Introduction to Dynamics
Transcript of Introduction to Dynamics
Introduction to Dynamics (N. Zabaras)
Review LectureProf. Nicholas Zabaras
Warwick Centre for Predictive Modelling
University of Warwick
Coventry CV4 7AL
United Kingdom
Email: [email protected]
URL: http://www.zabaras.com/
April 16, 2016
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Includes highlights from the various lectures – Please do not assume that the exam material is related or restricted
to these notes.
Introduction to Dynamics (N. Zabaras)
Velocity as a Function of Time
c
dva
dt
cdv a dt
0o
v t
c
v
dv a dt
0 cv v a t
Introduction to Dynamics (N. Zabaras)
Position as a Function of Time
0 c
dxv v a t
dt
0
0
( )
o
x t
c
s
dx v a t dt
2
0 0
1
2cx x v t a t
Introduction to Dynamics (N. Zabaras)
Velocity as a Function of Position
0 0
v x
c
v s
v dv a dx
cv dv a dx
2 2
0 02 ( )cv v a x x
2 2
0 0
1 1( )
2 2cv v a x x
Introduction to Dynamics (N. Zabaras)
Tangential and Normal Components
tevv
• With the velocity vector expressed as
the particle acceleration may be written as
t tt t
de dedv dv dv d dsa e v e v
dt dt dt dt d ds dt
but
vdt
dsdsde
d
edn
t
After substituting,
22 va
dt
dvae
ve
dt
dva ntnt
• Tangential component of acceleration reflects
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.
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Introduction to Dynamics (N. Zabaras)
Radial and Transverse Components
• When particle position is given in polar coordinates,
it is convenient to express velocity and acceleration
with components parallel and perpendicular to OP.
rr e
d
ede
d
ed
dt
de
dt
d
d
ed
dt
ed rr
dt
de
dt
d
d
ed
dt
edr
erer
edt
dre
dt
dr
dt
edre
dt
drer
dt
dv
r
rr
rr
• The particle velocity vector is
• Similarly, the particle acceleration vector is
errerr
dt
ed
dt
dre
dt
dre
dt
d
dt
dr
dt
ed
dt
dre
dt
rd
edt
dre
dt
dr
dt
da
r
rr
r
22
2
2
2
2
rerr
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Introduction to Dynamics (N. Zabaras)
Equations of Motion
• Newton’s second law provides
amF
• Solution for particle motion is facilitated by
resolving vector equation into scalar component
equations, e.g., for rectangular components,
zmFymFxmF
maFmaFmaF
kajaiamkFjFiF
zyx
zzyyxx
zyxzyx
• For tangential and normal components,
2vmF
dt
dvmF
maFmaF
nt
nntt
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Introduction to Dynamics (N. Zabaras)
Linear Momentum of a Particle
• Replacing the acceleration by the derivative of
the velocity yields
particle theof momentumlinear
L
dt
Ldvm
dt
d
dt
vdmF
• 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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Introduction to Dynamics (N. Zabaras)
Sample Problem
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.
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Introduction to Dynamics (N. Zabaras)
Sample Problem
• Write equations of motion for blocks and pulley.
:AAx amF
AaT kg1001
:BBy amF
B
B
BBB
aT
aT
amTgm
kg300-N2940
kg300sm81.9kg300
2
22
2
:0 CCy amF
02 12 TT
SOLUTION:
• Write the kinematic relationships for the dependent
motions and accelerations of the blocks.
ABAB aaxy21
21
x
y
O
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Introduction to Dynamics (N. Zabaras)
Angular Momentum of a Particle• moment of momentum or the
angular momentum of the particle about O. VmrHO
• Derivative of angular momentum with respect to time,
O
O
M
Fr
amrVmVVmrVmrH
• 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.
zyx
O
mvmvmv
zyx
kji
H
• is perpendicular to plane containingOH
Vmr
and
2
sin
mr
vrm
rmVHO
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Introduction to Dynamics (N. Zabaras)
Eqs of Motion in Radial & Transverse Components
rrmmaF
rrmmaF rr
2
2
• Consider particle at r and , in polar coordinates,
rrmF
rrrm
mrdt
dFr
mrHO
2
22
2
2
• This result may also be derived from
conservation of angular momentum,
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rr r v e e
Introduction to Dynamics (N. Zabaras)
Conservation of Angular Momentum
• 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 OO HM
constant OHVmr
• Position vector and motion of particle are in
a plane perpendicular to .OH
• Magnitude of angular momentum,
000 sin
constantsin
Vmr
VrmHO
massunit
momentumangular
constant
2
2
hrm
H
mrH
O
O
or
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Introduction to Dynamics (N. Zabaras)
Sample Problem
The 0.5 lb pellet is pushed against
the spring and released from rest
at A. Neglecting friction,
determine the smallest deflection
of the spring for which the pellet
will travel around the loop and
remain in contact with the loop at
all times.
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Introduction to Dynamics (N. Zabaras)
Sample Problem
SOLUTION:
• Setting the force exerted by the loop to zero, solve
for the minimum velocity at D.
:nn maF
222
2
sft4.64sft32.2ft 2
rgv
rvmmgmaW
D
Dn
• Apply the principle of conservation of energy
between points A and D.
0
18ftlb360
1
22
212
21
1
T
xxkxVVV ge
lbft5.0sft4.64sft2.32
lb5.0
2
1
lbft2ft4lb5.00
22
2
2
21
2
2
D
ge
mvT
WyVVV
25.0180 2
2211
x
VTVT
in. 47.4ft 3727.0 x
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Introduction to Dynamics (N. Zabaras)
Principle of Impulse and Momentum
21
12
2
1
2
1
LdtFL
LLdtF
LF
t
t
t
t
21
12
2
1
2
1
HdtMH
HHdtM
HM
t
tO
t
tO
OO
• The momenta of the particles at time t1 and the impulse of the
forces from t1 to t2 form a system of vectors equipollent to the
system of momenta of the particles at time t2 .
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Introduction to Dynamics (N. Zabaras)
2
10 1 0 0 2( ) ( )
t
tdt H M H
2
10 0 0 0 2 0 1( ) ( )
t
t
ddt
dt M H M H H
2 2
1 10Angular impulse
t t
t tdt dt M r F
2
1 21
t
tr mv M dt r F dt r m v
Angular Impulse and Momentum Principles
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0 1 0 2( ) ( )H H
1 1 2 2r m r m
Conservation of
Angular
Momentum
when angular
impulse is zero
r
mv
Introduction to Dynamics (N. Zabaras)
W = 0.8 Ib
Smooth table
r1=1.7 ft
v1= 4 ft/s
vc=6ft/s (constant)
v2= ? at (r2)= 0.6ft
Work done = ?
1 2
1 1 2 2'B B
H H
r m r m
2
2
0.8 0.81.75 ( ) 4 0.6 ( ) '
32.2 32.2
' 11.67 /ft s
2 2
2 (11.67) (6) 13.1 /ft s
Work Done (energy balance for the ball)
1 1 2 2T U T 2 21 0.8 1 0.8
( )(4) ( )(13.1)2 32.2 2 32.2
FU
1.94 ft.IbFU
Example
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The cord force F (not constant) on the
ball passes through the z axis, and
the weight and NB are parallel to it.
Hence the moments, or angular
impulses created by these forces,
are all zero about this axis.
Therefore, angular momentum is
conserved about the z axis.
Introduction to Dynamics (N. Zabaras)
two components of
acceleration:
one component of
velocity:
Fixed-Axis Rotation: Summary
Introduction to Dynamics (N. Zabaras)
Absolute and Relative Velocity in Plane Motion
• Any plane motion can be replaced by a translation of
an arbitrary reference point A and a simultaneous
rotation about A.
ABAB vvv
rvrkv ABABAB
ABAB rkvv
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Introduction to Dynamics (N. Zabaras)
Instantaneous Center of Rotation in Plane Motion• The instantaneous center of rotation lies at the
intersection of the perpendiculars to the velocity
vectors through A and B .
cosl
v
AC
v AA
tan
cossin
A
AB
v
l
vlBCv
• The velocities of all particles on the rod are as if they
were rotated about C.
• The particle at the center of rotation has zero velocity.
• The particle coinciding with the center of rotation
changes with time and the acceleration of the particle
at the instantaneous center of rotation is not zero.
• The acceleration of the particles in the slab cannot be
determined as if the slab were simply rotating about C.
• The trace of the locus of the center of rotation on the
body is the body centrode and in space is the space
centrode.
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Introduction to Dynamics (N. Zabaras)
Rolling wheels
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vB r
Rolls without slipping
Cv (2 )r
C
Introduction to Dynamics (N. Zabaras)
IC
C
ICCC r /
D
Instantaneous center of zero velocity
ICDD r /
Rolling wheels
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Introduction to Dynamics (N. Zabaras)
Absolute and Relative Acceleration in Plane Motion
• Absolute acceleration of a particle of the
slab,
ABAB aaa
• Relative acceleration associated with rotation about A
includes tangential and normal components,ABa
ABnAB
ABtAB
ra
rka
2
2
ra
ra
nAB
tAB
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Introduction to Dynamics (N. Zabaras)
Absolute and Relative Acceleration in Plane Motion
• Given
determine
, and AA va
. and
Ba
tABnABA
ABAB
aaa
aaa
• Vector result depends on sense of and the
relative magnitudes of nABA aa and
Aa
• Must also know angular velocity .
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Introduction to Dynamics (N. Zabaras)
Equations of Motion for a Rigid Body• Consider a rigid body acted
upon by several external forces.
• Assume that the body is made
of a large number of particles.
• For the motion of the mass
center G of the body with
respect to the Newtonian frame
Oxyz, amF
• For the motion of the body with
respect to the centroidal frame
Gx’y’z’,
GG HM
• System of external forces is
equipollent to the system
consisting of . and GHam
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Introduction to Dynamics (N. Zabaras)
Angular Momentum of a Rigid Body in Plane Motion
• Consider a rigid slab
in plane motion.
• Angular momentum of the slab may be
computed by
I
mr
mrr
mvrH
ii
n
iiii
n
iiiiG
Δ
Δ
Δ
2
1
1
• After differentiation,
IIHG
• Results are also valid for plane motion of
bodies which are symmetrical with respect
to the reference plane.
• Results are not valid for asymmetrical
bodies or three-dimensional motion.
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Introduction to Dynamics (N. Zabaras)
( ) ( ) ( )P P G y G xM x m a y m a I kΜ
Kinetic Moment
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( )
( )
x G x
y G y
G G
F m a
F m a
M I α
( )P PM kΜ
Introduction to Dynamics (N. Zabaras)
2( )
( )
n G n G
t G t G
G G
F m a mω r
F m a mr α
M I α
2 ( )
G G
G G
O
I α r m r α
I mr α
I α
( ) ( )O O G G G tM I α r m aΜ k
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Rotation About a Fixed Axis
Introduction to Dynamics (N. Zabaras)
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2GT mv 2 21 1
2 2G GT mv I ω
2 21 1
2 2
Translational Rotational
Kinetic energy Kinetic energy
G GT mv I ω
ωrv GG 2 2 21 1
2 2G GT m r ω I ω
2 21( )
2G GI m r ω
21
2OI ω
Translation Rotation General
Kinetic Energy
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Introduction to Dynamics (N. Zabaras)
1 1 2 2T U T
2 2 2 2 2 2
1 1 2 1 2 1 2 2
1 1 1 1 1. ( ) ( ) ( )
2 2 2 2 2O Om I F S W y k s s M m I
S rr
Translation
n
Rotation
Principle of Work and Energy
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Introduction to Dynamics (N. Zabaras)
0
( ) ( )
G
G
A G
L mv
H
H d mv
G
G G
O G G G
L mv
H I ω
H I ω r mv
( )
G
G G
A G G
L mv
H I ω
H I ω d mv
Translation Rotation About a Fixed Axis General Plane Motion
2
2( )
G G
G G
O
I ω mr ω
I m r ω
I ω
Angular Momentum
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Introduction to Dynamics (N. Zabaras)
( )
G G
A G G
H I ω
H I ω d mv
1 2G G G GG
I mv r M dt F r dt I mv r
General Plane Motion
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Introduction to Dynamics (N. Zabaras)
2
10 1 0 0 2( ) ( )
t
tdt H M H
2
1 21
t
tr mv M dt r F dt r m v
2
11 2
t
G G Gt
I ω M dt I ω
1 2G GI mv r M dt F r dt I mv r
Angular Impulse and Momentum Principles
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Introduction to Dynamics (N. Zabaras)
Sample Problem
Uniform sphere of mass m and
radius r is projected along a
rough horizontal surface with a
linear velocity and no angular
velocity. The coefficient of
kinetic friction is
Determine a) the time t2 at which
the sphere will start rolling
without sliding and b) the linear
and angular velocities of the
sphere at time t2.
.k
1v
SOLUTION:
• Apply principle of impulse and
momentum to find variation of linear
and angular velocities with time.
• Relate the linear and angular
velocities when the sphere stops
sliding by noting that the velocity of
the point of contact is zero at that
instant.
• Substitute for the linear and angular
velocities and solve for the time at
which sliding stops.
• Evaluate the linear and angular
velocities at that instant.
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Introduction to Dynamics (N. Zabaras)
Sample Problem
SOLUTION:
• Apply principle of impulse and
momentum to find variation of linear
and angular velocities with time.
0WtNt
y components:
x components:
21
21
vmmgtvm
vmFtvm
k
gtvv k 12
mgWN
moments about G:
22
52
2
mrtrmg
IFtr
k
tr
gk2
52
Sys Momenta1 + Sys Ext Imp1-2 = Sys Momenta2
• Relate linear and angular velocities
when sphere stops sliding by noting
that velocity of point of contact is zero
at that instant.
tr
grgtv
rv
kk
2
51
22
• Substitute for the linear and angular
velocities and solve for the time at
which sliding stops.
g
vt
k1
7
2
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