VECTOR MECHANICS FOR ENGINEERS:
DYNAMICS
DYNAMICS
Tenth
Tenth
Edition
Edition
Ferdinand P. Beer
Ferdinand P. Beer
E. Russell Johnston, Jr.
E. Russell Johnston, Jr.
Phillip J. Cornwell
Phillip J. Cornwell
Lecture Notes:
Lecture Notes:
Brian P. Self
Brian P. Self
California Polytechnic State University
California Polytechnic State University
CHAPTER
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12
Kinetics of Particles:
Newton’s Second Law
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Contents
12 - 2
Introduction
Newton’s Second Law of
Motion
Linear Momentum of a Particle
Systems of Units
Equations of Motion
Dynamic Equilibrium
Sample Problem 12.1
Sample Problem 12.3
Sample Problem 12.4
Sample Problem 12.5
Sample Problem 12.6
Angular Momentum of a Particle
Equations of Motion in Radial &
Transverse Components
Conservation of Angular Momentum
Newton’s Law of Gravitation
Sample Problem 12.7
Sample Problem 12.8
Trajectory of a Particle Under a
Central Force
Application to Space Mechanics
Sample Problem 12.9
Kepler’s Laws of Planetary Motion
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Kinetics of Particles
2 - 3
We must analyze all of the forces
acting on the wheelchair in order
to design a good ramp
High swing velocities can
result in large forces on a
swing chain or rope, causing
it to break.
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Introduction
12 - 4
• Newton’s Second Law of Motion
m
 
F a
• 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.
• Must be expressed with respect to a Newtonian (or inertial)
frame of reference, i.e., one that is not accelerating or rotating.
• This form of the equation is for a constant mass system
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Linear Momentum of a Particle
12 - 5
• Replacing the acceleration by the derivative of the velocity
yields
 
particle
the
of
momentum
linear





L
dt
L
d
v
m
dt
d
dt
v
d
m
F





• Linear Momentum Conservation Principle:
If the resultant force on a particle is zero, the linear momentum
of the particle remains constant in both magnitude and direction.
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Systems of Units
12 - 6
• Of the units for the four primary dimensions (force,
mass, length, and time), three may be chosen arbitrarily.
The fourth must be compatible with Newton’s 2nd Law.
• International System of Units (SI Units): base units are
the units of length (m), mass (kg), and time (second).
The unit of force is derived,
  2
2
s
m
kg
1
s
m
1
kg
1
N
1









• U.S. Customary Units: base units are the units of force
(lb), length (m), and time (second). The unit of mass is
derived,
ft
s
lb
1
s
ft
1
lb
1
slug
1
s
ft
32.2
lb
1
lbm
1
2
2
2




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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
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Equations of Motion
12 - 7
• Newton’s second law a
m
F




• Can use scalar component equations, e.g., for
rectangular components,
   
z
m
F
y
m
F
x
m
F
ma
F
ma
F
ma
F
k
a
j
a
i
a
m
k
F
j
F
i
F
z
y
x
z
z
y
y
x
x
z
y
x
z
y
x






























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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
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Dynamic Equilibrium
12 - 8
• Alternate expression of Newton’s second law,
ector
inertial v
a
m
a
m
F 0








• With the inclusion of the inertial vector, the system
of forces acting on the particle is equivalent to
zero. The particle is in dynamic equilibrium.
• Methods developed for particles in static
equilibrium may be applied, e.g., coplanar forces
may be represented with a closed vector polygon.
• Inertia vectors are often called inertial forces as
they measure the resistance that particles offer to
changes in motion, i.e., changes in speed or
direction.
• Inertial forces may be conceptually useful but are
not like the contact and gravitational forces found
in statics.
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Free Body Diagrams and Kinetic Diagrams
12 - 9
The free body diagram is the same as you have done in statics; we
will add the kinetic diagram in our dynamic analysis.
2. Draw your axis system (e.g., Cartesian, polar, path)
3. Add in applied forces (e.g., weight, 225 lb pulling force)
4. Replace supports with forces (e.g., normal force)
1. Isolate the body of interest (free body)
5. Draw appropriate dimensions (usually angles for particles)
x y
225 N
Ff
N
mg
25o
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
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Free Body Diagrams and Kinetic Diagrams
12 - 10
Put the inertial terms for the body of interest on the kinetic diagram.
2. Draw in the mass times acceleration of the particle; if unknown,
do this in the positive direction according to your chosen axes
1. Isolate the body of interest (free body)
x y
225 N
Ff
N
mg
25o
may
max
m
 
F a

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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
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Free Body Diagrams and Kinetic Diagrams
2 - 11
Draw the FBD and KD for block A (note that the
massless, frictionless pulleys are attached to block A
and should be included in the system).
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
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Free Body Diagrams and Kinetic Diagrams
2 - 12
1. Isolate body
2. Axes
3. Applied forces
4. Replace supports with forces
5. Dimensions (already drawn)
x
y
mg
Ff-1
N1
T
T
T
T
T
Ff-B
NB
may = 0
max
6. Kinetic diagram
=
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Free Body Diagrams and Kinetic Diagrams
2 - 13
Draw the FBD and KD for the collar B. Assume
there is friction acting between the rod and collar,
motion is in the vertical plane, and  is increasing
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Free Body Diagrams and Kinetic Diagrams
2 - 14
1. Isolate body
2. Axes
3. Applied forces
4. Replace supports with forces
5. Dimensions
6. Kinetic diagram
mg
Ff
N
mar
ma
e er
=


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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
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Sample Problem 12.1
12 - 15
A 200-lb block rests on a horizontal
plane. Find the magnitude of the force
P required to give the block an
acceleration of 10 ft/s2
to the right. The
coefficient of kinetic friction between
the block and plane is k0.25.
SOLUTION:
• Resolve the equation of motion for the
block into two rectangular component
equations.
• Unknowns consist of the applied force
P and the normal reaction N from the
plane. The two equations may be
solved for these unknowns.
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
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Sample Problem 12.1
12 - 16
N
N
F
g
W
m
k
25
.
0
ft
s
lb
21
.
6
s
ft
2
.
32
lb
200
2
2







x
y
O
SOLUTION:
• Resolve the equation of motion for the block
into two rectangular component equations.
:
ma
Fx 

  
lb
1
.
62
s
ft
10
ft
s
lb
21
.
6
25
.
0
30
cos 2
2




 N
P
:
0

 y
F
0
lb
200
30
sin 


 P
N
• Unknowns consist of the applied force P and
the normal reaction N from the plane. The two
equations may be solved for these unknowns.
  lb
1
.
62
lb
200
30
sin
25
.
0
30
cos
lb
200
30
sin








P
P
P
N
lb
151

P
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Sample Problem 12.3
12 - 17
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 the cord.
SOLUTION:
• Write the kinematic relationships for the
dependent motions and accelerations of
the blocks.
• Write the equations of motion for the
blocks and pulley.
• Combine the kinematic relationships
with the equations of motion to solve for
the accelerations and cord tension.
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
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Sample Problem 12.3
12 - 18
• Write equations of motion for blocks and pulley.
:
A
A
x a
m
F 

  A
a
T kg
100
1 
:
B
B
y a
m
F 

    
  B
B
B
B
B
a
T
a
T
a
m
T
g
m
kg
300
-
N
2940
kg
300
s
m
81
.
9
kg
300
2
2
2
2





:
0


 C
C
y a
m
F
0
2 1
2 
 T
T
SOLUTION:
• Write the kinematic relationships for the dependent
motions and accelerations of the blocks.
A
B
A
B a
a
x
y 2
1
2
1 

x
y
O
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
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Sample Problem 12.3
12 - 19
 
N
1680
2
N
840
kg
100
s
m
20
.
4
s
m
40
.
8
1
2
1
2
2
1
2







T
T
a
T
a
a
a
A
A
B
A
• Combine kinematic relationships with equations of
motion to solve for accelerations and cord tension.
A
B
A
B a
a
x
y 2
1
2
1 

  A
a
T kg
100
1 
 
  
A
B
a
a
T
2
1
2
kg
300
-
N
2940
kg
300
-
N
2940


    0
kg
100
2
kg
150
N
2940
0
2 1
2





A
A a
a
T
T
x
y
O
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Sample Problem 12.4
12 - 20
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.
SOLUTION:
• The block is constrained to slide down
the wedge. Therefore, their motions are
dependent. Express the acceleration of
block as the acceleration of wedge plus
the acceleration of the block relative to
the wedge.
• Write the equations of motion for the
wedge and block.
• Solve for the accelerations.
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Sample Problem 12.4
12 - 21
SOLUTION:
• The block is constrained to slide down the
wedge. Therefore, their motions are dependent.
A
B
A
B a
a
a





• Write equations of motion for wedge and block.
x
y
:
A
A
x a
m
F 

  A
A
A
A
a
g
W
N
a
m
N



1
1
5
.
0
30
sin
 :
30
cos A
B
A
B
x
B
x a
a
m
a
m
F 




  









30
sin
30
cos
30
cos
30
sin
g
a
a
a
a
g
W
W
A
A
B
A
B
A
B
B
 :
30
sin 



 A
B
y
B
y a
m
a
m
F
  



 30
sin
30
cos
1 A
B
B a
g
W
W
N
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Sample Problem 12.4
12 - 22
  A
A a
g
W
N 
1
5
.
0
• Solve for the accelerations.
 
   
  
    

















30
sin
lb
12
lb
30
2
30
cos
lb
12
s
ft
2
.
32
30
sin
2
30
cos
30
sin
30
cos
2
30
sin
30
cos
2
1
A
B
A
B
A
A
B
B
A
A
A
B
B
a
W
W
gW
a
a
g
W
W
a
g
W
a
g
W
W
N
2
s
ft
07
.
5

A
a
    







30
sin
s
ft
2
.
32
30
cos
s
ft
07
.
5
30
sin
30
cos
2
2
A
B
A
A
B
a
g
a
a
2
s
ft
5
.
20

A
B
a
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Group Problem Solving
2 - 23
The two blocks shown are originally at
rest. Neglecting the masses of the pulleys
and the effect of friction in the pulleys and
between block A and the horizontal
surface, determine (a) the acceleration of
each block, (b) the tension in the cable.
SOLUTION:
• Write the kinematic relationships for the
dependent motions and accelerations of
the blocks.
• Write the equations of motion for the
blocks and pulley.
• Combine the kinematic relationships
with the equations of motion to solve for
the accelerations and cord tension.
• Draw the FBD and KD for each block
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Group Problem Solving
2 - 24
xA
yB
const nts
3 a
A B
x y L
  
3 0
A B
v v
 
3 0
A B
a a
 
3
A B
a a

SOLUTION:
• Write the kinematic relationships for the
dependent motions and accelerations of
the blocks.
This is the same problem worked last
chapter- write the constraint equation
Differentiate this twice to get the
acceleration relationship.
(1)
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Group Problem Solving
2 - 25
:
 
x A A
F m a
  A B
T m a
3 A B
T m a

y B B
F m a
 
3(3 )
B A B B B
m g m a m a
 
2
2
9.81 m/s
0.83136 m/s
30 kg
1 9
1 9
25 kg
B
A
B
g
a
m
m
  

 2
2.49 2.49 m/s
A  
a
2
3 30 kg 0.83136 m/s
T   
74.8 N
T 
• Draw the FBD and KD for each block
mAg
T
NA
maAx
mBg
2T T
maBy
• Write the equation of motion for each block
=
=
From Eq (1)
(2) (3)
3
B B B
W T m a
 
(2)
(3)
B
A
• Solve the three equations, 3 unknowns
+y
+x
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Concept Quiz
2 - 26
The three systems are released from rest. Rank the
accelerations, from highest to lowest.
a) (1) > (2) > (3)
b) (1) = (2) > (3)
c) (2) > (1) > (3)
d) (1) = (2) = (3)
e) (1) = (2) < (3)
(1) (2) (3)
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
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Kinetics: Normal and Tangential Coordinates
2 - 27
Aircraft and roller coasters can both experience large
normal forces during turns.
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
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Equations of Motion
12 - 28
• For tangential and normal components,
t t
t
F ma
dv
F m
dt




• Newton’s second law a
m
F




2
n n
n
F ma
v
F m





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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
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Sample Problem 12.5
12 - 29
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 accel-
eration of the bob in that position.
SOLUTION:
• Resolve the equation of motion for the
bob into tangential and normal
components.
• Solve the component equations for the
normal and tangential accelerations.
• Solve for the velocity in terms of the
normal acceleration.
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Sample Problem 12.5
12 - 30
SOLUTION:
• Resolve the equation of motion for the bob into
tangential and normal components.
• Solve the component equations for the normal and
tangential accelerations.
:
t
t ma
F 





30
sin
30
sin
g
a
ma
mg
t
t
2
s
m
9
.
4

t
a
:
n
n ma
F 

 






30
cos
5
.
2
30
cos
5
.
2
g
a
ma
mg
mg
n
n
2
s
m
03
.
16

n
a
• Solve for velocity in terms of normal acceleration.
  
2
2
s
m
03
.
16
m
2


 n
n a
v
v
a 

s
m
66
.
5


v
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Sample Problem 12.6
12 - 31
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.
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.
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Sample Problem 12.6
12 - 32
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.
:
0

 y
F


cos
0
cos
W
R
W
R



:
n
n ma
F 





2
sin
cos
sin
v
g
W
W
a
g
W
R n


• Solve for the vehicle speed.
   


18
tan
ft
400
s
ft
2
.
32
tan
2
2


g
v
h
mi
1
.
44
s
ft
7
.
64 

v
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Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Group Problem Solving
2 - 33
The 3-kg collar B rests on the
frictionless arm AA. The collar is
held in place by the rope attached to
drum D and rotates about O in a
horizontal plane. The linear velocity
of the collar B is increasing
according to v= 0.2 t2
where v is in
m/s and t is in sec. Find the tension
in the rope and the force of the bar on
the collar after 5 seconds if r = 0.4 m.
v SOLUTION:
• Write the equations of motion for the
collar.
• Combine the equations of motion with
kinematic relationships and solve.
• Draw the FBD and KD for the collar.
• Determine kinematics of the collar.
© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Group Problem Solving
2 - 34
SOLUTION: • Given: v= 0.2 t2
, r = 0.4 m
• Find: T and N at t = 5 sec
Draw the FBD and KD of the collar
man
T N
et
en
mat
Write the equations of motion
=
n n
F ma
  t t
F ma
 
2
v
N m


dv
T m
dt

© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Group Problem Solving
2 - 35
man
T N
et
en
mat
=
2 2
2
5
62.5 (m/s )
0.4
n
v
a

  
2
0.4 0.4(5) 2 m/s
t
dv
a t
dt
   
Kinematics : find vt, an, at
2 2
0.2 0.2(5 )=5 m/s
t
v t
 
Substitute into equations of motion
3.0(62.5)
N  3.0(2)
T 
187.5 N
N  6.0 N
T 

n n
F ma
  t t
F ma
 
© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Group Problem Solving
2 - 36
man
T N
et
en
mat
=
How would the problem
change if motion was in the
vertical plane?
mg

You would add an mg term
and would also need to
calculate 
When is the tangential force greater than the normal
force?
Only at the very beginning, when starting to accelerate.
In most applications, an >> at
© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Concept Question
2 - 37
D
B
C
A
A car is driving from A to D on the curved path shown.
The driver is doing the following at each point:
A – going at a constant speed B – stepping on the accelerator
C – stepping on the brake D – stepping on the accelerator
Draw the approximate direction of the car’s acceleration
at each point.
© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Kinetics: Radial and Transverse Coordinates
2 - 38
Hydraulic actuators and
extending robotic arms are
often analyzed using radial
and transverse coordinates.
© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Eqs of Motion in Radial & Transverse Components
12 - 39
 
 












r
r
m
ma
F
r
r
m
ma
F r
r
2
2








• Consider particle at r and , in polar coordinates,
© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Sample Problem 12.7
12 - 40
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

a) the component vr of the velocity of B
along OA, and
b) the magnitude of the horizontal force
exerted on B by the arm OA.
Knowing that B is released at a distance
r0 from O, express as a function of r
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.
© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Sample Problem 12.7
12 - 41
SOLUTION:
• Write the radial and transverse
equations of motion for the block.
:
:

 a
m
F
a
m
F r
r



  
 










r
r
m
F
r
r
m
2
0 2




• Integrate the radial equation to find an
expression for the radial velocity.

 






r
r
v
r
r
r
r
r
r
r
r
r
dr
r
dv
v
dr
r
dr
r
dv
v
dr
dv
v
dt
dr
dr
dv
dt
dv
v
r
r
0
2
0
0
2
0
2









dr
dv
v
dt
dr
dr
dv
dt
dv
v
r r
r
r
r
r 





 
2
0
2
2
0
2
r
r
vr 

• Substitute known information into the
transverse equation to find an expression
for the force on the block.
  2
1
2
0
2
2
0
2 r
r
m
F 
 
© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Group Problem Solving
2 - 42
• Write the equations of motion for the
collar.
• Combine the equations of motion with
kinematic relationships and solve.
• Draw the FBD and KD for the collar.
• Determine kinematics of the collar.
SOLUTION:
The 3-kg collar B slides on the frictionless arm AA. The arm is attached to
drum D and rotates about O in a horizontal plane at the rate where
and t are expressed in rad/s and seconds, respectively. As the arm-drum
assembly rotates, a mechanism within the drum releases the cord so that the
collar moves outward from O with a constant speed of 0.5 m/s. Knowing that
at t = 0, r = 0, determine the time at which the tension in the cord is equal to
the magnitude of the horizontal force exerted on B by arm AA.
0.75t
 
 

© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Group Problem Solving
2 - 43
mar
T N
e
er
ma
=
r r
F ma
  B
F m a
 
 
Draw the FBD and KD of the collar
Write the equations of motion
SOLUTION: • Given:
• Find: time when T = N
2
( )
T m r r
   
 ( 2 )
N m r r
 
 
 

0.75t
 

5 m/s
r 

(0) 0
r 
© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Group Problem Solving
2 - 44
3 2
: (3 kg)( 0.28125 ) m/s
r r
F ma T t
    
2
: (3 kg)(1.125 ) m/s
B
F m a N t
 
  
0 0
0.5
r t
dr dt

 
(0.5 ) m
r t

0
r 

2
(0.75 ) rad/s
0.75 rad/s
t






2 2 3 2
0 [(0.5 ) m][(0.75 ) rad/s] (0.28125 ) m/s
r
a r r t t t

    


2
2
2 [(0.5 ) m][0.75 rad/s ] 2(0.5 m/s)[(0.75 ) rad/s]
(1.125 ) m/s
a r r t t
t
  
   

 

Kinematics : find expressions for r and 
Substitute values into ar , a
Substitute into equation of motion
3
(0.84375 ) (3.375 )
t t

2
4.000
t 
2.00 s
t 
Set T = N
5 m/s
r 

© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Concept Quiz
2 - 45
Top View
e1
e2

v
The girl starts walking towards the outside of the spinning
platform, as shown in the figure. She is walking at a constant
rate with respect to the platform, and the platform rotates at a
constant rate. In which direction(s) will the forces act on her?
a) +e1 b) - e1 c) +e2 d) - e2
e) The forces are zero in the e1 and e2 directions
© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Angular Momentum of a Particle
2 - 46
Satellite orbits are analyzed using conservation
of angular momentum.
© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Eqs of Motion in Radial & Transverse Components
12 - 47
 
 












r
r
m
ma
F
r
r
m
ma
F r
r
2
2








• Consider particle at r and , in polar coordinates,
 
 
 


















r
r
m
F
r
r
r
m
mr
dt
d
F
r
mr
HO
2
2
2
2
2








• This result may also be derived from conservation
of angular momentum,
© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Angular Momentum of a Particle
12 - 48
• moment of momentum or the
angular momentum of the particle about O.


 V
m
r
HO



• Derivative of angular momentum with respect to time,













O
O
M
F
r
a
m
r
V
m
V
V
m
r
V
m
r
H














• It follows from Newton’s second law that the sum of
the moments about O of the forces acting on the
particle is equal to the rate of change of the angular
momentum of the particle about O.
z
y
x
O
mv
mv
mv
z
y
x
k
j
i
H





• is perpendicular to plane containing
O
H

V
m
r


and




2
sin
mr
v
rm
rmV
HO



© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Conservation of Angular Momentum
12 - 49
• When only 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.
• Since the line of action of the central force
passes through O, and
0
 
 O
O H
M 


constant


 O
H
V
m
r



• Position vector and motion of particle are in a
plane perpendicular to .
O
H

• Magnitude of angular momentum,
0
0
0 sin
constant
sin


V
m
r
V
rm
HO



mass
unit
momentum
angular
constant
2
2





h
r
m
H
mr
H
O
O




or
© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Conservation of Angular Momentum
12 - 50
• Radius vector OP sweeps infinitesimal area

d
r
dA 2
2
1

• Define 

 
 
2
2
1
2
2
1 r
dt
d
r
dt
dA
areal velocity
• Recall, for a body moving under a central force,
constant
2

 
r
h
• When a particle moves under a central force, its
areal velocity is constant.
© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Newton’s Law of Gravitation
12 - 51
• Gravitational force exerted by the sun on a planet or by
the earth on a satellite is an important example of
gravitational force.
• Newton’s law of universal gravitation - two particles of
mass M and m attract each other with equal and opposite
force directed along the line connecting the particles,
4
4
9
2
3
12
2
s
lb
ft
10
4
.
34
s
kg
m
10
73
.
66
n
gravitatio
of
constant










G
r
Mm
G
F
• For particle of mass m on the earth’s surface,
2
2
2
s
ft
2
.
32
s
m
81
.
9 


 g
mg
R
MG
m
W
© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Sample Problem 12.8
12 - 52
A satellite is launched in a direction
parallel to the surface of the earth
with a velocity of 18820 mi/h from
an altitude of 240 mi. Determine the
velocity of the satellite as it reaches it
maximum altitude of 2340 mi. The
radius of the earth is 3960 mi.
SOLUTION:
• Since the satellite is moving under a
central force, its angular momentum is
constant. Equate the angular momentum
at A and B and solve for the velocity at B.
© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Sample Problem 12.8
12 - 53
SOLUTION:
• Since the satellite is moving under a
central force, its angular momentum is
constant. Equate the angular momentum
at A and B and solve for the velocity at B.
   
 mi
2340
3960
mi
240
3960
h
mi
18820
constant
sin







B
A
A
B
B
B
A
A
O
r
r
v
v
v
m
r
v
m
r
H
v
rm 
h
mi
12550

B
v
© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Trajectory of a Particle Under a Central Force
12 - 54
• For particle moving under central force directed towards force center,
    0
2
2






 
 


 F
r
r
m
F
F
r
r
m r







• Second expression is equivalent to from which,
,
constant
2

h
r 









r
d
d
r
h
r
r
h 1
and 2
2
2
2
2

 


• After substituting into the radial equation of motion and simplifying,
r
u
u
mh
F
u
d
u
d 1
where
2
2
2
2




• If F is a known function of r or u, then particle trajectory may be
found by integrating for u = f(), with constants of integration
determined from initial conditions.
© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Application to Space Mechanics
12 - 55
constant
1
where
2
2
2
2
2
2
2
2
2








h
GM
u
d
u
d
GMmu
r
GMm
F
r
u
u
mh
F
u
d
u
d


• Consider earth satellites subjected to only gravitational pull
of the earth,
• Solution is equation of conic section,
  ty
eccentrici
cos
1
1 2
2





GM
h
C
h
GM
r
u 


• Origin, located at earth’s center, is a focus of the conic
section.
• Trajectory may be ellipse, parabola, or hyperbola depending
on value of eccentricity.
© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Application to Space Mechanics
12 - 56
  ty
eccentrici
cos
1
1 2
2




GM
h
C
h
GM
r



• Trajectory of earth satellite is defined by
• hyperbola,  > 1 or C > GM/h2
. The radius vector
becomes infinite for





















 

2
1
1
1
1 cos
1
cos
0
cos
1
h
C
GM




• parabola,  = 1 or C = GM/h2
. The radius vector
becomes infinite for



 180
0
cos
1 2
2 

• ellipse,  < 1 or C < GM/h2
. The radius vector is finite
for  and is constant, i.e., a circle, for  < 0.
© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Application to Space Mechanics
12 - 57
• Integration constant C is determined by
conditions at beginning of free flight,  =0, r = r0 ,
 2
0
0
0
2
0
2
2
0
1
1
0
cos
1
1
v
r
GM
r
h
GM
r
C
GM
Ch
h
GM
r















 
0
0
2
0
0
2
2
or
1
r
GM
v
v
v
r
GM
h
GM
C
esc 





• Satellite escapes earth orbit for
• Trajectory is elliptic for v0 < vesc and becomes
circular for  = 0 or C = 0,
0
r
GM
vcirc 
© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Application to Space Mechanics
12 - 58
• Recall that for a particle moving under a central
force, the areal velocity is constant, i.e.,
constant
2
1
2
2
1 

 h
r
dt
dA

• Periodic time or time required for a satellite to
complete an orbit is equal to area within the orbit
divided by areal velocity,
h
ab
h
ab 


2
2


where  
1
0
1
0
2
1
r
r
b
r
r
a



© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Sample Problem 12.9
12 - 59
Determine:
a) the maximum altitude reached by
the satellite, and
b) the periodic time of the satellite.
A satellite is launched in a direction
parallel to the surface of the earth
with a velocity of 36,900 km/h at an
altitude of 500 km.
SOLUTION:
• Trajectory of the satellite is described by

cos
1
2
C
h
GM
r


Evaluate C using the initial conditions
at  = 0.
• Determine the maximum altitude by
finding r at  = 180o
.
• With the altitudes at the perigee and
apogee known, the periodic time can
be evaluated.
© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Sample Problem 12.9
12 - 60
SOLUTION:
• Trajectory of the satellite is described by

cos
1
2
C
h
GM
r


Evaluate C using the initial conditions
at  = 0.
 
  
  
2
3
12
2
6
2
2
2
9
3
6
0
0
3
0
6
0
s
m
10
398
m
10
37
.
6
s
m
81
.
9
s
m
10
4
.
70
s
m
10
25
.
10
m
10
6.87
s
m
10
25
.
10
s/h
3600
m/km
1000
h
km
36900
m
10
6.87
km
500
6370



















gR
GM
v
r
h
v
r
 
1
-
9
2
2
2
3
12
6
2
0
m
10
3
.
65
s
m
4
.
70
s
m
10
398
m
10
87
.
6
1
1









h
GM
r
C
© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Sample Problem 12.9
12 - 61
• Determine the maximum altitude by finding r1
at  = 180o
.
 
km
66700
m
10
7
.
66
m
1
10
3
.
65
s
m
4
.
70
s
m
10
398
1
6
1
9
2
2
2
3
12
2
1








 
r
C
h
GM
r
  km
60300
km
6370
-
66700
altitude
max 

• With the altitudes at the perigee and apogee
known, the periodic time can be evaluated.
   
  
s
m
10
70.4
m
10
21.4
m
10
36.8
2
h
2
m
10
21.4
m
10
7
.
66
87
.
6
m
10
36.8
m
10
7
.
66
87
.
6
2
9
6
6
6
6
1
0
6
6
2
1
1
0
2
1





















ab
r
r
b
r
r
a
min
31
h
19
s
10
3
.
70 3




© 2013 The McGraw-Hill Companies, Inc. All rights reserved.
Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
Tenth
Editio
Kepler’s Laws of Planetary Motion
12 - 62
• Results obtained for trajectories of satellites around earth may also be
applied to trajectories of planets around the sun.
• Properties of planetary orbits around the sun were determined
astronomical observations by Johann Kepler (1571-1630) before
Newton had developed his fundamental theory.
1) Each planet describes an ellipse, with the sun located at one of its
foci.
2) The radius vector drawn from the sun to a planet sweeps equal
areas in equal times.
3) The squares of the periodic times of the planets are proportional
to the cubes of the semimajor axes of their orbits.

dynamicsclassnoteslecturess12lecture.ppt

  • 1.
    VECTOR MECHANICS FORENGINEERS: DYNAMICS DYNAMICS Tenth Tenth Edition Edition Ferdinand P. Beer Ferdinand P. Beer E. Russell Johnston, Jr. E. Russell Johnston, Jr. Phillip J. Cornwell Phillip J. Cornwell Lecture Notes: Lecture Notes: Brian P. Self Brian P. Self California Polytechnic State University California Polytechnic State University CHAPTER © 2013 The McGraw-Hill Companies, Inc. All rights reserved. 12 Kinetics of Particles: Newton’s Second Law
  • 2.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Contents 12 - 2 Introduction Newton’s Second Law of Motion Linear Momentum of a Particle Systems of Units Equations of Motion Dynamic Equilibrium Sample Problem 12.1 Sample Problem 12.3 Sample Problem 12.4 Sample Problem 12.5 Sample Problem 12.6 Angular Momentum of a Particle Equations of Motion in Radial & Transverse Components Conservation of Angular Momentum Newton’s Law of Gravitation Sample Problem 12.7 Sample Problem 12.8 Trajectory of a Particle Under a Central Force Application to Space Mechanics Sample Problem 12.9 Kepler’s Laws of Planetary Motion
  • 3.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Kinetics of Particles 2 - 3 We must analyze all of the forces acting on the wheelchair in order to design a good ramp High swing velocities can result in large forces on a swing chain or rope, causing it to break.
  • 4.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Introduction 12 - 4 • Newton’s Second Law of Motion m   F a • 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. • Must be expressed with respect to a Newtonian (or inertial) frame of reference, i.e., one that is not accelerating or rotating. • This form of the equation is for a constant mass system
  • 5.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Linear Momentum of a Particle 12 - 5 • Replacing the acceleration by the derivative of the velocity yields   particle the of momentum linear      L dt L d v m dt d dt v d m F      • Linear Momentum Conservation Principle: If the resultant force on a particle is zero, the linear momentum of the particle remains constant in both magnitude and direction.
  • 6.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Systems of Units 12 - 6 • Of the units for the four primary dimensions (force, mass, length, and time), three may be chosen arbitrarily. The fourth must be compatible with Newton’s 2nd Law. • International System of Units (SI Units): base units are the units of length (m), mass (kg), and time (second). The unit of force is derived,   2 2 s m kg 1 s m 1 kg 1 N 1          • U.S. Customary Units: base units are the units of force (lb), length (m), and time (second). The unit of mass is derived, ft s lb 1 s ft 1 lb 1 slug 1 s ft 32.2 lb 1 lbm 1 2 2 2    
  • 7.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Equations of Motion 12 - 7 • Newton’s second law a m F     • Can use scalar component equations, e.g., for rectangular components,     z m F y m F x m F ma F ma F ma F k a j a i a m k F j F i F z y x z z y y x x z y x z y x                              
  • 8.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Dynamic Equilibrium 12 - 8 • Alternate expression of Newton’s second law, ector inertial v a m a m F 0         • With the inclusion of the inertial vector, the system of forces acting on the particle is equivalent to zero. The particle is in dynamic equilibrium. • Methods developed for particles in static equilibrium may be applied, e.g., coplanar forces may be represented with a closed vector polygon. • Inertia vectors are often called inertial forces as they measure the resistance that particles offer to changes in motion, i.e., changes in speed or direction. • Inertial forces may be conceptually useful but are not like the contact and gravitational forces found in statics.
  • 9.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Free Body Diagrams and Kinetic Diagrams 12 - 9 The free body diagram is the same as you have done in statics; we will add the kinetic diagram in our dynamic analysis. 2. Draw your axis system (e.g., Cartesian, polar, path) 3. Add in applied forces (e.g., weight, 225 lb pulling force) 4. Replace supports with forces (e.g., normal force) 1. Isolate the body of interest (free body) 5. Draw appropriate dimensions (usually angles for particles) x y 225 N Ff N mg 25o
  • 10.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Free Body Diagrams and Kinetic Diagrams 12 - 10 Put the inertial terms for the body of interest on the kinetic diagram. 2. Draw in the mass times acceleration of the particle; if unknown, do this in the positive direction according to your chosen axes 1. Isolate the body of interest (free body) x y 225 N Ff N mg 25o may max m   F a 
  • 11.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Free Body Diagrams and Kinetic Diagrams 2 - 11 Draw the FBD and KD for block A (note that the massless, frictionless pulleys are attached to block A and should be included in the system).
  • 12.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Free Body Diagrams and Kinetic Diagrams 2 - 12 1. Isolate body 2. Axes 3. Applied forces 4. Replace supports with forces 5. Dimensions (already drawn) x y mg Ff-1 N1 T T T T T Ff-B NB may = 0 max 6. Kinetic diagram =
  • 13.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Free Body Diagrams and Kinetic Diagrams 2 - 13 Draw the FBD and KD for the collar B. Assume there is friction acting between the rod and collar, motion is in the vertical plane, and  is increasing
  • 14.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Free Body Diagrams and Kinetic Diagrams 2 - 14 1. Isolate body 2. Axes 3. Applied forces 4. Replace supports with forces 5. Dimensions 6. Kinetic diagram mg Ff N mar ma e er =  
  • 15.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Sample Problem 12.1 12 - 15 A 200-lb block rests on a horizontal plane. Find the magnitude of the force P required to give the block an acceleration of 10 ft/s2 to the right. The coefficient of kinetic friction between the block and plane is k0.25. SOLUTION: • Resolve the equation of motion for the block into two rectangular component equations. • Unknowns consist of the applied force P and the normal reaction N from the plane. The two equations may be solved for these unknowns.
  • 16.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Sample Problem 12.1 12 - 16 N N F g W m k 25 . 0 ft s lb 21 . 6 s ft 2 . 32 lb 200 2 2        x y O SOLUTION: • Resolve the equation of motion for the block into two rectangular component equations. : ma Fx      lb 1 . 62 s ft 10 ft s lb 21 . 6 25 . 0 30 cos 2 2      N P : 0   y F 0 lb 200 30 sin     P N • Unknowns consist of the applied force P and the normal reaction N from the plane. The two equations may be solved for these unknowns.   lb 1 . 62 lb 200 30 sin 25 . 0 30 cos lb 200 30 sin         P P P N lb 151  P
  • 17.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Sample Problem 12.3 12 - 17 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 the cord. SOLUTION: • Write the kinematic relationships for the dependent motions and accelerations of the blocks. • Write the equations of motion for the blocks and pulley. • Combine the kinematic relationships with the equations of motion to solve for the accelerations and cord tension.
  • 18.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Sample Problem 12.3 12 - 18 • Write equations of motion for blocks and pulley. : A A x a m F     A a T kg 100 1  : B B y a m F          B B B B B a T a T a m T g m kg 300 - N 2940 kg 300 s m 81 . 9 kg 300 2 2 2 2      : 0    C C y a m F 0 2 1 2   T T SOLUTION: • Write the kinematic relationships for the dependent motions and accelerations of the blocks. A B A B a a x y 2 1 2 1   x y O
  • 19.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Sample Problem 12.3 12 - 19   N 1680 2 N 840 kg 100 s m 20 . 4 s m 40 . 8 1 2 1 2 2 1 2        T T a T a a a A A B A • Combine kinematic relationships with equations of motion to solve for accelerations and cord tension. A B A B a a x y 2 1 2 1     A a T kg 100 1       A B a a T 2 1 2 kg 300 - N 2940 kg 300 - N 2940       0 kg 100 2 kg 150 N 2940 0 2 1 2      A A a a T T x y O
  • 20.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Sample Problem 12.4 12 - 20 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. SOLUTION: • The block is constrained to slide down the wedge. Therefore, their motions are dependent. Express the acceleration of block as the acceleration of wedge plus the acceleration of the block relative to the wedge. • Write the equations of motion for the wedge and block. • Solve for the accelerations.
  • 21.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Sample Problem 12.4 12 - 21 SOLUTION: • The block is constrained to slide down the wedge. Therefore, their motions are dependent. A B A B a a a      • Write equations of motion for wedge and block. x y : A A x a m F     A A A A a g W N a m N    1 1 5 . 0 30 sin  : 30 cos A B A B x B x a a m a m F                  30 sin 30 cos 30 cos 30 sin g a a a a g W W A A B A B A B B  : 30 sin      A B y B y a m a m F        30 sin 30 cos 1 A B B a g W W N
  • 22.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Sample Problem 12.4 12 - 22   A A a g W N  1 5 . 0 • Solve for the accelerations.                                30 sin lb 12 lb 30 2 30 cos lb 12 s ft 2 . 32 30 sin 2 30 cos 30 sin 30 cos 2 30 sin 30 cos 2 1 A B A B A A B B A A A B B a W W gW a a g W W a g W a g W W N 2 s ft 07 . 5  A a             30 sin s ft 2 . 32 30 cos s ft 07 . 5 30 sin 30 cos 2 2 A B A A B a g a a 2 s ft 5 . 20  A B a
  • 23.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Group Problem Solving 2 - 23 The two blocks shown are originally at rest. Neglecting the masses of the pulleys and the effect of friction in the pulleys and between block A and the horizontal surface, determine (a) the acceleration of each block, (b) the tension in the cable. SOLUTION: • Write the kinematic relationships for the dependent motions and accelerations of the blocks. • Write the equations of motion for the blocks and pulley. • Combine the kinematic relationships with the equations of motion to solve for the accelerations and cord tension. • Draw the FBD and KD for each block
  • 24.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Group Problem Solving 2 - 24 xA yB const nts 3 a A B x y L    3 0 A B v v   3 0 A B a a   3 A B a a  SOLUTION: • Write the kinematic relationships for the dependent motions and accelerations of the blocks. This is the same problem worked last chapter- write the constraint equation Differentiate this twice to get the acceleration relationship. (1)
  • 25.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Group Problem Solving 2 - 25 :   x A A F m a   A B T m a 3 A B T m a  y B B F m a   3(3 ) B A B B B m g m a m a   2 2 9.81 m/s 0.83136 m/s 30 kg 1 9 1 9 25 kg B A B g a m m      2 2.49 2.49 m/s A   a 2 3 30 kg 0.83136 m/s T    74.8 N T  • Draw the FBD and KD for each block mAg T NA maAx mBg 2T T maBy • Write the equation of motion for each block = = From Eq (1) (2) (3) 3 B B B W T m a   (2) (3) B A • Solve the three equations, 3 unknowns +y +x
  • 26.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Concept Quiz 2 - 26 The three systems are released from rest. Rank the accelerations, from highest to lowest. a) (1) > (2) > (3) b) (1) = (2) > (3) c) (2) > (1) > (3) d) (1) = (2) = (3) e) (1) = (2) < (3) (1) (2) (3)
  • 27.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Kinetics: Normal and Tangential Coordinates 2 - 27 Aircraft and roller coasters can both experience large normal forces during turns.
  • 28.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Equations of Motion 12 - 28 • For tangential and normal components, t t t F ma dv F m dt     • Newton’s second law a m F     2 n n n F ma v F m     
  • 29.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Sample Problem 12.5 12 - 29 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 accel- eration of the bob in that position. SOLUTION: • Resolve the equation of motion for the bob into tangential and normal components. • Solve the component equations for the normal and tangential accelerations. • Solve for the velocity in terms of the normal acceleration.
  • 30.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Sample Problem 12.5 12 - 30 SOLUTION: • Resolve the equation of motion for the bob into tangential and normal components. • Solve the component equations for the normal and tangential accelerations. : t t ma F       30 sin 30 sin g a ma mg t t 2 s m 9 . 4  t a : n n ma F           30 cos 5 . 2 30 cos 5 . 2 g a ma mg mg n n 2 s m 03 . 16  n a • Solve for velocity in terms of normal acceleration.    2 2 s m 03 . 16 m 2    n n a v v a   s m 66 . 5   v
  • 31.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Sample Problem 12.6 12 - 31 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. 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.
  • 32.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Sample Problem 12.6 12 - 32 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. : 0   y F   cos 0 cos W R W R    : n n ma F       2 sin cos sin v g W W a g W R n   • Solve for the vehicle speed.       18 tan ft 400 s ft 2 . 32 tan 2 2   g v h mi 1 . 44 s ft 7 . 64   v
  • 33.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Group Problem Solving 2 - 33 The 3-kg collar B rests on the frictionless arm AA. The collar is held in place by the rope attached to drum D and rotates about O in a horizontal plane. The linear velocity of the collar B is increasing according to v= 0.2 t2 where v is in m/s and t is in sec. Find the tension in the rope and the force of the bar on the collar after 5 seconds if r = 0.4 m. v SOLUTION: • Write the equations of motion for the collar. • Combine the equations of motion with kinematic relationships and solve. • Draw the FBD and KD for the collar. • Determine kinematics of the collar.
  • 34.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Group Problem Solving 2 - 34 SOLUTION: • Given: v= 0.2 t2 , r = 0.4 m • Find: T and N at t = 5 sec Draw the FBD and KD of the collar man T N et en mat Write the equations of motion = n n F ma   t t F ma   2 v N m   dv T m dt 
  • 35.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Group Problem Solving 2 - 35 man T N et en mat = 2 2 2 5 62.5 (m/s ) 0.4 n v a     2 0.4 0.4(5) 2 m/s t dv a t dt     Kinematics : find vt, an, at 2 2 0.2 0.2(5 )=5 m/s t v t   Substitute into equations of motion 3.0(62.5) N  3.0(2) T  187.5 N N  6.0 N T   n n F ma   t t F ma  
  • 36.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Group Problem Solving 2 - 36 man T N et en mat = How would the problem change if motion was in the vertical plane? mg  You would add an mg term and would also need to calculate  When is the tangential force greater than the normal force? Only at the very beginning, when starting to accelerate. In most applications, an >> at
  • 37.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Concept Question 2 - 37 D B C A A car is driving from A to D on the curved path shown. The driver is doing the following at each point: A – going at a constant speed B – stepping on the accelerator C – stepping on the brake D – stepping on the accelerator Draw the approximate direction of the car’s acceleration at each point.
  • 38.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Kinetics: Radial and Transverse Coordinates 2 - 38 Hydraulic actuators and extending robotic arms are often analyzed using radial and transverse coordinates.
  • 39.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Eqs of Motion in Radial & Transverse Components 12 - 39                 r r m ma F r r m ma F r r 2 2         • Consider particle at r and , in polar coordinates,
  • 40.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Sample Problem 12.7 12 - 40 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  a) the component vr of the velocity of B along OA, and b) the magnitude of the horizontal force exerted on B by the arm OA. Knowing that B is released at a distance r0 from O, express as a function of r 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.
  • 41.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Sample Problem 12.7 12 - 41 SOLUTION: • Write the radial and transverse equations of motion for the block. : :   a m F a m F r r                   r r m F r r m 2 0 2     • Integrate the radial equation to find an expression for the radial velocity.          r r v r r r r r r r r r dr r dv v dr r dr r dv v dr dv v dt dr dr dv dt dv v r r 0 2 0 0 2 0 2          dr dv v dt dr dr dv dt dv v r r r r r r         2 0 2 2 0 2 r r vr   • Substitute known information into the transverse equation to find an expression for the force on the block.   2 1 2 0 2 2 0 2 r r m F   
  • 42.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Group Problem Solving 2 - 42 • Write the equations of motion for the collar. • Combine the equations of motion with kinematic relationships and solve. • Draw the FBD and KD for the collar. • Determine kinematics of the collar. SOLUTION: The 3-kg collar B slides on the frictionless arm AA. The arm is attached to drum D and rotates about O in a horizontal plane at the rate where and t are expressed in rad/s and seconds, respectively. As the arm-drum assembly rotates, a mechanism within the drum releases the cord so that the collar moves outward from O with a constant speed of 0.5 m/s. Knowing that at t = 0, r = 0, determine the time at which the tension in the cord is equal to the magnitude of the horizontal force exerted on B by arm AA. 0.75t     
  • 43.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Group Problem Solving 2 - 43 mar T N e er ma = r r F ma   B F m a     Draw the FBD and KD of the collar Write the equations of motion SOLUTION: • Given: • Find: time when T = N 2 ( ) T m r r      ( 2 ) N m r r        0.75t    5 m/s r   (0) 0 r 
  • 44.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Group Problem Solving 2 - 44 3 2 : (3 kg)( 0.28125 ) m/s r r F ma T t      2 : (3 kg)(1.125 ) m/s B F m a N t      0 0 0.5 r t dr dt    (0.5 ) m r t  0 r   2 (0.75 ) rad/s 0.75 rad/s t       2 2 3 2 0 [(0.5 ) m][(0.75 ) rad/s] (0.28125 ) m/s r a r r t t t         2 2 2 [(0.5 ) m][0.75 rad/s ] 2(0.5 m/s)[(0.75 ) rad/s] (1.125 ) m/s a r r t t t            Kinematics : find expressions for r and  Substitute values into ar , a Substitute into equation of motion 3 (0.84375 ) (3.375 ) t t  2 4.000 t  2.00 s t  Set T = N 5 m/s r  
  • 45.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Concept Quiz 2 - 45 Top View e1 e2  v The girl starts walking towards the outside of the spinning platform, as shown in the figure. She is walking at a constant rate with respect to the platform, and the platform rotates at a constant rate. In which direction(s) will the forces act on her? a) +e1 b) - e1 c) +e2 d) - e2 e) The forces are zero in the e1 and e2 directions
  • 46.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Angular Momentum of a Particle 2 - 46 Satellite orbits are analyzed using conservation of angular momentum.
  • 47.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Eqs of Motion in Radial & Transverse Components 12 - 47                 r r m ma F r r m ma F r r 2 2         • Consider particle at r and , in polar coordinates,                         r r m F r r r m mr dt d F r mr HO 2 2 2 2 2         • This result may also be derived from conservation of angular momentum,
  • 48.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Angular Momentum of a Particle 12 - 48 • moment of momentum or the angular momentum of the particle about O.    V m r HO    • Derivative of angular momentum with respect to time,              O O M F r a m r V m V V m r V m r H               • It follows from Newton’s second law that the sum of the moments about O of the forces acting on the particle is equal to the rate of change of the angular momentum of the particle about O. z y x O mv mv mv z y x k j i H      • is perpendicular to plane containing O H  V m r   and     2 sin mr v rm rmV HO   
  • 49.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Conservation of Angular Momentum 12 - 49 • When only 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. • Since the line of action of the central force passes through O, and 0    O O H M    constant    O H V m r    • Position vector and motion of particle are in a plane perpendicular to . O H  • Magnitude of angular momentum, 0 0 0 sin constant sin   V m r V rm HO    mass unit momentum angular constant 2 2      h r m H mr H O O     or
  • 50.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Conservation of Angular Momentum 12 - 50 • Radius vector OP sweeps infinitesimal area  d r dA 2 2 1  • Define       2 2 1 2 2 1 r dt d r dt dA areal velocity • Recall, for a body moving under a central force, constant 2    r h • When a particle moves under a central force, its areal velocity is constant.
  • 51.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Newton’s Law of Gravitation 12 - 51 • Gravitational force exerted by the sun on a planet or by the earth on a satellite is an important example of gravitational force. • Newton’s law of universal gravitation - two particles of mass M and m attract each other with equal and opposite force directed along the line connecting the particles, 4 4 9 2 3 12 2 s lb ft 10 4 . 34 s kg m 10 73 . 66 n gravitatio of constant           G r Mm G F • For particle of mass m on the earth’s surface, 2 2 2 s ft 2 . 32 s m 81 . 9     g mg R MG m W
  • 52.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Sample Problem 12.8 12 - 52 A satellite is launched in a direction parallel to the surface of the earth with a velocity of 18820 mi/h from an altitude of 240 mi. Determine the velocity of the satellite as it reaches it maximum altitude of 2340 mi. The radius of the earth is 3960 mi. SOLUTION: • Since the satellite is moving under a central force, its angular momentum is constant. Equate the angular momentum at A and B and solve for the velocity at B.
  • 53.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Sample Problem 12.8 12 - 53 SOLUTION: • Since the satellite is moving under a central force, its angular momentum is constant. Equate the angular momentum at A and B and solve for the velocity at B.      mi 2340 3960 mi 240 3960 h mi 18820 constant sin        B A A B B B A A O r r v v v m r v m r H v rm  h mi 12550  B v
  • 54.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Trajectory of a Particle Under a Central Force 12 - 54 • For particle moving under central force directed towards force center,     0 2 2              F r r m F F r r m r        • Second expression is equivalent to from which, , constant 2  h r           r d d r h r r h 1 and 2 2 2 2 2      • After substituting into the radial equation of motion and simplifying, r u u mh F u d u d 1 where 2 2 2 2     • If F is a known function of r or u, then particle trajectory may be found by integrating for u = f(), with constants of integration determined from initial conditions.
  • 55.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Application to Space Mechanics 12 - 55 constant 1 where 2 2 2 2 2 2 2 2 2         h GM u d u d GMmu r GMm F r u u mh F u d u d   • Consider earth satellites subjected to only gravitational pull of the earth, • Solution is equation of conic section,   ty eccentrici cos 1 1 2 2      GM h C h GM r u    • Origin, located at earth’s center, is a focus of the conic section. • Trajectory may be ellipse, parabola, or hyperbola depending on value of eccentricity.
  • 56.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Application to Space Mechanics 12 - 56   ty eccentrici cos 1 1 2 2     GM h C h GM r    • Trajectory of earth satellite is defined by • hyperbola,  > 1 or C > GM/h2 . The radius vector becomes infinite for                         2 1 1 1 1 cos 1 cos 0 cos 1 h C GM     • parabola,  = 1 or C = GM/h2 . The radius vector becomes infinite for     180 0 cos 1 2 2   • ellipse,  < 1 or C < GM/h2 . The radius vector is finite for  and is constant, i.e., a circle, for  < 0.
  • 57.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Application to Space Mechanics 12 - 57 • Integration constant C is determined by conditions at beginning of free flight,  =0, r = r0 ,  2 0 0 0 2 0 2 2 0 1 1 0 cos 1 1 v r GM r h GM r C GM Ch h GM r                  0 0 2 0 0 2 2 or 1 r GM v v v r GM h GM C esc       • Satellite escapes earth orbit for • Trajectory is elliptic for v0 < vesc and becomes circular for  = 0 or C = 0, 0 r GM vcirc 
  • 58.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Application to Space Mechanics 12 - 58 • Recall that for a particle moving under a central force, the areal velocity is constant, i.e., constant 2 1 2 2 1    h r dt dA  • Periodic time or time required for a satellite to complete an orbit is equal to area within the orbit divided by areal velocity, h ab h ab    2 2   where   1 0 1 0 2 1 r r b r r a   
  • 59.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Sample Problem 12.9 12 - 59 Determine: a) the maximum altitude reached by the satellite, and b) the periodic time of the satellite. A satellite is launched in a direction parallel to the surface of the earth with a velocity of 36,900 km/h at an altitude of 500 km. SOLUTION: • Trajectory of the satellite is described by  cos 1 2 C h GM r   Evaluate C using the initial conditions at  = 0. • Determine the maximum altitude by finding r at  = 180o . • With the altitudes at the perigee and apogee known, the periodic time can be evaluated.
  • 60.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Sample Problem 12.9 12 - 60 SOLUTION: • Trajectory of the satellite is described by  cos 1 2 C h GM r   Evaluate C using the initial conditions at  = 0.         2 3 12 2 6 2 2 2 9 3 6 0 0 3 0 6 0 s m 10 398 m 10 37 . 6 s m 81 . 9 s m 10 4 . 70 s m 10 25 . 10 m 10 6.87 s m 10 25 . 10 s/h 3600 m/km 1000 h km 36900 m 10 6.87 km 500 6370                    gR GM v r h v r   1 - 9 2 2 2 3 12 6 2 0 m 10 3 . 65 s m 4 . 70 s m 10 398 m 10 87 . 6 1 1          h GM r C
  • 61.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Sample Problem 12.9 12 - 61 • Determine the maximum altitude by finding r1 at  = 180o .   km 66700 m 10 7 . 66 m 1 10 3 . 65 s m 4 . 70 s m 10 398 1 6 1 9 2 2 2 3 12 2 1           r C h GM r   km 60300 km 6370 - 66700 altitude max   • With the altitudes at the perigee and apogee known, the periodic time can be evaluated.        s m 10 70.4 m 10 21.4 m 10 36.8 2 h 2 m 10 21.4 m 10 7 . 66 87 . 6 m 10 36.8 m 10 7 . 66 87 . 6 2 9 6 6 6 6 1 0 6 6 2 1 1 0 2 1                      ab r r b r r a min 31 h 19 s 10 3 . 70 3    
  • 62.
    © 2013 TheMcGraw-Hill Companies, Inc. All rights reserved. Vector Mechanics for Engineers: Dynamics Vector Mechanics for Engineers: Dynamics Tenth Editio Kepler’s Laws of Planetary Motion 12 - 62 • Results obtained for trajectories of satellites around earth may also be applied to trajectories of planets around the sun. • Properties of planetary orbits around the sun were determined astronomical observations by Johann Kepler (1571-1630) before Newton had developed his fundamental theory. 1) Each planet describes an ellipse, with the sun located at one of its foci. 2) The radius vector drawn from the sun to a planet sweeps equal areas in equal times. 3) The squares of the periodic times of the planets are proportional to the cubes of the semimajor axes of their orbits.