A comparative study on the bending, vibration and buckling of viscoelastic sandwich nano-plates based on different nonlocal theories using DC, HDQ and DQ methods

被引:215
作者
Kolahchi, Reza [1 ]
机构
[1] Islamic Azad Univ, Kashan Branch, Dept Mech Engn, Kashan, Iran
关键词
Visco-nano-sandwich plate; Bending; Buckling; Vibration; Different theories; DCM; SHEAR DEFORMATION-THEORY; LAMINATED COMPOSITE; ZIGZAG THEORY; SIZE; CORE; BEHAVIOR; BEAMS; MODEL; LOAD;
D O I
10.1016/j.ast.2017.03.016
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this paper, bending, buckling and buckling of embedded nano-sandwich plates are investigated based on refined zigzag theory (RZT), sinusoidal shear deformation theory (SSDT), first order shear deformation theory (FSDT) and classical plate theory (CPT). In order to present a realistic model, the material properties of system are assumed viscoelastic using Kelvin-Voigt model. The elastic medium is simulated by orthotropic visco-Pasternak medium. Based on energy method and D'Alembert's principle, the derivation of the nonlinear equations of motion is presented. A novel numerical method namely as differential cubature (DC) method is applied for obtaining the static response, the natural frequencies and the buckling loads of nano-sandwich plates. The effects of different parameters such as nonlocal parameter, structural damping, viscoelastic foundation, geometrical parameters, stiffness of core and boundary conditions are shown on the bending, buckling and vibration behaviors of nanostructure. The accuracy of the proposed method is verified by comparing its numerical predictions with other published works as well as solution of system with differential quadrature (DQ) and harmonic differential quadrature (HDQ) methods. The numerical investigation shows that RZT is highly accurate in predicting the deflection, frequency and buckling load of nano-sandwich plates without requiring any shear correction factors. (C) 2017 Elsevier Masson SAS. All rights reserved.
引用
收藏
页码:235 / 248
页数:14
相关论文
共 37 条
[1]   Buckling load design of sandwich panels made with hybrid laminated faces and transversely flexible core [J].
Aiello, Maria Antonietta ;
Ombres, Luciano .
JOURNAL OF SANDWICH STRUCTURES & MATERIALS, 2007, 9 (05) :467-485
[2]   Effect of size on the chaotic behavior of nano resonators [J].
Alemansour, Hamed ;
Miandoab, Ehsan Maani ;
Pishkenari, Hossein Nejat .
COMMUNICATIONS IN NONLINEAR SCIENCE AND NUMERICAL SIMULATION, 2017, 44 :495-505
[3]   Analytical stress analysis of annular FGM sandwich plates with non-uniform shear and normal tractions, employing a zigzag-elasticity plate theory [J].
Alipour, M. M. ;
Shariyat, M. .
AEROSPACE SCIENCE AND TECHNOLOGY, 2014, 32 (01) :235-259
[4]  
[Anonymous], 2012, THESIS POLITECNICO T
[5]   Visco-surface-nonlocal piezoelasticity effects on nonlinear dynamic stability of graphene sheets integrated with ZnO sensors and actuators using refined zigzag theory [J].
Arani, A. Ghorbanpour ;
Kolahchi, R. ;
Zarei, M. Sh. .
COMPOSITE STRUCTURES, 2015, 132 :506-526
[6]   Nonlinear surface and nonlocal piezoelasticity theories for vibration of embedded single-layer boron nitride sheet using harmonic differential quadrature and differential cubature methods [J].
Arani, A. Ghorbanpour ;
Fereidoon, A. ;
Kolahchi, R. .
JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 2015, 26 (10) :1150-1163
[7]   Elastic foundation effect on nonlinear thermo-vibration of embedded double-layered orthotropic graphene sheets using differential quadrature method [J].
Arani, Ali Ghorbanpour ;
Kolahchi, Reza ;
Barzoki, Ali Akbar Mosallaie ;
Mozdianfard, Mohammad Reza ;
Farahani, S. Mosatafa Noudeh .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C-JOURNAL OF MECHANICAL ENGINEERING SCIENCE, 2013, 227 (C4) :862-879
[8]   On the choice of shear correction factor in sandwich structures [J].
Birman, V .
JOURNAL OF SANDWICH STRUCTURES & MATERIALS, 2002, 4 (01) :83-95
[9]  
BRUSH DO, 1975, BUCKLING BARS PLATES
[10]  
Chueng-Yuan C., 1980, NONLINEAR ANAL PLATE