Since TIME is directly related to the VELOCITY when the force and mass are constant, the LONGER the cannonball is in the barrel the greater the velocity. Also, you could say that the force acts over a larger ent, thus there is 1/27/2017 140 Engineering Me c h da n iic ss p –D lay n ca m ei c ms 14 0 Engineering Mechanics – Dynamics
  • 141. How about a collision? Consider 2 objects speeding toward each other. When they collide...... Due to Newton’s 3rd Law the FORCE they exert on each other are EQUAL and OPPOSITE. The TIMES of impact are also equal. Therefore, the IMPULSES of the 2 objects colliding are also EQUAL 2 1 J1  J2 (Ft)  (Ft) t1  t2 F1 F2 1/27/2017 141 Engineering Mechanics – Dynamics 14 1 Engineering Mechanics – Dynamics
  • 142. How about a collision? If the Impulses are equal then the also equal! 1 J2 m1v1m2v2 m1(v1 vo1)  m2 (v2 vo2 ) m1v1  m1vo1  m2v2 m2vo2 p1 p2 J  M  OMENTUMSare  pbefore  pafter m1vo1  m2vo2  m1v1m2v2 Engineering Mechanics – Dynamics 142
  • 143. Momentum is conserved! The Law of Conservation of Momentum: “In the absence of an external force (gravity, friction), the total momentum before the collision is equal to the total momentum after the collision.” po(truck)  mvo  (500)(5)  2500kg*m / s po(car)  (400)(2)  800kg*m / s po(total)  3300kg*m / s ptruck  500*3 1500kg*m / s pcar  400*4.5 1800kg*m / s ptotal  3300kg*m / s Engineering Mechanics – Dynamics 143
  • 144. Types of Collisions A situation where the objects DO NOT STICK is one type of collision Notice that in EACH case, you have TWO objects BEFORE and AFTER the collision. Engineering Mechanics – Dynamics 144
  • 145. A “no stick” type collision pbefore = pafter m1vo1  m2vo2  m1v1 m2v2 (1000)(20)  0  (1000)(v1)  (3000)(10) 10000 1000v1 v1  -10 m/s Engineering Mechanics – Dynamics 145
  • 146. Types of Collisions Another type of collision is one where the objects “STICK” together. Notice you have TWO objects before the collision and ONE object after the collision. Engineering Mechanics – Dynamics 146
  • 147. A “stick” type of collision 20000  4000vT vT  Engineering Mechanics – Dynamics 147 pbefore = pafter m1vo1  m2vo2  mTvT (1000)(20)  0  (4000)vT 5 m/s
  • 148. The “explosion” type This type is often referred to as “backwards inelastic”. Notice you have ONE object ( we treat this as a SYSTEM) before the explosion and TWO objects after the explosion. Engineering Mechanics – Dynamics 148
  • 149. Backwards Inelastic - Explosions 0  3 4v2 v2  Engineering Mechanics – Dynamics 149 Suppose we have a 4-kg rifle loaded with a 0.010 kg bullet. When the rifle is fired the bullet exits the barrel with a velocity of 300 m/s. How fast does the gun RECOIL backwards? pbefore = pafter mTvT  m1v1 m2v2 (4.010)(0)  (0.010)(300)  (4)(v2 ) -0.75 m/s
  • 150. Collision Summary m1v01  m2v02  m1v1m2v2 m1v01  m2v02  mtotalvtotal mtotalvo(total)  m1v1  m2v2 Sometimes objects stick together or blow apart. In this case, momentum is ALWAYS conserved.  pbefore  pafter When 2 objects collide and DON’ When 2 objects collide and stick to When 1 object breaks into 2 objec Engineering Mechanics – Dynamics 150 Elastic Collision = Kinetic Energy is Conserved Inelastic Collision = Kinetic Energy is NOT Conserved
  • 151. Elastic Collision KEcar (Before)  1 2 mv  0.5(1000)(20)  200,000J 2 2 KEtruck (After )  0.5(3000)(10) 150,000J 2 KEcar (After )  0.5(1000)(10)  50,000J 2 Since KINETIC ENERGY is conserved during the collision we call this an ELASTIC COLLISION. Engineering Mechanics – Dynamics 151
  • 152. Inelastic Collision KEcar (Before)  1 2 mv  0.5(1000)(20)  200,000J 2 2 KEtruck/car (After)  0.5(4000)(5)  50,000J 2 Since KINETIC ENERGY was NOT conserved during the collision we call this an INELASTIC COLLISION. Engineering Mechanics – Dynamics 152
  • 153. Examp Gl ra e nny (m=80 kg) whizzes around the rink with a velocity of 6 m/s. She suddenly collides with Ambrose (m=40 kg) who is at rest directly in her path. Rather than knock him over, she picks him up and continues in motion without "braking." Determine the velocity of Granny and Ambrose. How many objects do I have before the collision? Engineering Mechanics – Dynamics 153 2   b a vT  p  p m1vo1  m2vo2  mTvT How many objec1tsdo I have after the c (o 8l l i 0s i )o (n 6?)  (40)(0) 120vT 4 m/s
  • 154. Collisions in 2 Dimensions The figure to the left shows a collision between two pucks on an air hockey table. Puck A has a mass of 0.025-kg and is moving along the x-axis with a velocity of +5.5 m/s. It makes a collision with puck B, which has a mass of 0.050-kg and is initially at rest. The collision is NOT head on. After the collision, the two pucks fly vA Engineering Mechanics – Dynamics 154 A v sin vAcos vBcos vB vBsin apart with angles shown in the drawing. Calculate the speeds of the pucks after the collision.
  • 155. Collisions in 2 dimensions  pox  px mAvoxA  mBvoxB  mAvxA  mBvxB (0.025)(5.5) 0  (.025)(vA cos65) (.050)(vB cos37) vA vB vAcos A v sin B v cos B v sin 0  (0.025)(vA sin 65)  (0.050)(vB sin37) 0.0300vB 0.0227vA vB  0.757vA 0  mAvyA  mBvyB 0.1375  0.0106vA 0.040vB  poy  py Engineering Mechanics – Dynamics 155
  • 156. Collisions in 2 dimensions 0.1375  0.0106vA 0.040vB vB  0 vB. 7 0.7 5 577 (2.8 v 4) A  2.15m/ s 0.1375  0.0106vA (0.050)(0.757vA ) 0.1375  0.0106vA  0.03785vA 0.1375  0.04845vA vA  2.84m / s 1/27/2017 156 Engineering Mechanics – Dynamics 15 6 Engineering Mechanics – Dynamics
  • 157. WORK ENERGY METHOD UNIT -IV 1/27/2017 Engineering Mechanics – Dynamics 157 Work energy method: Law of conservation of energy, application of work energy, method to particle motion and connected system, work energy applied toconnected systems, work energy applied to fixed axis rotation. 15 7 Engineering Mechanics – Dynamics
  • 158. Law of Conservation of Energy • What you put in is what you get out • Total energy is conserved 15 8 Engineering Mechanics – Dynamics
  • 159. Practical Applications  Gasoline converts to energy which moves the car  A battery converts stored chemical energy to electrical energy  Dams convert the kinetic energy of falling water into electrical energy 15 9 Engineering Mechanics – Dynamics
  • 160. CanYouThink of Other Examples? 16 0 Engineering Mechanics – Dynamics
  • 161. Conservation of Mechanical Energy 1 mv2  mgh  E 2 Total Energy Potential Energy Kinetic Energy m = mass v = velocity g = gravitational acceleration h = height ILYA,did you know thateven though it wasa bumpy ride, our energy remained constant! 16 1 Engineering Mechanics – Dynamics
  • 162. Example of Conservation of Mechanical Energy 2 1 m v 2  m g h  E Constant 16 2 Engineering Mechanics – Dynamics
  • 165. Yet Another Example 16 5 Engineering Mechanics – Dynamics
  • 167. MECHANICAL VIBRATIONS UNIT -V 1/27/2017 Engineering Mechanics – Dynamics 167 Definitions and concepts, simple harmonic motion, free vibrations, simple and compound pendulum, torsion pendulum, free vibrations without damping, general cases. 16 7 Engineering Mechanics – Dynamics
  • 168. Simple Harmonic Motion • Harmonic Motion is any motion that repeats itself. • Examples of Harmonic Motion. Engineering Mechanics – Dynamics 168
  • 169. Engineering Mechanics – Dynamics 169
  • 170. Engineering Mechanics – Dynamics 170
  • 171. Engineering Mechanics – Dynamics 171
  • 172. Engineering Mechanics – Dynamics 172
  • 173. Engineering Mechanics – Dynamics 173 Period Displacement Time for one oscillation Frequency Number of oscillations in one second Amplitude Maximum displacement Distance from equilibrium
  • 174. • Simple harmonic motion is a special type of harmonic motion. • Consider a mass on a spring. • The cart is in equilibrium, because the total force is zero. • The acceleration is also (this doesn’t meazneriots.stationary) Engineering Mechanics – Dynamics 174
  • 175. Lets look at the forces force dispt = -A Engineering Mechanics – Dynamics 175
  • 176. force dispt = -A/2 Engineering Mechanics – Dynamics 176
  • 177. Force = 0 dispt = 0 Engineering Mechanics – Dynamics 177
  • 178. force dispt = A/2 Engineering Mechanics – Dynamics 178
  • 179. force dispt = A Engineering Mechanics – Dynamics 179
  • 180. force dispt = A • Notice that as the displacement increases, the restoring force increases. • Notice that the restoring force is always in the opposite direction to the displacement Engineering Mechanics – Dynamics 180
  • 181. Now we’ll look at the acceleration dispt = -A acceleration force Engineering Mechanics – Dynamics 181
  • 182. dispt = -A/2 acceleration force Engineering Mechanics – Dynamics 182
  • 183. Force = 0 dispt = 0 Engineering Mechanics – Dynamics 183 Acceleration =0
  • 184. dispt = A/2 acceleration force Engineering Mechanics – Dynamics 184
  • 185. dispt = A acceleration force Engineering Mechanics – Dynamics 185
  • 186. acceleration dispt = A • Notice that as the displacement increases, the acceleration increases. • Notice that the acceleration is always in the opposite direction to the displacement Engineering Mechanics – Dynamics 186
  • 187. Engineering Mechanics – Dynamics 187 • The relation between acceleration and displacement is ….. • Acceleration is proportional to displacement • Acceleration is in opposite direction to displacement. a   constant  y a   2  y T   2
  • 189. Acceleration/position graph acceleration Engineering Mechanics – Dynamics 189 position y  mx  c a  mx a 2 x
  • 190. Force/position graph force Engineering Mechanics – Dynamics 190 position a 2 x F  ma  (m2 )x
  • 191. Engineering Mechanics – Dynamics 191 Graphs of SHM • We have looked at simple harmonic motion as a function of position. • Now we’ll look at it as a function of time
  • 192. • raphs Engineering Mechanics – Dynamics 192
  • 193. graphical treatment 1/27/2017 Engineering Mechanics – Dynamics 19 3 Engineering Mechanics – Dynamics
  • 195. Engineering Mechanics – Dynamics 195 •
  • 197. Reference Circle Red ball moves in SHM horizontally Blue ball moves in a circle Both have same period Amplitude of SHM equals radius of circle Both have same horizontal displacement Engineering Mechanics – Dynamics 197
  • 198. Tofind the position of a swing at a certain time. The period is 4.0s The amplitude is 2.0m Where is the swing 2.0s after release? Engineering Mechanics – Dynamics 198
  • 199. The period is 4.0s The amplitude is 2.0m Where is the swing 1.0s after release? Engineering Mechanics – Dynamics 199
  • 200. Where is the swing 0.5s after release? 4.0 Convert time to angle (1period = 360o) 0.5 3600  450 450 2.0m x 2 x cos450  0.50s  450 Engineering Mechanics – Dynamics 200
  • 201. Where is the swing 2.5s after release? Convert time to angle (1period = 360o) 4.0 2.5 3600  2250 450 2.0m x 2 cos450  x 2.50s  2250 Engineering Mechanics – Dynamics 201
  • 202. How long does it take to go 1.4m from the start? (1) Calculate angle (2) Convert angle to time (1period = 360o)   600 2.0m 2 cos  0.59 600  60 of a period 360 600  1 6  4.0s 1.41m 0.59m Engineering Mechanics – Dynamics 202
  • 203. • The top of the sky tower is oscillating with an amplitude of 2.0 m and a period of 14 s. • How long is it more than 0.80m from equilibrium each cycle? • What is the horizontal acceleration when the displacement is maximum? Engineering Mechanics – Dynamics 203
  • 204. Equations 1 y  Asin   t y  Asint v  Acost a  A2 sint Engineering Mechanics – Dynamics 204
  • 205. Equations 2 y  Acost v  Asint a  A2 cost Engineering Mechanics – Dynamics 205
  • 206. Equations 3 y  Acost v  Asint a  A2 cost Engineering Mechanics – Dynamics 206
  • 207. Engineering Mechanics – Dynamics 207 y  Asint v  Acost a  A2 sint ymax  A vmax  A max a  A2 a  2 Asint  2 y a  2 y
  • 208. Anisha is on a swing. Kate pulls her back 2.0m and lets her go. Her period is 4.0s. (a) Calculate her maximum speed. (where is it?) (b) Calculate her maximum acceleration. (where is it?) Engineering Mechanics – Dynamics 208
  • 209. Anisha is on a swing. Kate pulls her back 2.0m and lets her go. Her period is 4.0s. (a) Calculate her speed 0.50s after being released (b) Calculate her acceleration 0.50s after being released Engineering Mechanics – Dynamics 209
  • 210. Engineering Mechanics – Dynamics 210 • Nik is bungee jumping. In one oscillation he travels 12 m and it takes 8.0s. • Tahi starts videoing him as he passes through the mid position moving UP. (a) Calculate his velocity 1.0s after the video starts (b) Calculate his acceleration 2.0s after the video starts.
  • 211. Engineering Mechanics – Dynamics 211 Mass on a Spring • As the mass increases, the period… increases • As the spring stiffness increases the period … increases
  • 212. Effect of mass: decreases • As the acceleration decreases the period … increases A larger mass means a longer period. (assuming constant force) m • As the mass increases, the acceleration… Engineering Mechanics – Dynamics 212 a  F
  • 213. Effect of spring stiffness: • As the stiffness increases, the restoring force… • As the acceleration increases the period … A stiffer spring means a shorter period. m Engineering Mechanics – Dynamics 213 a  F increases (assuming same displacement) • As the restoring force increases the acceleration … increases decreases F  kx
  • 214. m Engineering Mechanics – Dynamics 214 k T  2 Summary • mass ↑ acceln↓ period ↑ • stiffness ↑ force ↑ acceln ↑ period eq↓ uation
  • 215. Extension …..derivation of the equation: consider a mass on a spring. a  F F  -kx m m a  kx a   k x (i.e. m a x) m a  k x a 2 x k  2  ( 2 )2 m Engineering Mechanics – Dynamics 215 m T k m T k  2 T  2
  • 216. energy of motion 1/27/2017 Engineering Mechanics – Dynamics 21 6 Engineering Mechanics – Dynamics
  • 217. Simple Pendulum • This is where all the mass is concentrated in one point. Engineering Mechanics – Dynamics 217
  • 218. What provides the restoring force? the restoring force is the Tension plus Gravity Engineering Mechanics – Dynamics 218
  • 219. Why is the motion SHM? As the displacement increases, the restoring force. increases. the restoring force is always towards equilibrium Engineering Mechanics – Dynamics 219
  • 220. Engineering Mechanics – Dynamics 220
  • 221. Engineering Mechanics – Dynamics 221 • This next bit is very important
  • 222. Why does length affect period? For the same amplitude, if the pendulum is shorter, the angle of the string to the vertical is greater. The restoring force is greater. The acceleration is greater So the period is shorter Engineering Mechanics – Dynamics 222
  • 223. period of a pendulum l g T  2 How is lengthmeasured? Engineering Mechanics – Dynamics 223
  • 224. As the pendulum expands down, Engineering Mechanics – Dynamics 224 The mercury expands up This keeps the center of mass in the same place Same length same period.
  • 225. Engineering Mechanics – Dynamics 225 Energy of SHM
  • 226. energy of motion 1/27/2017 Engineering Mechanics – Dynamics 22 6 Engineering Mechanics – Dynamics
  • 227. a sprung system 1/27/2017 Engineering Mechanics – Dynamics 227 22 7 Engineering Mechanics – Dynamics
  • 228. dampers 1/27/2017 Engineering Mechanics – Dynamics 228 22 8 Engineering Mechanics – Dynamics
  • 229. energy dissipation plunger hydraulic oil dividing piston high pressure nitrogen gas 1/27/2017 Engineering Mechanics – Dynamics 229 22 9 Engineering Mechanics – Dynamics
  • 230. bridge dampers 1/27/2017 Engineering Mechanics – Dynamics 230 23 0 Engineering Mechanics – Dynamics
  • 231. Resonance 1/27/2017 Engineering Mechanics – Dynamics 231  Any elastic system has a natural period of oscillation.  If bursts of energy (pushes) are supplied at the natural period, the amplitude will increase.  This is called resonance 23 1 Engineering Mechanics – Dynamics
  • 232. 1/27/2017 Engineering Mechanics – Dynamics 232 23 2 Engineering Mechanics – Dynamics
  • 233. Examples of resonance 1/27/2017 Engineering Mechanics – Dynamics 233 23 3 Engineering Mechanics – Dynamics
  • 234.  The glass has a natural frequency of vibration.  If you tap the glass, it vibrates at the natural frequency causing sound.  If you put energy in at the natural frequency,the amplitude increases. This is resonance.  If the amplitude gets high enough,the glass can break. 1/27/2017 Engineering Mechanics – Dynamics 234 23 4 Engineering Mechanics – Dynamics
  • 235. Bay of Fundy 1/27/2017 Engineering Mechanics – Dynamics 235 23 5 Engineering Mechanics – Dynamics
  • 236. Bay of Fundy 1/27/2017 Engineering Mechanics – Dynamics 236 The period of the tide is 12 hours. The time for a wave to move up the bay and back is 12 hours 23 6 Engineering Mechanics – Dynamics
  • 237. What is vibration?  Vibrations are oscillations of a system about an equilbrium position. 23 7 Engineering Mechanics – Dynamics
  • 238. Vibration… It is also an everyday phenomenon we meet on everyday life 23 8 Engineering Mechanics – Dynamics
  • 239. Vibration … Useful Vibration Harmful vibration Noise Destruction Compressor Ultrasonic cleaning Testing Wear Fatigue 23 9 Engineering Mechanics – Dynamics
  • 240. Vibration parameters All mechanical systems can be modeled by containing three basic components: spring, damper, mass When these components are subjected to constant force, they react with a constant displacement, velocity and acceleration 24 0 Engineering Mechanics – Dynamics
  • 241. Free vibration Equilibrium pos.  When a system is initially disturbed by a displacement, velocity or acceleration, the system begins to vibrate with a constant amplitude and frequency depend on its stiffness and mass.  This frequency is called as natural frequency,and the form of the vibration is called as mode shapes 24 1 Engineering Mechanics – Dynamics
  • 242. ForcedVibration If an external force applied to a system, the system will follow the force with the same frequency. However, when the force frequency is increased to the system’s natural frequency, amplitudes will dangerously increase in this region. This phenomenon called as “Resonance” ’ 24 2 Engineering Mechanics – Dynamics
  • 243. Bridge collapse: http://www.youtube.com/watch?v=j-zczJXSxnw Hellicopter resonance: http://www.youtube.com/watch?v=0FeXjhUEXlc Resonance vibration test: http://www.youtube.com/watch?v=LV_UuzEznHs Flutter (Aeordynamically induced vibration) : http://www.youtube.com/watch?v=OhwLojNerMU Watch these … 24 3 Engineering Mechanics – Dynamics
  • 244. Lumped (Rigid) Modelling Numerical Modelling Element-based methods (FEM, BEM) Statistical and Energy-based methods (SEA, EFA, etc.) Modelling of vibrating systems 24 4 Engineering Mechanics – Dynamics
  • 245. •Mathematical modeling of a physical system requires the selection of a set of variables that describes the behavior of the system. •The number of degrees of freedom for a system is the number of kinematically independent variables necessary to completely describe the motion of every particle in the system DOF=1 Single degree of freedom (SDOF) DOF=2 Multi degree of freedom (MDOF) Degree of Freedom (DOF) 24 5 Engineering Mechanics – Dynamics
  • 246. Equivalent model of systems Example 1: Example 2: SDOF DOF=1 MDOF DOF=2 24 6 Engineering Mechanics – Dynamics
  • 247. Equivalent model of systems Example 3: SDOF MDOF DOF=2 DOF= 3 if body 1 has no rotation DOF= b4odiyf1body1has rotation 24 7 Engineering Mechanics – Dynamics
  • 248. SDOF systems  Helical springs F: Force, D: Diameter, G: Shear modulus of the rod, Shear stress: Stiffness coefficient: N: Number of turns, r : Radius  Springs in combinations: Parallel combination Series combination 24 8 Engineering Mechanics – Dynamics
  • 249. Elastic elements as springs 24 9 Engineering Mechanics – Dynamics
  • 250. Moment of Inertia 25 0 Engineering Mechanics – Dynamics
  • 251. What are the equivalent stiffnesses? 25 1 Engineering Mechanics – Dynamics