Geometrically nonlinear analysis of composite piezoelectric plates using meshfree RPIM with a new layerwise approach

被引:0
|
作者
Nourmohammadi, Hossein [1 ]
Behjat, Bashir [1 ]
机构
[1] Sahand Univ Technol, Dept Mech Engn, POB 51335-1996, Tabriz, Iran
关键词
FUNCTIONALLY GRADED SANDWICH; SHEAR DEFORMATION-THEORY; LAMINATED COMPOSITE; FINITE-ELEMENT; THICK COMPOSITE; VIBRATION ANALYSIS; FORMULATION; STRESSES;
D O I
10.1093/qjmam/hbae009
中图分类号
O29 [应用数学];
学科分类号
070104 ;
摘要
In this article, nonlinear analysis of piezoelectric plates using Ferreira layerwise theory based on radial point interpolation method (RPIM) meshfree method is presented. This paper develops Ferreira layerwise method for geometrically nonlinear analysis of composite plates considering piezoelectric effects. Based on this layerwise method, the first-order shear deformation theory is used for layers. Nonlinear Von Karman-type strains are considered to predict the geometrically nonlinear behavior of the piezoelectric plates. By a combination of Ferreira layerwise method and meshfree RPIM and using electrical enthalpy, the matrix form of nonlinear equations is obtained. The Newton-Raphson iteration method is used to obtain the solution of governing nonlinear equations. Using this form of formulation and combining it with the meshfree method increase the linear displacements and stresses accuracy. Consequently, the accuracy of the nonlinear results will increase. Linear and nonlinear solutions are compared with some numerical and exact solutions in the literature. The presented results show that there is a good agreement between them and the exact solution. The results presented in this paper show that Ferreira layerwise model has a good ability to predict the nonlinear behavior of thick or thin piezoelectric composite plates.
引用
收藏
页数:28
相关论文
共 50 条
  • [31] Geometrically nonlinear static and free vibration analysis of functionally graded piezoelectric plates
    Behjat, B.
    Khoshravan, M. R.
    COMPOSITE STRUCTURES, 2012, 94 (03) : 874 - 882
  • [32] Buckling analysis of delaminated composite plates using a novel layerwise theory
    Kharazi, M.
    Ovesy, H. R.
    Mooneghi, M. Asghari
    THIN-WALLED STRUCTURES, 2014, 74 : 246 - 254
  • [33] An optimal approach to active damping of nonlinear vibrations in composite plates using piezoelectric patches
    Saviz, M. R.
    SMART MATERIALS AND STRUCTURES, 2015, 24 (11)
  • [34] Assessment of a layerwise mixed least-squares model for analysis of multilayered piezoelectric composite plates
    Moleiro, F.
    Soares, C. M. Mota
    Soares, C. A. Mota
    Reddy, J. N.
    COMPUTERS & STRUCTURES, 2012, 108 : 14 - 30
  • [35] A GALERKIN MESHFREE METHOD WITH STABILIZED CONFORMING NODAL INTEGRATION FOR GEOMETRICALLY NONLINEAR ANALYSIS OF SHEAR DEFORMABLE PLATES
    Wang, Dongdong
    Sun, Yue
    INTERNATIONAL JOURNAL OF COMPUTATIONAL METHODS, 2011, 8 (04) : 685 - 703
  • [36] Assessment of a Layerwise Mixed Least-Squares Model for Analysis of Multilayered Piezoelectric Composite Plates
    Moleiro, F.
    Mota Soares, C. M.
    Mota Soares, C. A.
    Reddy, J. N.
    PROCEEDINGS OF THE TENTH INTERNATIONAL CONFERENCE ON COMPUTATIONAL STRUCTURES TECHNOLOGY, 2010, 93
  • [37] Geometrically nonlinear analysis of time-dependent composite plates using time function optimization
    Jafari, Nasrin
    Azhari, Mojtaba
    Boroomand, Bijan
    INTERNATIONAL JOURNAL OF NON-LINEAR MECHANICS, 2019, 116 : 219 - 229
  • [38] Geometrically nonlinear analysis of laminated composite plates using RBF-PS meshless method
    Roque, C. M. C.
    Grasa, J.
    COMPOSITE STRUCTURES, 2021, 267
  • [39] Active control of geometrically nonlinear vibrations of functionally graded laminated composite plates using piezoelectric fiber reinforced composites
    Panda, Satyajit
    Ray, M. C.
    JOURNAL OF SOUND AND VIBRATION, 2009, 325 (1-2) : 186 - 205
  • [40] A new symplectic approach for piezoelectric cantilever composite plates
    Leung, A. Y. T.
    Zheng, J. J.
    Lim, C. W.
    Zhang, Xiaochun
    Xu, Xin-Sheng
    Gu, Qian
    COMPUTERS & STRUCTURES, 2008, 86 (19-20) : 1865 - 1874