Nonlinear free vibration of piezoelectric laminated composite plate

This paper addresses the nonlinear free vibration characteristic of laminated composite plate with embedded and/or surface bonded piezoelectric layer. Nonlinear governing equations are derived in Green-Lagrange sense in the framework of a higher order shear deformation theory. All higher order terms arising from nonlinear strain-displacement relations are included in mathematical formulation. The present plate theory satisfies zero transverse shear strains conditions at the top and bottom surfaces of the plate in von-Karman sense. A C^0 isoparametric finite element is proposed for the present nonlinear model. Comparisons of the present results with those obtained by exact approach show the accuracy and necessity of the model especially for the structures undergoing large deformations. Some new examples covering various features are presented to bring out the different aspects of the model. The results would be useful for the designers.

[1]  Hui-Shen Shen,et al.  Nonlinear vibration and dynamic response of FGM plates with piezoelectric fiber reinforced composite actuators , 2009 .

[2]  Satyajit Panda,et al.  Nonlinear finite element analysis of functionally graded plates integrated with patches of piezoelectric fiber reinforced composite , 2008 .

[3]  Ugo Icardi,et al.  Large-deflection and stress analysis of multilayered plates with induced-strain actuators , 1996 .

[4]  Shanyi Du,et al.  A theoretical analysis of piezoelectric/composite anisotropic laminate with larger-amplitude deflection effect, Part I: Fundamental equations , 2005 .

[5]  J. N. Reddy,et al.  On laminated composite plates with integrated sensors and actuators , 1999 .

[6]  Dimitris A. Saravanos,et al.  Exact free‐vibration analysis of laminated plates with embedded piezoelectric layers , 1995 .

[7]  Ali H. Nayfeh,et al.  A refined nonlinear model of composite plates with integrated piezoelectric actuators and sensors , 1993 .

[8]  J. N. Reddy,et al.  Nonlinear finite element analysis of laminated composite shells with actuating layers , 2006 .

[9]  Jx X. Gao,et al.  Active control of geometrically nonlinear transient vibration of composite plates with piezoelectric actuators , 2003 .

[10]  Anindya Ghoshal,et al.  Non-linear vibration analysis of smart composite structures with discrete delamination using a refined layerwise theory , 2004 .

[11]  Hui‐Shen Shen,et al.  Nonlinear free and forced vibration of simply supported shear deformable laminated plates with piezoelectric actuators , 2005 .

[12]  Dipak K. Maiti,et al.  Post buckling analysis of smart laminated doubly curved shells , 2007 .

[13]  C. K. Lee Theory of laminated piezoelectric plates for the design of distributed sensors/actuators. Part I: Governing equations and reciprocal relationships , 1990 .

[14]  R. Cook,et al.  Concepts and Applications of Finite Element Analysis , 1974 .

[15]  Sung Yi,et al.  Large deformation finite element analyses of composite structures integrated with piezoelectric sensors and actuators , 2000 .

[16]  V. Balamurugan,et al.  Shell finite element for smart piezoelectric composite plate/shell structures and its application to the study of active vibration control , 2001 .

[17]  Carlos A. Mota Soares,et al.  Geometrically non-linear analysis of composite structures with integrated piezoelectric sensors and actuators , 2002 .

[18]  Peter Hagedorn,et al.  Non-linear shear vibrations of piezoceramic actuators , 2005 .

[19]  J. Reddy,et al.  Deformations of Piezothermoelastic Laminates with Internal Electrodes , 2001 .

[20]  H. F. Tiersten,et al.  Linear Piezoelectric Plate Vibrations , 1969 .