Three-Dimensional Solutions for Free Vibrations of Initially-Stressed Thermoelectroelastic Multilayered Plates

Analytic three-dimensional solutions are presented for the free vibration frequencies of initially stressed hybrid multilayered composite plates. The plates consist of a combination of fiber-reinforced cross-ply and piezothermoelastic layers. The initial stresses are generated by either a temperature change and/or an electric field. Sensitivity coefficients are also evaluated and used to study the sensitivity of the vibrational response to variations in the different mechanical, thermal and piezoelectric material properties of the plate. Both the temperature change and the electric field are assumed to be independent of the surface coordinates, but have arbitrary variation through the thickness of the plate. A linear constitutive model is used, and the material properties are assumed to be independent of both the temperature and the electric field. The thermoelectroelastic response of the plate is subjected to time-varying displacements, strains and stresses.

[1]  A. Rao,et al.  Bending, vibration and buckling of simply supported thick orthotropic rectangular plates and laminates , 1970 .

[2]  E. Crawley,et al.  Use of piezoelectric actuators as elements of intelligent structures , 1987 .

[3]  T. Bailey,et al.  Distributed Piezoelectric-Polymer Active Vibration Control of a Cantilever Beam , 1985 .

[4]  George E. Blandford,et al.  Piezothermoelastic composite plate analysis using first-order shear deformation theory , 1994 .

[5]  N. J. Pagano,et al.  Elastic Behavior of Multilayered Bidirectional Composites , 1972 .

[6]  J. Whitney,et al.  Shear Correction Factors for Orthotropic Laminates Under Static Load , 1973 .

[7]  K. Washizu Variational Methods in Elasticity and Plasticity , 1982 .

[8]  C. Fuller,et al.  Piezoelectric Actuators for Distributed Vibration Excitation of Thin Plates , 1991 .

[9]  C. I. Tseng,et al.  Distributed piezoelectric sensor/actuator design for dynamic measurement/control of distributed parameter systems: A piezoelectric finite element approach , 1990 .

[10]  A. Noor,et al.  Three-dimensional solutions for coupled thermoelectroelastic response of multilayered plates , 1995 .

[11]  N. Pagano,et al.  Exact Solutions for Rectangular Bidirectional Composites and Sandwich Plates , 1970 .

[12]  Y. Y. Tang,et al.  DYNAMIC ANALYSIS OF A PIEZOTHERMOELASTIC LAMINATED PLATE , 1995 .

[13]  T. R. Tauchert THERMAL BUCKLING OF THICK ANTISYMMETRIC ANGLE-PLY LAMINATES , 1987 .

[14]  Francis C. Moon,et al.  Laminated piezopolymer plates for torsion and bending sensors and actuators , 1989 .

[15]  Ahmed K. Noor,et al.  Three-Dimensional Solutions for the Free Vibrations and Buckling of Thermally Stressed Multilayered Angle-Ply Composite Plates , 1992 .

[16]  Fan Jiarang,et al.  An exact solution for the statics and dynamics of laminated thick plates with orthotropic layers , 1990 .

[17]  D. H. Robbins,et al.  Analysis of piezoelectrically actuated beams using a layer-wise displacement theory , 1991 .

[18]  Ahmed K. Noor,et al.  Three-dimensional solutions for antisymmetrically laminated anisotropic plates , 1990 .