Nonlinear vibrations and damping of fractional viscoelastic rectangular plates

被引:61
作者
Amabili, Marco [1 ]
Balasubramanian, Prabakaran [1 ]
Ferrari, Giovanni [1 ]
机构
[1] McGill Univ, Dept Mech Engn, Macdonald Engn Bldg,817 Sherbrooke St West, Montreal, PQ H3A 0C3, Canada
基金
加拿大自然科学与工程研究理事会; 加拿大创新基金会;
关键词
Nonlinear damping; Nonlinear vibrations; Fractional viscoelasticity; Storage modulus; Rectangular plate; LARGE-AMPLITUDE VIBRATIONS; DAMPED VIBRATIONS; SANDWICH PLATES; CURVED PANELS; STEADY-STATE; MODEL; IDENTIFICATION; DERIVATION; DYNAMICS; CALCULUS;
D O I
10.1007/s11071-020-05892-0
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Damping is largely increasing with the vibration amplitude during nonlinear vibrations of rectangular plates. At the same time, soft materials present an increase in their stiffness with the vibration frequency. These two phenomena appear together and are both explained in the framework of the viscoelasticity. While the literature on nonlinear vibrations of plates is very large, these aspects are rarely touched. The present study applies the fractional linear solid model to describe the viscoelastic material behavior. This allows to capture at the same time (i) the increase in the storage modulus with the vibration frequency and (ii) the frequency-dependent nonlinear damping in nonlinear vibrations of rectangular plates. The solution to the nonlinear vibration problems is obtained through Lagrange equations by deriving the potential energy of the plate and the dissipated energy, both geometrically nonlinear and frequency dependent. The model is then applied to a silicone rubber rectangular plate tested experimentally. The plate was glued to a metal frame and harmonically excited by stepped sine testing at different force levels, and the vibration response was measured by a laser Doppler vibrometer. The comparison of numerical and experimental results was very satisfactorily carried out for: (i) nonlinear vibration responses in the frequency and time domain at different excitation levels, (ii) dissipated energy versus excitation frequency and excitation force, (iii) storage energy and (iv) loss factor, which is particularly interesting to evaluate the plate dissipation versus frequency at different excitation levels. Finally, the linear and nonlinear damping terms are compared.
引用
收藏
页码:3581 / 3609
页数:29
相关论文
共 55 条
[11]   Nonlinear vibrations of viscoelastic rectangular plates [J].
Amabili, Marco .
JOURNAL OF SOUND AND VIBRATION, 2016, 362 :142-156
[12]  
[Anonymous], 2003, Physics of Fractal Operators, Institute for Nonlinear Science, DOI DOI 10.1007/978-0-387-21746-8
[13]   Identification of the viscoelastic response and nonlinear damping of a rubber plate in nonlinear vibration regime [J].
Balasubramanian, Prabakaran ;
Ferrari, Giovanni ;
Amabili, Marco .
MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2018, 111 :376-398
[14]   Experimental and theoretical study on large amplitude vibrations of clamped rubber plates [J].
Balasubramanian, Prabakaran ;
Ferrari, Giovanni ;
Amabili, Marco ;
del Prado, Zenon J. Guzman N. .
INTERNATIONAL JOURNAL OF NON-LINEAR MECHANICS, 2017, 94 :36-45
[15]   Nonlinear dynamic behavior of viscoelastic sandwich composite plates under non-uniform blast load: Theory and experiment [J].
Balkan, Demet ;
Mecitoglu, Zahit .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2014, 72 :85-104
[16]   Complex modes based numerical analysis of viscoelastic sandwich plates vibrations [J].
Bilasse, M. ;
Azrar, L. ;
Daya, E. M. .
COMPUTERS & STRUCTURES, 2011, 89 (7-8) :539-555
[17]   A harmonic balance method for the non-linear vibration of viscoelastic shells [J].
Boutyour, EH ;
Daya, EM ;
Potier-Ferry, M .
COMPTES RENDUS MECANIQUE, 2006, 334 (01) :68-73
[18]   Uncertainty quantification in computational linear structural dynamics for viscoelastic composite structures [J].
Capillon, R. ;
Desceliers, C. ;
Soize, C. .
COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 2016, 305 :154-172
[19]  
Chia C.Y., 1980, Nonlinear Analysis of Plates, V1st
[20]  
Chia C.Y., 1988, APPL MECH REV, V41, P439, DOI 10.1115/1.3151873