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Single Degree of Freedom Systems
(Free Vibrations )
© Dr.V.R Deulgaonkar, 2018
Mechanical Vibrations
Essentials
© Dr.V.R Deulgaonkar, 2018
What is Vibration?????
• Vibration is the physical movement or oscillation of
a mechanical part about a reference position.
• Why do we care for vibration???
Wasted Energy
Major cause of premature component faliure
© Dr.V.R Deulgaonkar, 2018
Vibration Terminology
1) Amplitude: Amplitude is an indicator of the
severity of a vibration. Amplitude can be
expressed as one of the following engineering
units:
a)Velocity b) Acceleration c)Displacement
© Dr.V.R Deulgaonkar, 2018
Velocity
• It is defined as the rate of change of
displacement or rate of change in position.
• It is measured in mm/s, m/s or IPS(Inches Per
Second).
• As it is not frequency related it is the most
accurate measure of vibration.s
© Dr.V.R Deulgaonkar, 2018
Acceleration
• Acceleration is the rate of change of velocity
and is the measurement of the force being
produced.
• Acceleration is expressed in gravitational
forces or “G’s”.
• Acceleration is frequency related.
© Dr.V.R Deulgaonkar, 2018
Displacement
• Displacement is a measure of the actual
distance an object is moving from a reference
point.
• Measured in mm, m inches, etc..
• It is also frequency related.
© Dr.V.R Deulgaonkar, 2018
Elements of a Vibrating System
• Springs: Potential energy storage.
• Mass: Inertial element .
• Damper : Energy dissipation.
© Dr.V.R Deulgaonkar, 2018
Energy Methods
9
• Kinetic Energy
– Discrete masses:
• Point mass: Has translation only, therefore kinetic energy is

Rigid body: Has both translation and rotation, therefore kinetic energy is
 The so called “Energy Methods” draw on the interplay between kinetic and
potential energies associated with a conservative system
© Dr.V.R Deulgaonkar, 2018
Potential Energy Component
• U – change in potential energy of the system from its value in the static-
equilibrium configuration
10
 Conservation of Energy
 Can use with conservative systems only
 At any two different moments of time t1 and t2 we have that
© Dr.V.R Deulgaonkar, 2018
Derivation of EOM
• For the free vibration of an undamped system the energy is partly kinetic and
partly potential.
• Kinetic energy T is stored in the mass by virtue of its velocity
• Potential energy U is stored in the form of strain energy in elastic deformation
or work done in a force field such as gravity.
11
 The expression obtained above after taking the time derivative is (after some
massaging) precisely the EOM
© Dr.V.R Deulgaonkar, 2018
Single Degree of Freedom
Vibrating Systems
© Dr.V.R Deulgaonkar, 2018
One Degree of Freedom Systems
• Single degree Degree of Freedom Un-damped Free
Vibration
k m
x
K (δ+x)
mg
m
δ x
m x’’
F = kδ F = mg
Static Equilibrium δ= static deflection
K = spring rate = force/deflection
X = displacement
© Dr.V.R Deulgaonkar, 2018
One Degree of Freedom Systems
• Single degree Degree of Freedom Un-damped Free Vibration
m
K (δ+x)
mg
x
m x’’
0=Fx∑
0)(2
2
=−++ mgxk
dt
xd
m δ
0'' =−++ mgkkxmx δ
mgk =δsince 0'' =+ kxmx
© Dr.V.R Deulgaonkar, 2018
One Degree of Freedom Systems
• Single degree Degree of Freedom Un-damped Free Vibration
0'' =+ kxmx
0'' =





+ x
m
k
x
m
k
=2
ω
m
k
=ω
0'' 2
=+ xx ω
Solution is of the form of
st
ex = st
sex ='
st
esx 2
'' =
Therefore, by substitution
0'' 2
=+ xx ω 022
=+ stst
ees ω
© Dr.V.R Deulgaonkar, 2018
One Degree of Freedom Systems
• Single degree Degree of Freedom Un-damped Free Vibration
By substitution
022
=+ stst
ees ω
or 022
=+ ωs ωω is −+=−= /2
from Euler identity,
titi
eCeCx ωω −
+= 21
( ) ( )titCtitCx ωωωω sincossincos 21 +++=
Grouping terms
( ) ( ) tiCCtCCx ωω sincos 2121 −++=
© Dr.V.R Deulgaonkar, 2018
One Degree of Freedom Systems
• Single degree Degree of Freedom Un-damped Free Vibration
( ) ( ) tiCCtCCx ωω sincos 2121 −++=
tBtAx ωω sincos +=
( ) ( ) BiCCACCLet =−=+ 2121
A & B are now found from initial conditions
nt)displacemeinitial()0(0@ 0XAxt ===
)0()1()0( BAx +=
tBtXx ωωωω cossin' 0 +−=
00 )1()0()0(' VBXx =+−= ωω
© Dr.V.R Deulgaonkar, 2018
One Degree of Freedom Systems
• Single degree Degree of Freedom Un-damped Free Vibration
00 )1()0()0(' VBXx =+−= ωω
ω
0V
B =
therefore, for a free vibrating single DOF system
t
V
tXtx ω
ω
ω sincos)( 0
0 





+=
m
k
=ω
m
k
fn
π2
1
=
© Dr.V.R Deulgaonkar, 2018
Single Degree of Freedom Damped
Systems
© Dr.V.R Deulgaonkar, 2018
One Degree of Freedom Systems
• Single degree Degree of Freedom Damped Free Vibration
k m
x
K (x)
m
x
m x’’
C (x’)
C
0=Fx∑ 0)(2
2
=++
dt
dx
Cxk
dt
xd
m
© Dr.V.R Deulgaonkar, 2018
One Degree of Freedom Systems
• Single degree Degree of Freedom damped system
0=Fx∑ 0)(2
2
=++
dt
dx
Cxk
dt
xd
m
Utilizing the quadratic equation
02
2
=





+





+ x
m
k
dt
dx
m
C
dt
xd
m
k
m
C
m
C
or
m
k
m
C
m
C
−





−+





−
−





−+





−
=
2
2
2
/
22
4/
λ
© Dr.V.R Deulgaonkar, 2018
One Degree of Freedom Systems
• Single degree Degree of Freedom damped system
m
k
m
C
m
C
ss −





−+





−=
2
21
2
/
2
,
imaginaryand-real,and0,becan
2
2
+=−





m
k
m
C
The solution is of the form
tsts
eCeCtx 21
21)( +=
m
k
m
C
m
C
ss −





−+





−=
2
21
2
/
2
,
© Dr.V.R Deulgaonkar, 2018
One Degree of Freedom Systems
• Expanding
t
m
k
m
C
m
C
t
m
k
m
C
m
C
eCeCtx








−





−





−








−





+





−
+=
22
22
2
22
1)(
or










+=








−





−








−





+






−
t
m
k
m
C
t
m
k
m
C
t
m
C
eCeCetx
22
2
2
2
1
2
)(
imaginaryand-real,and0,becan
2
2
+=−





m
k
m
C
Note that three conditions can occur
© Dr.V.R Deulgaonkar, 2018
One Degree of Freedom Systems
• Single degree Degree of Freedom damped system
– Condition 1, CRITICAL DAMPING
0
2
2
=−





m
k
m
C
kmCor
m
k
m
C
24
2
==





damping)critical(2 cCkmC ==
{ })()1()( 21
2
tCCetx
t
m
C
+=






−
recall
m
k
n =ω
m
k
n =
2
ω
By substitution nc mkmC ω22 ==
© Dr.V.R Deulgaonkar, 2018
One Degree of Freedom Systems
• Single degree Degree of Freedom damped system
– Condition 2, UNDER DAMPING
}{imaginary0
2
2
<−





m
k
m
C
















−





+








−





=






−
t
m
k
m
C
SinCt
m
k
m
C
CosCetx
t
m
C 2
2
2
1
2
22
)(
Note: The system now has damped oscillatory behavior
© Dr.V.R Deulgaonkar, 2018
One Degree of Freedom Systems
• Single degree Degree of Freedom damped system
– Condition 3, OVER DAMPING
Real}{All0
2
2
>−





m
k
m
C
Note: The system now has no oscillatory behavior










+=








−





−








−





+






−
t
m
k
m
C
t
m
k
m
C
t
m
C
eCeCetx
22
2
2
2
1
2
)(
© Dr.V.R Deulgaonkar, 2018
One Degree of Freedom Systems
• Single degree Degree of Freedom damped system
damping)critical(2 cCkmC ==
By definition
ratio)damping(== ξ
cC
C
kmC
km
C
C
C
c
2
2
ξξ ===
therefore
n
m
k
m
km
m
C
ωξξξ ===
2
2
2
© Dr.V.R Deulgaonkar, 2018
One Degree of Freedom Systems
• Single degree Degree of Freedom damped system
also
therefore
n
m
k
m
km
m
C
ωξξξ ===
2
2
2
1
2
2222
2
−=−=−





ξωωωξ nnn
m
k
m
C
12
−= ξωω nd
© Dr.V.R Deulgaonkar, 2018
One Degree of Freedom Systems
• Single degree Degree of Freedom damped system
– Critical Damping
– Over Damped Condition
– Under damping
This is the condition of greatest interest as it represents normal
damping on vehicles. Solve for the constants in the system.
1=ξ
{ })()( 21 tCCetx tn
+= − ωξ
( )
( ) ( ){ }tSinCtCosCetx dd
tn
ωωωξ
21)( += −
1<ξ
( )






+=



 



 −−


 



 −
−
tt
t nn
n
eCeCetx
ωξωξ
ξω
1
2
1
1
22
)(
1>ξ
© Dr.V.R Deulgaonkar, 2018
Under Damped System Behavior
Under Damped System Behavior
-3
-2
-1
0
1
2
3
4
5
6
0 1 2 3
Time (sec)
Displacement(cm)
Forcing function
Displace (cm)
ξ = 0.3 ωn = 7.0 V0 = 0
© Dr.V.R Deulgaonkar, 2018
One Degree of Freedom Systems
• Single degree Degree of Freedom damped system
– Under Damped condition
• @ t = 0
• @ t = 0
( )
( ) ( ){ }tSinCtCosCetx dd
tn
ωωωξ
21)( += −
( )
( ) ( ){ }
( )
( ) ( ){ }tCosCtSinCe
tSinCtCosCe
dt
dx
dddd
t
dd
t
n
n
n
ωωωω
ωωωξ
ωξ
ωξ
21
21
+−+
+−=
−
−
{ } 101 )1()1()0( CXCx ==
{ } { })1()1()1()1( 200 CXV
dt
dx
dn ωωξ +−==
© Dr.V.R Deulgaonkar, 2018
One Degree of Freedom Systems
• Single degree Degree of Freedom damped system
– Under Damped condition
• @ t = 0
{ } { })1()1()1()1( 200 CXV
dt
dx
dn ωωξ +−==
d
n XV
C
ω
ξω 00
2
+
=
( )





 +
+= −
tSin
XV
tCosXetx d
d
n
d
tn
ω
ω
ξω
ωωξ 00
0)(
Under Damped System Behavior
-3
-2
-1
0
1
2
3
4
5
6
0 1 2 3
Time (sec)
Displacement(cm)
Forcing function
Displace (cm)
© Dr.V.R Deulgaonkar, 2018

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Single degree freedom free vibration

  • 1. Single Degree of Freedom Systems (Free Vibrations ) © Dr.V.R Deulgaonkar, 2018
  • 3. What is Vibration????? • Vibration is the physical movement or oscillation of a mechanical part about a reference position. • Why do we care for vibration??? Wasted Energy Major cause of premature component faliure © Dr.V.R Deulgaonkar, 2018
  • 4. Vibration Terminology 1) Amplitude: Amplitude is an indicator of the severity of a vibration. Amplitude can be expressed as one of the following engineering units: a)Velocity b) Acceleration c)Displacement © Dr.V.R Deulgaonkar, 2018
  • 5. Velocity • It is defined as the rate of change of displacement or rate of change in position. • It is measured in mm/s, m/s or IPS(Inches Per Second). • As it is not frequency related it is the most accurate measure of vibration.s © Dr.V.R Deulgaonkar, 2018
  • 6. Acceleration • Acceleration is the rate of change of velocity and is the measurement of the force being produced. • Acceleration is expressed in gravitational forces or “G’s”. • Acceleration is frequency related. © Dr.V.R Deulgaonkar, 2018
  • 7. Displacement • Displacement is a measure of the actual distance an object is moving from a reference point. • Measured in mm, m inches, etc.. • It is also frequency related. © Dr.V.R Deulgaonkar, 2018
  • 8. Elements of a Vibrating System • Springs: Potential energy storage. • Mass: Inertial element . • Damper : Energy dissipation. © Dr.V.R Deulgaonkar, 2018
  • 9. Energy Methods 9 • Kinetic Energy – Discrete masses: • Point mass: Has translation only, therefore kinetic energy is  Rigid body: Has both translation and rotation, therefore kinetic energy is  The so called “Energy Methods” draw on the interplay between kinetic and potential energies associated with a conservative system © Dr.V.R Deulgaonkar, 2018
  • 10. Potential Energy Component • U – change in potential energy of the system from its value in the static- equilibrium configuration 10  Conservation of Energy  Can use with conservative systems only  At any two different moments of time t1 and t2 we have that © Dr.V.R Deulgaonkar, 2018
  • 11. Derivation of EOM • For the free vibration of an undamped system the energy is partly kinetic and partly potential. • Kinetic energy T is stored in the mass by virtue of its velocity • Potential energy U is stored in the form of strain energy in elastic deformation or work done in a force field such as gravity. 11  The expression obtained above after taking the time derivative is (after some massaging) precisely the EOM © Dr.V.R Deulgaonkar, 2018
  • 12. Single Degree of Freedom Vibrating Systems © Dr.V.R Deulgaonkar, 2018
  • 13. One Degree of Freedom Systems • Single degree Degree of Freedom Un-damped Free Vibration k m x K (δ+x) mg m δ x m x’’ F = kδ F = mg Static Equilibrium δ= static deflection K = spring rate = force/deflection X = displacement © Dr.V.R Deulgaonkar, 2018
  • 14. One Degree of Freedom Systems • Single degree Degree of Freedom Un-damped Free Vibration m K (δ+x) mg x m x’’ 0=Fx∑ 0)(2 2 =−++ mgxk dt xd m δ 0'' =−++ mgkkxmx δ mgk =δsince 0'' =+ kxmx © Dr.V.R Deulgaonkar, 2018
  • 15. One Degree of Freedom Systems • Single degree Degree of Freedom Un-damped Free Vibration 0'' =+ kxmx 0'' =      + x m k x m k =2 ω m k =ω 0'' 2 =+ xx ω Solution is of the form of st ex = st sex =' st esx 2 '' = Therefore, by substitution 0'' 2 =+ xx ω 022 =+ stst ees ω © Dr.V.R Deulgaonkar, 2018
  • 16. One Degree of Freedom Systems • Single degree Degree of Freedom Un-damped Free Vibration By substitution 022 =+ stst ees ω or 022 =+ ωs ωω is −+=−= /2 from Euler identity, titi eCeCx ωω − += 21 ( ) ( )titCtitCx ωωωω sincossincos 21 +++= Grouping terms ( ) ( ) tiCCtCCx ωω sincos 2121 −++= © Dr.V.R Deulgaonkar, 2018
  • 17. One Degree of Freedom Systems • Single degree Degree of Freedom Un-damped Free Vibration ( ) ( ) tiCCtCCx ωω sincos 2121 −++= tBtAx ωω sincos += ( ) ( ) BiCCACCLet =−=+ 2121 A & B are now found from initial conditions nt)displacemeinitial()0(0@ 0XAxt === )0()1()0( BAx += tBtXx ωωωω cossin' 0 +−= 00 )1()0()0(' VBXx =+−= ωω © Dr.V.R Deulgaonkar, 2018
  • 18. One Degree of Freedom Systems • Single degree Degree of Freedom Un-damped Free Vibration 00 )1()0()0(' VBXx =+−= ωω ω 0V B = therefore, for a free vibrating single DOF system t V tXtx ω ω ω sincos)( 0 0       += m k =ω m k fn π2 1 = © Dr.V.R Deulgaonkar, 2018
  • 19. Single Degree of Freedom Damped Systems © Dr.V.R Deulgaonkar, 2018
  • 20. One Degree of Freedom Systems • Single degree Degree of Freedom Damped Free Vibration k m x K (x) m x m x’’ C (x’) C 0=Fx∑ 0)(2 2 =++ dt dx Cxk dt xd m © Dr.V.R Deulgaonkar, 2018
  • 21. One Degree of Freedom Systems • Single degree Degree of Freedom damped system 0=Fx∑ 0)(2 2 =++ dt dx Cxk dt xd m Utilizing the quadratic equation 02 2 =      +      + x m k dt dx m C dt xd m k m C m C or m k m C m C −      −+      − −      −+      − = 2 2 2 / 22 4/ λ © Dr.V.R Deulgaonkar, 2018
  • 22. One Degree of Freedom Systems • Single degree Degree of Freedom damped system m k m C m C ss −      −+      −= 2 21 2 / 2 , imaginaryand-real,and0,becan 2 2 +=−      m k m C The solution is of the form tsts eCeCtx 21 21)( += m k m C m C ss −      −+      −= 2 21 2 / 2 , © Dr.V.R Deulgaonkar, 2018
  • 23. One Degree of Freedom Systems • Expanding t m k m C m C t m k m C m C eCeCtx         −      −      −         −      +      − += 22 22 2 22 1)( or           +=         −      −         −      +       − t m k m C t m k m C t m C eCeCetx 22 2 2 2 1 2 )( imaginaryand-real,and0,becan 2 2 +=−      m k m C Note that three conditions can occur © Dr.V.R Deulgaonkar, 2018
  • 24. One Degree of Freedom Systems • Single degree Degree of Freedom damped system – Condition 1, CRITICAL DAMPING 0 2 2 =−      m k m C kmCor m k m C 24 2 ==      damping)critical(2 cCkmC == { })()1()( 21 2 tCCetx t m C +=       − recall m k n =ω m k n = 2 ω By substitution nc mkmC ω22 == © Dr.V.R Deulgaonkar, 2018
  • 25. One Degree of Freedom Systems • Single degree Degree of Freedom damped system – Condition 2, UNDER DAMPING }{imaginary0 2 2 <−      m k m C                 −      +         −      =       − t m k m C SinCt m k m C CosCetx t m C 2 2 2 1 2 22 )( Note: The system now has damped oscillatory behavior © Dr.V.R Deulgaonkar, 2018
  • 26. One Degree of Freedom Systems • Single degree Degree of Freedom damped system – Condition 3, OVER DAMPING Real}{All0 2 2 >−      m k m C Note: The system now has no oscillatory behavior           +=         −      −         −      +       − t m k m C t m k m C t m C eCeCetx 22 2 2 2 1 2 )( © Dr.V.R Deulgaonkar, 2018
  • 27. One Degree of Freedom Systems • Single degree Degree of Freedom damped system damping)critical(2 cCkmC == By definition ratio)damping(== ξ cC C kmC km C C C c 2 2 ξξ === therefore n m k m km m C ωξξξ === 2 2 2 © Dr.V.R Deulgaonkar, 2018
  • 28. One Degree of Freedom Systems • Single degree Degree of Freedom damped system also therefore n m k m km m C ωξξξ === 2 2 2 1 2 2222 2 −=−=−      ξωωωξ nnn m k m C 12 −= ξωω nd © Dr.V.R Deulgaonkar, 2018
  • 29. One Degree of Freedom Systems • Single degree Degree of Freedom damped system – Critical Damping – Over Damped Condition – Under damping This is the condition of greatest interest as it represents normal damping on vehicles. Solve for the constants in the system. 1=ξ { })()( 21 tCCetx tn += − ωξ ( ) ( ) ( ){ }tSinCtCosCetx dd tn ωωωξ 21)( += − 1<ξ ( )       +=          −−         − − tt t nn n eCeCetx ωξωξ ξω 1 2 1 1 22 )( 1>ξ © Dr.V.R Deulgaonkar, 2018
  • 30. Under Damped System Behavior Under Damped System Behavior -3 -2 -1 0 1 2 3 4 5 6 0 1 2 3 Time (sec) Displacement(cm) Forcing function Displace (cm) ξ = 0.3 ωn = 7.0 V0 = 0 © Dr.V.R Deulgaonkar, 2018
  • 31. One Degree of Freedom Systems • Single degree Degree of Freedom damped system – Under Damped condition • @ t = 0 • @ t = 0 ( ) ( ) ( ){ }tSinCtCosCetx dd tn ωωωξ 21)( += − ( ) ( ) ( ){ } ( ) ( ) ( ){ }tCosCtSinCe tSinCtCosCe dt dx dddd t dd t n n n ωωωω ωωωξ ωξ ωξ 21 21 +−+ +−= − − { } 101 )1()1()0( CXCx == { } { })1()1()1()1( 200 CXV dt dx dn ωωξ +−== © Dr.V.R Deulgaonkar, 2018
  • 32. One Degree of Freedom Systems • Single degree Degree of Freedom damped system – Under Damped condition • @ t = 0 { } { })1()1()1()1( 200 CXV dt dx dn ωωξ +−== d n XV C ω ξω 00 2 + = ( )       + += − tSin XV tCosXetx d d n d tn ω ω ξω ωωξ 00 0)( Under Damped System Behavior -3 -2 -1 0 1 2 3 4 5 6 0 1 2 3 Time (sec) Displacement(cm) Forcing function Displace (cm) © Dr.V.R Deulgaonkar, 2018