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The 15th World Conference on Earthquake Engineering
       Lisbon (Portugal), 28th September 2012




         Toward an Improved Computational
             Strategy for Vibration-Proof
           Structures Equipped with Nano-
           Enhanced Viscoelastic Devices

             Evangelos Ntotsios, Alessandro Palmeri


School of Civil and Building Engineering, Loughborough University
    <A.Palmeri@LBORO.ac.uk>
Loughborough University




2                   A.Palmeri@LBORO.ac.uk
Outline

• Introduction

• Linear Viscoelastic Structures
    • Generalised Maxwell (GM) model
    • Laguerre’s Polynomial Approximation (LPA)
    • State-space equations of motion

• Non-Linear Viscoelastic Structures

• Numerical Application

• Conclusions

3                                 A.Palmeri@LBORO.ac.uk
Introduction

• Energy-dissipation devices exploiting viscoelastic rubber
  improve the performance of civil engineering structures to
  dynamic loadings
                           Soong, Dargush (1997), Passive Energy Dissipation Systems in Structural Engineering




• Very complicated constitutive laws Vs. Oversimplified design
  rules (particularly in presence of nano-reinforcement)
                     Dall'Asta, Ragni (2008), Earthquake Engineering & Structural Dynamics 37: 1511-1526
                                                         Johnson, Kienholz (1982), AIAA J. 20: 1284-1290



• It is desirable to perform the dynamic analysis of
  viscoelastically-damped structures on a reduced modal space
                                       Zambrano, Inaudi, Kelly (1996), J. Engineering Mechanics 122: 603–612
                                                               Palmeri et al (2004), Wind & Structures 7: 89–106
                                   Palmeri, Muscolino (2011), Structural Control & Health Monitoring 18: 519-539



4                                           A.Palmeri@LBORO.ac.uk
Linear Viscoelastic Structures


• Reaction force in the time domain:
             +¥                           +¥

    r(t) =   ò j (t - s) u(s)ds = R u(t) + ò g(t - s) u(s)ds
             -¥
                                 0
                                          -¥
                                                      


• Depends on equilibrium modulus R0
  and the time-dependent part of the relaxation
  function g(t):
    ì R0 = t®+¥ j (t) = j (¥)
    ï      lim
    í
    ï g(t) = j (t) - j (¥)
    î

5                                       A.Palmeri@LBORO.ac.uk
Generalised Maxwell (GM) Model

• The reaction force can be expressed as
  the superposition of l+1 terms, each one
  associated with a different rigidity
  coefficient Ri
                        
       r(t) = R0 u(t) + åRi li (t)
                       i=1

• The evolution in time of the l internal
  variables λi(t) depends on the
  corresponding relaxation time τi
                    l (t)
      li (t) = u(t) - i
               
                      ti

6                                    A.Palmeri@LBORO.ac.uk
Laguerre’s Polynomial Approximation (LPA)

• The function g(t) is expressed as a single exponential
  function, depending on a single relaxation time τ0,
  modulated by the Laguerre’s polynomials
                                             Palmeri et al (2003), J. Engineering Mechanics 129: 715–724
                     æ t ö        æ t ö
          g(t) = exp ç - ÷ å Ri Li ç ÷
                     è t 0 ø i=1   è t0 ø

• Similarly to the GM model:
                           
    r(t) = R0 u(t) + åRi li (t)
                           i=1
                               i
                      1
    
    li (t) = u(t) -
             
                      ti
                           å l (t) j
                            j=1


7                                           A.Palmeri@LBORO.ac.uk
State-Space Equations of Motion

    • Physical space of the actual DoFs
                                        p      t

      M × u(t) + C × u(t) + K × u(t) + å b j × ò j j (t - s)b T × u(s)ds = f(t)
                                                           j 
                                       j=1     o

    • Modal transformation of coordinates



    • Equations of motion in the modal space




                              Modal relaxation matrix

8                                             A.Palmeri@LBORO.ac.uk
Non-Linear Viscoelastic Structures

• Non-linear device
                                       t

                       (
    r(t) = R0 u(t) + 1+ a u 2 (t)    ) ò g(t - s) u(t)ds =  +  
                                                          R u(t) (1+ a u (t)) R l (t)
                                                            0
                                                                        
                                                                           2

                                                                                   1   1
                                      0
                                                           r0 (t)          r1 (t)
• Matrix form




• Equations of motion in the modal space
    z(t) = F0 × z(t) + F1 ( z(t),t ) × z(t)
    




9                                                  A.Palmeri@LBORO.ac.uk
Numerical Example (1/2)

                                         m3
                                                                         u3 (t)
                         k3                                   k3
                         2                                    2
                                         m2
                                                                         u2 (t)
                         k2             j 2 (t)               k2
                         2                                    2
                                         m1
                                                                         u1 (t)
                         k1             j1 (t)                k1
                         2                                    2
                                                                     ag (t)
                                                                     



               3


               2


               1


               0


               -1


               -2


               -3
                    0   0.5   1   1.5     2       2.5     3        3.5    4   4.5   5




10                                                      A.Palmeri@LBORO.ac.uk
Numerical Example (2/2)

                             m3
                                                           u3 (t)
               k3                               k3
               2                                2
                             m2
                                                           u2 (t)
               k2           j 2 (t)             k2
               2                                2
                             m1
                                                           u1 (t)
               k1           j1 (t)              k1
               2                                2
                                                          ag (t)
                                                          



      5




      0




      -5
           0   2    4   6     8       10   12        14      16     18   20




11                                                                            A.Palmeri@LBORO.ac.uk
Conclusions

•    An novel computational framework has been suggested for the dynamic
     analysis of non-classically damped structures equipped with linear and non-
     linear viscoelastic devices
•    The preliminary results show that the inaccuracy introduced in the numerical
     solution by reducing the size of the problem in the modal space is
     substantially independent of the level of non-linearity of the viscoelastic
     devices
•    This study should be considered as a first step toward a general strategy to
     effectively incorporate accurate rheological information on nano-reinforced
     elastomeric devices in the non-linear time-domain dynamic analysis of
     viscoelastically damped structures
•    Further investigations are currently being developed to validate
     experimentally the proposed procedure for frames made of composite
     beams made with different rubber mixes


12                                        A.Palmeri@LBORO.ac.uk
Future Work

Non-classically non-viscously damped frame
= Assembly of sandwich metal-rubber viscoelastic
   beams with different properties
Steel thickness: 0.006”, 0.100”, 0.015”
Rubber recipe: Natural (control), Low- and High- load
   carbon black, silica




 This work is supported by the EPSRC First Grant
 EP/I033924/1 “TREViS: Tailoring Nano-Reinforced
 Elastomers to Vibrating Structures”

13                                         A.Palmeri@LBORO.ac.uk

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Toward an Improved Computational Strategy for Vibration-Proof Structures Equipped with Nano-Enhanced Viscoelastic Devices

  • 1. The 15th World Conference on Earthquake Engineering Lisbon (Portugal), 28th September 2012 Toward an Improved Computational Strategy for Vibration-Proof Structures Equipped with Nano- Enhanced Viscoelastic Devices Evangelos Ntotsios, Alessandro Palmeri School of Civil and Building Engineering, Loughborough University <A.Palmeri@LBORO.ac.uk>
  • 2. Loughborough University 2 A.Palmeri@LBORO.ac.uk
  • 3. Outline • Introduction • Linear Viscoelastic Structures • Generalised Maxwell (GM) model • Laguerre’s Polynomial Approximation (LPA) • State-space equations of motion • Non-Linear Viscoelastic Structures • Numerical Application • Conclusions 3 A.Palmeri@LBORO.ac.uk
  • 4. Introduction • Energy-dissipation devices exploiting viscoelastic rubber improve the performance of civil engineering structures to dynamic loadings Soong, Dargush (1997), Passive Energy Dissipation Systems in Structural Engineering • Very complicated constitutive laws Vs. Oversimplified design rules (particularly in presence of nano-reinforcement) Dall'Asta, Ragni (2008), Earthquake Engineering & Structural Dynamics 37: 1511-1526 Johnson, Kienholz (1982), AIAA J. 20: 1284-1290 • It is desirable to perform the dynamic analysis of viscoelastically-damped structures on a reduced modal space Zambrano, Inaudi, Kelly (1996), J. Engineering Mechanics 122: 603–612 Palmeri et al (2004), Wind & Structures 7: 89–106 Palmeri, Muscolino (2011), Structural Control & Health Monitoring 18: 519-539 4 A.Palmeri@LBORO.ac.uk
  • 5. Linear Viscoelastic Structures • Reaction force in the time domain: +¥ +¥ r(t) = ò j (t - s) u(s)ds = R u(t) + ò g(t - s) u(s)ds -¥  0 -¥  • Depends on equilibrium modulus R0 and the time-dependent part of the relaxation function g(t): ì R0 = t®+¥ j (t) = j (¥) ï lim í ï g(t) = j (t) - j (¥) î 5 A.Palmeri@LBORO.ac.uk
  • 6. Generalised Maxwell (GM) Model • The reaction force can be expressed as the superposition of l+1 terms, each one associated with a different rigidity coefficient Ri  r(t) = R0 u(t) + åRi li (t) i=1 • The evolution in time of the l internal variables λi(t) depends on the corresponding relaxation time τi  l (t) li (t) = u(t) - i  ti 6 A.Palmeri@LBORO.ac.uk
  • 7. Laguerre’s Polynomial Approximation (LPA) • The function g(t) is expressed as a single exponential function, depending on a single relaxation time τ0, modulated by the Laguerre’s polynomials Palmeri et al (2003), J. Engineering Mechanics 129: 715–724 æ t ö  æ t ö g(t) = exp ç - ÷ å Ri Li ç ÷ è t 0 ø i=1 è t0 ø • Similarly to the GM model:  r(t) = R0 u(t) + åRi li (t) i=1 i 1  li (t) = u(t) -  ti å l (t) j j=1 7 A.Palmeri@LBORO.ac.uk
  • 8. State-Space Equations of Motion • Physical space of the actual DoFs p t M × u(t) + C × u(t) + K × u(t) + å b j × ò j j (t - s)b T × u(s)ds = f(t)   j  j=1 o • Modal transformation of coordinates • Equations of motion in the modal space Modal relaxation matrix 8 A.Palmeri@LBORO.ac.uk
  • 9. Non-Linear Viscoelastic Structures • Non-linear device t ( r(t) = R0 u(t) + 1+ a u 2 (t) ) ò g(t - s) u(t)ds =  +    R u(t) (1+ a u (t)) R l (t) 0  2 1 1 0 r0 (t) r1 (t) • Matrix form • Equations of motion in the modal space z(t) = F0 × z(t) + F1 ( z(t),t ) × z(t)  9 A.Palmeri@LBORO.ac.uk
  • 10. Numerical Example (1/2) m3 u3 (t) k3 k3 2 2 m2 u2 (t) k2 j 2 (t) k2 2 2 m1 u1 (t) k1 j1 (t) k1 2 2 ag (t)  3 2 1 0 -1 -2 -3 0 0.5 1 1.5 2 2.5 3 3.5 4 4.5 5 10 A.Palmeri@LBORO.ac.uk
  • 11. Numerical Example (2/2) m3 u3 (t) k3 k3 2 2 m2 u2 (t) k2 j 2 (t) k2 2 2 m1 u1 (t) k1 j1 (t) k1 2 2 ag (t)  5 0 -5 0 2 4 6 8 10 12 14 16 18 20 11 A.Palmeri@LBORO.ac.uk
  • 12. Conclusions • An novel computational framework has been suggested for the dynamic analysis of non-classically damped structures equipped with linear and non- linear viscoelastic devices • The preliminary results show that the inaccuracy introduced in the numerical solution by reducing the size of the problem in the modal space is substantially independent of the level of non-linearity of the viscoelastic devices • This study should be considered as a first step toward a general strategy to effectively incorporate accurate rheological information on nano-reinforced elastomeric devices in the non-linear time-domain dynamic analysis of viscoelastically damped structures • Further investigations are currently being developed to validate experimentally the proposed procedure for frames made of composite beams made with different rubber mixes 12 A.Palmeri@LBORO.ac.uk
  • 13. Future Work Non-classically non-viscously damped frame = Assembly of sandwich metal-rubber viscoelastic beams with different properties Steel thickness: 0.006”, 0.100”, 0.015” Rubber recipe: Natural (control), Low- and High- load carbon black, silica This work is supported by the EPSRC First Grant EP/I033924/1 “TREViS: Tailoring Nano-Reinforced Elastomers to Vibrating Structures” 13 A.Palmeri@LBORO.ac.uk