sd lecture04 2d0ffreedom
TRANSCRIPT
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Soil Dynamics
Lecture 04
Systems with Two-Degrees of Freedom
Luis A. Prieto-Portar, August 2006.
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The figure at right shows a simple
non-damped mass and spring system
with two-degrees of freedom.
This simple system can be excited
into vibration in two different ways:
(1) A sinusoidal force is applied to
the mass m1, thereby resulting
in a forced vibration of the
system, or
(2) The system is set to vibrate by
an impact force on the mass m2.
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The calculation of the systems natural frequency. Consider the free-bodydiagram on the previous slide. The differential equations of motion are,
1 1 1 1 2 1 2
2 2 2 2 1
1 2
2
1 2 1 2
22 2 2
0
0
0
0
n n
n
n
m z k z k ( z z ) and
m z k ( z z )
Let z A sin t and z B sin t
Backsubstituting these solution s int o the basic differential equations,
A( k k m ) k B and
Ak ( k m )B
Since A and B are not zero, the n
+ + =
+ =
= =
+ =
+ =
2 2 2
1 2 1 2 2 2
4 21 1 2 2 2 1 1 2
1 2 1 2
0
n n
n n
on trivial solution is,
( k k m )( k m ) k
or ,
k m k m k m k k
m m m m
+ =
+ + + =
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1 2
1 2 1 2
2
1
1 2
1 2 2
4 2 2 2 2 21 1 0
n
nl nl
n nl nl n nl nl
The equation for the natural frequency of the system can be simplified by
msettingm
k kand and
m m m
which yields,
( )( ) ( )( )( )
=
= =+
+ + + + =
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Case 1: The amplitude of vibration for a
force on mass m1.
Consider the case when a vibration is induced
on the system through a force acting upon the
mass m1. The differential equations of motion
are now,
1 1 1 1 2 1 2 0
2 2 2 2 1
1 1 2 2
2
1 1 1 2 2 2 02
2 2 2 1 2
0
0
m z k z k ( z z ) Q sin t and
m z k ( z z )
Let z A sin t and z A sin t
Substituting back int o the d .e.s,
A ( m k k ) A k Q
A ( k m ) A k
+ + =
+ =
= =
+ + =
=
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( ) ( )
( ) ( )( )
2 2
1 2 1 2
2
2 2 2
0 01 22 2
1 1
2 4 2 2 2 2 2
1
1 1
1 1
0
nl nl
nl nl nl nl
nl
From these two equations,we obta in t he two coefficients,
Q ( ) Q ( )A and Am m
where ( )( )( )
Notice that if A then
The is formemain system d by m and k , wherea
= =
= + + + +
= =
2
2 2
nl
s the is
formed by m and k .Thus ,the vibration of the main system can be reduced
or even e li minated
auxiliary syst
by the auxiliary system if its natural frequenc .
The auxiliary system is the
em
vibrationrefore absor era .b
=
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Case 2: An impact force upon mass m2. This case can be modeled by assuming thatthe vibration is induced via an initial velocity v0 to the mass m2. Hence,
( )( )( )
( ) ( )
1 2
1 2
2 1 2 2 1 2
1 22 1 2
2 2 1 2
11 2
1 1 2
2 1 2
1 2 1 2 0
2 2 2 2
1 02 2 2
2 2 2
2 2 2
0 0 0
1
n n
n n
nl n nl n n n
n nnl n n
nl n n nl
nn n
z C sin t C sin t
z D sin t D sin t
At time t z z and z and z v
Substituting ,
sin t sin t z v and
sin t z
= +
= +
= = = = =
=
=
( )
( )( )( )
( )
( )
1 2
2
2 1 2 2
2 1 2 2
2 1
1 2 2
2
0
1 2 1 2
2 2 2 2
1 02 2 2
2 2
2 02 2
n n
n
nl n nl n
nl n n n
nl n
n n n
sin t v
therefore , the amplitudes Z and Z of the masses m and m are ,
Z v and
Z v
=
=
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Example 1.
Calculate the natural frequencies of the system n1 and n2 shown below, ifW1 = 25 lb
and W2 = 5 lb, and the spring constants are k1 = 100 lb/in and k2 = 50 lb/in.
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( ) ( )( )( )
( ) ( )( )
( )
1 2 1 2
1
2
4 2 2 2 2 2
2 2
1 1
1
1 2
2
2
4
1 1 0
50 20
25
100 32 2 1236
25 5
50 32 2 12
625
1
n nl nl n nl nl
nl
nl
n
The equation for the natural frequencies is,
( )( ) ( )( )( )
where,
m W.
m W
.kradians / s
m m
.k
radians / sm
Therefore,
( )(
+ + + + =
= = = =
= = =+ +
= = =
+
( ) ( )
( ) ( )
1 2
2
1
1
2
1 2
2 2 2 2 2
2 24 2 2 2
4 2
2
2
1 0
1 0 2 36 62 1 0 2 36 62 0
6 140
34 70
5 900 000 0
6 140 6 140 4 5 900 000
2,
nl nl n nl nl
n n
n n
nn n
) ( )( )( )
( . ) ( . )( ) ( )
, , ,
, ,rad / s rad
, ,or and / s
+ + + =
+ + + + =
=
+ =
=
=
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Example 2.
Calculate the amplitudes of vibrationZ1 andZ2 for the two masses ofExample 1, if avibratory force Q = 10 sint(lb) is applied to the mass m1 with a frequency =78.54
radians/s.
( ) ( )( )( ) ( ) ( ) ( ) ( ) ( ) ( ) ( )
1 2 1 2
1 1 2
2 4 2 2 2 2 2
4 2 2 2 2 2
1
1 1
78 54 1 0 2 36 62 78 54 1 0 2 36 62
6 000 000
nl nl nl nl
This is case # , where a vibration i s induced on m .We seek the values of A and A ,
( )( )( )
. . . .
, ,
From these two equations,we obta in t he coeff
= + + + +
= + + + +
=
( )
( ) ( ) ( )
( )
( )( )
( )
2
2
2 22 2
0
1 261
2 20
2 261
10 62 78 54
256 10
32 2
0 06
0
12
10 62
256 10
10
32 2 12
nl
nl
icients,
.Q ( )A
mx
. ( )
Q ( ) ( )A
mx
. inches
. inches
. ( )
= = =
= = =
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A free vibration system of coupled translation and rotation.
The 2-D of freedom system shown below will experience both translation and rotation.
The two differential equations of motion of the mass m are,
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1 1 2 2
2
1 1 1 2 2 2
2
2
2
0
0
mz k ( z l ) k ( z l )
mr l k ( z l ) l k ( z l )
where
is the angle of rotation of the mass m ,
ddt
r is the radius of gyration of the body about the center of gravity ,
mr J is the mass moment of inertia about the cen
+ + + =
+ + =
=
=
( )
( )
2 2
1 2 1 1 2 2
2 2 1 1
2
2 2 1 1
0
0
z
z
ter of gravity.
Let ,
k k k and l k l k k
Therefore,
mz k z l k l k
mr k l k l k z
+ = + =
+ + =
+ + =
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1 1 2 2
2
2
00
z
Notice that if l k l k then the mz equation i s independent of .
Similarly ,the mr equation i s independent of z.
Therefore , the two motions, translation and rotation exist independent
of each other ,
mz k z
mr k
The
=
+ =+ =
2
nz
z
nz
n
n
natural circular frequency of translation is,
k
m
and the natural circular frequency of rotation is,
kmr
=
=
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1 1 2 2
2 2 1 11 2 2
1 2
3 22 2
0
0
z
n
However , if l k l k the equations are coupled ,and can be solved ,
k kl k l k E and E and Em m m
So , the coupled differential equations are ,
z E z E
E E zr r
Let the solutions be ,
z Z cos t and
= = =
+ + =
+ + =
= =
( )
( )
1
1
2
2
1 1 2 2 1 1 2 2
2 2
31 2
2 2
1 1 2
2 2
32 2
2 2
2 1 2
n
n n n n
n
n
n
n
cos t
from whence the general equations of motion are ,
z Z cos t Z cos t and cos t cos t
where the amplitude ratios are,
E / rZ E andE E / r
E / rZ E
E E / r
= + = +
= =
= =
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Homework Problem #1.
Determine the natural frequency of the undamped free vibration of the system shown
below.
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Homework Problem #2.
Determine the natural frequency of the undamped free vibration of the system
shown below.
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Homework Problem #3.
Determine the natural frequency and the period of the system shown below.
100 N/mm 200 N/mm
150 N/mm
100 N/mm 150 N/mm 100 kg
Q=50(N)sint where =47 rad/s
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References.
Das, B., Principles of Soil Dynamics, PWS-Kent Publishing Co., Boston, 1993;
Richart F.E., Hall J.R., Woods R.D., Vibrations of Soils and Foundations, Prentice-
Hall Inc., New Jersey, 1970;
Humar J.L., Dynamics of Structures, Prentice-Hall, New Jersey, 1990;
Prakash S., Soil Dynamics, McGraw-Hill, New York, 1981;