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Periodic Structures: A Passive
Vibration Filter

Mohammad Tawfik
Aero631 – Vibrations of Structures
What is a Periodic Structure?
• A structure that consists fundamentally of
a number of identical substructure
components that are joined together to
form a continuous structure

Mohammad Tawfik
Aero631 – Vibrations of Structures
Examples of periodic structures
•
•
•
•
•

Satellite panels
Railway tracks
Aircraft Fuselage
Multistory buildings
Etc…
Etc

Mohammad Tawfik
Aero631 – Vibrations of Structures
Structure Discontinuity!

Mohammad Tawfik
Aero631 – Vibrations of Structures
Types of Discontinuity /
Periodicity
Material Periodicity
y

Geometric/Support
Periodicity

Mohammad Tawfik
Aero631 – Vibrations of Structures
Recall what happens to a
wave as it travels through a
boundary between two
different media

Mohammad Tawfik
Aero631 – Vibrations of Structures
Wave propagation in different
media

Mohammad Tawfik
Aero631 – Vibrations of Structures
Mechanical waves behave in
a similar way!

Mohammad Tawfik
Aero631 – Vibrations of Structures
Stop Bands

• As the wave faces an abrupt change in the geometry a
geometry,
part if it is reflected
• The reflected part, interferes with the incident wave
• At some frequency bands that interference becomes
bands,
destructive creating the “Stop Bands”

Mohammad Tawfik
Aero631 – Vibrations of Structures
Stop bands are the center of
interest for the periodic
p
analysis of structures!

Mohammad Tawfik
Aero631 – Vibrations of Structures
Periodic Analysis of Structures

Mohammad Tawfik
Aero631 – Vibrations of Structures
Why Periodic Analysis?
• Periodic structures can be modeled like
any ordinary structure, BUT
• In a periodic structure, the study of the
structure
behavior of one cell is enough to
determine the stop and pass bands of the
complete structure independent of the
number of cells

Mohammad Tawfik
Aero631 – Vibrations of Structures
How?!

Mohammad Tawfik
Aero631 – Vibrations of Structures
Equations of Motion

 m11 m12  U1   k 11 k 12  U1   F1 
    
m m      
k 22  U 2  F2 
22  U 2  k 21
 21
 k 11   2 m11

k 21   2 m21


 D11
D
 21

k 12   2 m12  U1   F1 
    
2
k 22   m22  U 2   F2 

D12  U1   F1 
 U    F 
D22   2   2 

Rearranging the terms

Mohammad Tawfik
Aero631 – Vibrations of Structures
Equations of Motion
D11U1  D12U 2  F1
D21U1  D22U 2  F2


U 2   D121 D11U1  D121 F1

F2  D21U1  D22U 2
1
12

1
12 1

U 2   D D11U1  D F







F2  D21  D22 D121 D11 U1  D22 D121 F1

Mohammad Tawfik
Aero631 – Vibrations of Structures
Equations of Motion

U 2    D121 D11

 

F2   D21  D22 D121 D11


 U1 

1  
D22 D12   F1 
1
12

D

U 2    U1 
 e 

 F2 
 F1 
1
U1  
 D12 D11

e  

F1   D21  D22 D121 D11


 U1 

1  
 D22 D12   F1 
1
12

D

Mohammad Tawfik
Aero631 – Vibrations of Structures
Equations of Motion
T11 T12  U1   U1 
T T   F   e  F 
 21 22   1 
 1
T11 T12 
e  Eigenvalues 

T21 T22 


Propagation factor

Mohammad Tawfik
Aero631 – Vibrations of Structures
Note!
• The transfer matrix is dependent on the
excitation frequency
• Hence the propagation factor is
Hence,
dependent on the frequency
• Th eigenvalues of th t
The i
l
f the transfer matrix will
f
ti
ill
appear in reciprocal pairs (.

Mohammad Tawfik
Aero631 – Vibrations of Structures
Example: Periodic Spring Mass

• W it down th equations of motion f the
Write d
the
ti
f
ti for th
cell given by 2 half masses and one spring

m 0  u1   k
 0 m      k

 u2  

 k  u1   f1 
    
k  u2   f 2 
Mohammad Tawfik
Aero631 – Vibrations of Structures
Example
• Getting the dynamic stiffness matrix
k   2 m
 k  u1   f1 
 

2 
k   m u2   f 2 
 k

• Rearranging:

 2m
 1
k

k   2m
k 

k






2


u  u 
 1    2 
 2 m   f1   f 2 
1
k 

1

k

Mohammad Tawfik
Aero631 – Vibrations of Structures
Example
• Getting the transfer matrix:

 2m
 1
k

2
2
 k  m  k

k






1 


k   u1   e   u1 
 
 
2
 m   f1 
 f1 
 1
k


• Using Matlab to calculate the eigenvalues,
g
we will get.

Mohammad Tawfik
Aero631 – Vibrations of Structures
The Eigenvalues

Mohammad Tawfik
Aero631 – Vibrations of Structures
The Propagation Factor

Mohammad Tawfik
Aero631 – Vibrations of Structures
Frequency Resp of Cell
Resp.

Mohammad Tawfik
Aero631 – Vibrations of Structures
Freq. Resp
Freq Resp. of 6 Cells

Mohammad Tawfik
Aero631 – Vibrations of Structures
Homework
• Prepare a MATLAB program to perform
the periodic analysis of a bar.

Mohammad Tawfik
Aero631 – Vibrations of Structures
Modeling

K 

M 

&

Eigen
nvalues(


Rearrangement

Eigenvalue problem

T  

(Hz)

Mohammad Tawfik
Aero631 – Vibrations of Structures
Modeling

K 

M 

&

Rea
al(

Rearrangement

Ima
aginary(

Eigenvalue problem

 e
(Hz)

T  



  Propagation Factor

Mohammad Tawfik
Aero631 – Vibrations of Structures
 k11
k
 21

k12  u1   f1 
 u    f 
k 22   2   2 

k

 11

u2 
k12
  k k
 f 2   11 22  k12
 k12


u3    u1 
 e 

f3 
 f1 



1 
k12  u1 

k 22   f1 
 
k12 


EigenvalueT12  T23    
Forward Approach
pp

 k11
k
 21

k31
 k11

 k 21
k31e  


k13  u1   f1 
   
k 23  u2    f 2 

k33  u3   f 3 
   

k12
k 22
k32

k13e   u1   f1 
  

k 23e   u 2    0 
k33  u1   f1 

  

k12
k 22
k32

k11  k13e   k31e    k33

k 21  k 23e 




k12  k32 e    u1  0
    
k 22
 u2  0



Eigenvalue M 1  K    
Reverse Approach
Mohammad Tawfik
Aero631 – Vibrations of Structures
Modeling

K 

&

M 

(
(Hz)

Rearrangement

K     2 M  


(Hz)

Eigenvalue
problem

Imaginary(
Mohammad Tawfik
Aero631 – Vibrations of Structures
Propagation Curves
Forward Approach

Reverse Approach

Imag
ginary(

Attenuation Band

Propagation Curves
p g


(Hz)

Propagation
Bands

(Hz)

Imaginary(
Mohammad Tawfik
Aero631 – Vibrations of Structures
Note!
All the above mentioned
analysis is independent of the
y
p
structure type
(beams, bars, or plates)

Mohammad Tawfik
Aero631 – Vibrations of Structures
So … What really happens?

Mohammad Tawfik
Aero631 – Vibrations of Structures
Experimental Investigation
• Bars with periodic geometry and material
changes.
• Beams with periodic geometry
geometry.
• Plates with periodic geometry.

Mohammad Tawfik
Aero631 – Vibrations of Structures
Periodic Bar

Mohammad Tawfik
Aero631 – Vibrations of Structures
Results

Mohammad Tawfik
Aero631 – Vibrations of Structures
Experimental Setup for the
Periodic Beam

Mohammad Tawfik
Aero631 – Vibrations of Structures
Overview Picture

Mohammad Tawfik
Aero631 – Vibrations of Structures
Beam Cell

Mohammad Tawfik
Aero631 – Vibrations of Structures
Case#1
30

10
9

20

10
7
0
0

500

1000

1500

2000

2500

3000

3500

6
4000
5

-10

4

20
-20

Plain Beam
Periodic Beam
Attenuation Factor

-30

-40

Atte
enuatin Factor (ra
ad)

Transfer Function Amplitu (dB)
ude

8

3
2
1

-50

0
Frequency (Hz)

Mohammad Tawfik
Aero631 – Vibrations of Structures
Case#2
20

10
9

10

0
0

500

1000

1500

2000

2500

3000

3500

7
4000
6

-1 0
5
-2 0
4

P lain B eam
P e riod ic B eam
A ttenu atio n F ac tor

-3 0

Att
tenuatin Factor (ra
ad)

Transfer Function Amplitu (dB)
r
ude

8

3
2

-4 0
4
1
0

-5 0
F re q u e n c y (H z)

Mohammad Tawfik
Aero631 – Vibrations of Structures
Case#3
20

10
9

10

0
0

500

1000

1500

2000

2500

3000

3500

7
4000
6

-10
5
-20
4

-30

Atte
enuatin Factor (ra
ad)

Transfer Function Amplitu (dB)
ude

8

3

Plain Beam
Periodic Beam
Attenuation Factor

2

-40
40
1
-50

0
Frequency (Hz)

Mohammad Tawfik
Aero631 – Vibrations of Structures
Periodic Plate

Mohammad Tawfik
Aero631 – Vibrations of Structures
Problems Associated with 2-D
Structures
• Wave propagates in 2-dimensions
2 dimensions.
• Input-Output relations are not readily
available (no forward approach)
• Requires higher order elements for
numerical analysis
i l
l i

Mohammad Tawfik
Aero631 – Vibrations of Structures
Wave propagates in 2-D
2D

Wave is split
into its components
in X and Y-directions

Mohammad Tawfik
Aero631 – Vibrations of Structures
(
(Hz)

No forward approach 
Reverse approach

K     2 M  


(Hz)

Eigenvalue
problem

Imaginary(
Mohammad Tawfik
Aero631 – Vibrations of Structures
Propagation Surfaces Analytical



x

y

Mead and
Parathan 1979

Mohammad Tawfik
Aero631 – Vibrations of Structures
Requires higher order elements!

64 DOF element used

Mohammad Tawfik
Aero631 – Vibrations of Structures
Propagation Surfaces Numerical



x

y

Mohammad Tawfik
Aero631 – Vibrations of Structures
Experiments

Mohammad Tawfik
Aero631 – Vibrations of Structures
Periodic Plate

Mohammad Tawfik
Aero631 – Vibrations of Structures
Periodic Plate

Mohammad Tawfik
Aero631 – Vibrations of Structures
Propagation Surfaces

Mohammad Tawfik
Aero631 – Vibrations of Structures
Comparison

Mohammad Tawfik
Aero631 – Vibrations of Structures
Effect of shunted inductance

Mohammad Tawfik
Aero631 – Vibrations of Structures
Vibration Absorber

0   Wb 
 M b 
 0
 
 M D  WD 


  K b   K bD   Wb 
0


 K Db   K D   WD 




Mohammad Tawfik
Aero631 – Vibrations of Structures
Adding the Inductance



Inductance

x

y

Mohammad Tawfik
Aero631 – Vibrations of Structures
Further developments

Mohammad Tawfik
Aero631 – Vibrations of Structures
Further Development
• More analytical numerical and
analytical, numerical,
experimental studies need to further
investigate the periodic plate
• Periodic Shells
–L
Longitudinal periodicity i cylindrical shell
it di l
i di it in li d i l h ll
– Circumferential periodicity in axisymmetric
shells

Mohammad Tawfik
Aero631 – Vibrations of Structures
Effect of Shunt Circuit on
Propagation Surfaces
Not Shunted

Shunted

Mohammad Tawfik
Aero631 – Vibrations of Structures

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Periodic Structures

  • 1. Periodic Structures: A Passive Vibration Filter Mohammad Tawfik Aero631 – Vibrations of Structures
  • 2. What is a Periodic Structure? • A structure that consists fundamentally of a number of identical substructure components that are joined together to form a continuous structure Mohammad Tawfik Aero631 – Vibrations of Structures
  • 3. Examples of periodic structures • • • • • Satellite panels Railway tracks Aircraft Fuselage Multistory buildings Etc… Etc Mohammad Tawfik Aero631 – Vibrations of Structures
  • 5. Types of Discontinuity / Periodicity Material Periodicity y Geometric/Support Periodicity Mohammad Tawfik Aero631 – Vibrations of Structures
  • 6. Recall what happens to a wave as it travels through a boundary between two different media Mohammad Tawfik Aero631 – Vibrations of Structures
  • 7. Wave propagation in different media Mohammad Tawfik Aero631 – Vibrations of Structures
  • 8. Mechanical waves behave in a similar way! Mohammad Tawfik Aero631 – Vibrations of Structures
  • 9. Stop Bands • As the wave faces an abrupt change in the geometry a geometry, part if it is reflected • The reflected part, interferes with the incident wave • At some frequency bands that interference becomes bands, destructive creating the “Stop Bands” Mohammad Tawfik Aero631 – Vibrations of Structures
  • 10. Stop bands are the center of interest for the periodic p analysis of structures! Mohammad Tawfik Aero631 – Vibrations of Structures
  • 11. Periodic Analysis of Structures Mohammad Tawfik Aero631 – Vibrations of Structures
  • 12. Why Periodic Analysis? • Periodic structures can be modeled like any ordinary structure, BUT • In a periodic structure, the study of the structure behavior of one cell is enough to determine the stop and pass bands of the complete structure independent of the number of cells Mohammad Tawfik Aero631 – Vibrations of Structures
  • 13. How?! Mohammad Tawfik Aero631 – Vibrations of Structures
  • 14. Equations of Motion   m11 m12  U1   k 11 k 12  U1   F1       m m       k 22  U 2  F2  22  U 2  k 21  21  k 11   2 m11  k 21   2 m21   D11 D  21 k 12   2 m12  U1   F1       2 k 22   m22  U 2   F2  D12  U1   F1   U    F  D22   2   2  Rearranging the terms Mohammad Tawfik Aero631 – Vibrations of Structures
  • 15. Equations of Motion D11U1  D12U 2  F1 D21U1  D22U 2  F2   U 2   D121 D11U1  D121 F1 F2  D21U1  D22U 2 1 12 1 12 1 U 2   D D11U1  D F     F2  D21  D22 D121 D11 U1  D22 D121 F1 Mohammad Tawfik Aero631 – Vibrations of Structures
  • 16. Equations of Motion  U 2    D121 D11     F2   D21  D22 D121 D11   U1   1   D22 D12   F1  1 12 D U 2    U1   e    F2   F1  1 U1    D12 D11  e    F1   D21  D22 D121 D11   U1   1    D22 D12   F1  1 12 D Mohammad Tawfik Aero631 – Vibrations of Structures
  • 17. Equations of Motion T11 T12  U1   U1  T T   F   e  F   21 22   1   1 T11 T12  e  Eigenvalues   T21 T22   Propagation factor Mohammad Tawfik Aero631 – Vibrations of Structures
  • 18. Note! • The transfer matrix is dependent on the excitation frequency • Hence the propagation factor is Hence, dependent on the frequency • Th eigenvalues of th t The i l f the transfer matrix will f ti ill appear in reciprocal pairs (. Mohammad Tawfik Aero631 – Vibrations of Structures
  • 19. Example: Periodic Spring Mass • W it down th equations of motion f the Write d the ti f ti for th cell given by 2 half masses and one spring  m 0  u1   k  0 m      k   u2    k  u1   f1       k  u2   f 2  Mohammad Tawfik Aero631 – Vibrations of Structures
  • 20. Example • Getting the dynamic stiffness matrix k   2 m  k  u1   f1     2  k   m u2   f 2   k • Rearranging:   2m  1 k  k   2m k   k    2  u  u   1    2   2 m   f1   f 2  1 k   1  k Mohammad Tawfik Aero631 – Vibrations of Structures
  • 21. Example • Getting the transfer matrix:   2m  1 k  2 2  k  m  k  k    1    k   u1   e   u1      2  m   f1   f1   1 k  • Using Matlab to calculate the eigenvalues, g we will get. Mohammad Tawfik Aero631 – Vibrations of Structures
  • 22. The Eigenvalues Mohammad Tawfik Aero631 – Vibrations of Structures
  • 23. The Propagation Factor Mohammad Tawfik Aero631 – Vibrations of Structures
  • 24. Frequency Resp of Cell Resp. Mohammad Tawfik Aero631 – Vibrations of Structures
  • 25. Freq. Resp Freq Resp. of 6 Cells Mohammad Tawfik Aero631 – Vibrations of Structures
  • 26. Homework • Prepare a MATLAB program to perform the periodic analysis of a bar. Mohammad Tawfik Aero631 – Vibrations of Structures
  • 27. Modeling K  M  & Eigen nvalues(  Rearrangement Eigenvalue problem T   (Hz) Mohammad Tawfik Aero631 – Vibrations of Structures
  • 28. Modeling K  M  & Rea al( Rearrangement Ima aginary( Eigenvalue problem  e (Hz) T      Propagation Factor Mohammad Tawfik Aero631 – Vibrations of Structures
  • 29.  k11 k  21 k12  u1   f1   u    f  k 22   2   2  k   11  u2  k12   k k  f 2   11 22  k12  k12  u3    u1   e   f3   f1    1  k12  u1   k 22   f1    k12   EigenvalueT12  T23     Forward Approach pp  k11 k  21  k31  k11   k 21 k31e    k13  u1   f1      k 23  u2    f 2   k33  u3   f 3      k12 k 22 k32 k13e   u1   f1      k 23e   u 2    0  k33  u1   f1      k12 k 22 k32 k11  k13e   k31e    k33  k 21  k 23e    k12  k32 e    u1  0      k 22  u2  0  Eigenvalue M 1  K     Reverse Approach Mohammad Tawfik Aero631 – Vibrations of Structures
  • 30. Modeling K  & M  ( (Hz) Rearrangement K     2 M    (Hz) Eigenvalue problem Imaginary( Mohammad Tawfik Aero631 – Vibrations of Structures
  • 31. Propagation Curves Forward Approach Reverse Approach Imag ginary( Attenuation Band Propagation Curves p g  (Hz) Propagation Bands (Hz) Imaginary( Mohammad Tawfik Aero631 – Vibrations of Structures
  • 32. Note! All the above mentioned analysis is independent of the y p structure type (beams, bars, or plates) Mohammad Tawfik Aero631 – Vibrations of Structures
  • 33. So … What really happens? Mohammad Tawfik Aero631 – Vibrations of Structures
  • 34. Experimental Investigation • Bars with periodic geometry and material changes. • Beams with periodic geometry geometry. • Plates with periodic geometry. Mohammad Tawfik Aero631 – Vibrations of Structures
  • 35. Periodic Bar Mohammad Tawfik Aero631 – Vibrations of Structures
  • 36. Results Mohammad Tawfik Aero631 – Vibrations of Structures
  • 37. Experimental Setup for the Periodic Beam Mohammad Tawfik Aero631 – Vibrations of Structures
  • 38. Overview Picture Mohammad Tawfik Aero631 – Vibrations of Structures
  • 39. Beam Cell Mohammad Tawfik Aero631 – Vibrations of Structures
  • 40. Case#1 30 10 9 20 10 7 0 0 500 1000 1500 2000 2500 3000 3500 6 4000 5 -10 4 20 -20 Plain Beam Periodic Beam Attenuation Factor -30 -40 Atte enuatin Factor (ra ad) Transfer Function Amplitu (dB) ude 8 3 2 1 -50 0 Frequency (Hz) Mohammad Tawfik Aero631 – Vibrations of Structures
  • 41. Case#2 20 10 9 10 0 0 500 1000 1500 2000 2500 3000 3500 7 4000 6 -1 0 5 -2 0 4 P lain B eam P e riod ic B eam A ttenu atio n F ac tor -3 0 Att tenuatin Factor (ra ad) Transfer Function Amplitu (dB) r ude 8 3 2 -4 0 4 1 0 -5 0 F re q u e n c y (H z) Mohammad Tawfik Aero631 – Vibrations of Structures
  • 42. Case#3 20 10 9 10 0 0 500 1000 1500 2000 2500 3000 3500 7 4000 6 -10 5 -20 4 -30 Atte enuatin Factor (ra ad) Transfer Function Amplitu (dB) ude 8 3 Plain Beam Periodic Beam Attenuation Factor 2 -40 40 1 -50 0 Frequency (Hz) Mohammad Tawfik Aero631 – Vibrations of Structures
  • 43. Periodic Plate Mohammad Tawfik Aero631 – Vibrations of Structures
  • 44. Problems Associated with 2-D Structures • Wave propagates in 2-dimensions 2 dimensions. • Input-Output relations are not readily available (no forward approach) • Requires higher order elements for numerical analysis i l l i Mohammad Tawfik Aero631 – Vibrations of Structures
  • 45. Wave propagates in 2-D 2D Wave is split into its components in X and Y-directions Mohammad Tawfik Aero631 – Vibrations of Structures
  • 46. ( (Hz) No forward approach  Reverse approach K     2 M    (Hz) Eigenvalue problem Imaginary( Mohammad Tawfik Aero631 – Vibrations of Structures
  • 47. Propagation Surfaces Analytical  x y Mead and Parathan 1979 Mohammad Tawfik Aero631 – Vibrations of Structures
  • 48. Requires higher order elements! 64 DOF element used Mohammad Tawfik Aero631 – Vibrations of Structures
  • 49. Propagation Surfaces Numerical  x y Mohammad Tawfik Aero631 – Vibrations of Structures
  • 50. Experiments Mohammad Tawfik Aero631 – Vibrations of Structures
  • 51. Periodic Plate Mohammad Tawfik Aero631 – Vibrations of Structures
  • 52. Periodic Plate Mohammad Tawfik Aero631 – Vibrations of Structures
  • 53. Propagation Surfaces Mohammad Tawfik Aero631 – Vibrations of Structures
  • 54. Comparison Mohammad Tawfik Aero631 – Vibrations of Structures
  • 55. Effect of shunted inductance Mohammad Tawfik Aero631 – Vibrations of Structures
  • 56. Vibration Absorber  0   Wb   M b   0    M D  WD      K b   K bD   Wb  0    K Db   K D   WD     Mohammad Tawfik Aero631 – Vibrations of Structures
  • 57. Adding the Inductance  Inductance x y Mohammad Tawfik Aero631 – Vibrations of Structures
  • 58. Further developments Mohammad Tawfik Aero631 – Vibrations of Structures
  • 59. Further Development • More analytical numerical and analytical, numerical, experimental studies need to further investigate the periodic plate • Periodic Shells –L Longitudinal periodicity i cylindrical shell it di l i di it in li d i l h ll – Circumferential periodicity in axisymmetric shells Mohammad Tawfik Aero631 – Vibrations of Structures
  • 60. Effect of Shunt Circuit on Propagation Surfaces Not Shunted Shunted Mohammad Tawfik Aero631 – Vibrations of Structures