Self-strained piezothermoelastic composite beam analysis using first-order shear deformation theory

Abstract The static response of beams constructed of graphite–epoxy and piezoelectric laminae (hybrid laminate) subjected to electric field and thermal (i.e. self-strained) loading is considered. Two theoretical formulations are considered: uncoupled which ignores the `direct piezoelectric effect' (induced electric field due to variation in stress), and `coupled' which includes the direct piezoelectric effect. A hierarchical finite element approximation of the governing equations using reduced material stiffness coefficients is developed. The electromagnetic potential is assumed to vary piecewise linearly through each piezoelectric lamina and the lamina surface that is in contact with a structural lamina is assumed to be grounded. Beam displacement theory is based on Reissner–Mindlin shear deformation theory. Sample problems are presented demonstrating the accuracy of the developed finite element model, and the response of hybrid laminates to self-strained loading.

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

[2]  D. Saravanos,et al.  Coupled discrete-layer finite elements for laminated piezoelectric platess , 1994 .

[3]  Craig A. Rogers,et al.  Laminate Plate Theory for Spatially Distributed Induced Strain Actuators , 1991 .

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

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

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

[7]  H. Tzou Piezoelectric Shells: Distributed Sensing and Control of Continua , 1993 .

[8]  Ho-Jun Lee,et al.  Generalized finite element formulation for smart multilayered thermal piezoelectric composite plates , 1997 .

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

[10]  Ho-Jun Lee,et al.  Coupled layerwise analysis of thermopiezoelectric composite beams , 1996 .

[11]  George E. Blandford,et al.  High-order thermoelastic composite plate theories: an analytic comparison , 1993 .

[12]  D. J. Inman,et al.  Distributed Parameter Actuators for Structural Control , 1989, 1989 American Control Conference.

[13]  Dimitris A. Saravanos,et al.  Mixed Laminate Theory and Finite Element for Smart Piezoelectric Composite Shell Structures , 1997 .

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

[15]  Baruch Pletner,et al.  Consistent Methodology for the Modeling of Piezolaminated Shells , 1997 .

[16]  Kenneth B. Lazarus,et al.  Induced strain actuation of isotropic and anisotropic plates , 1991 .

[17]  Theodore R. Tauchert Plane piezothermoelastic response of a hybrid laminate : a benchmark problem , 1997 .

[18]  Dimitris A. Saravanos,et al.  Coupled Layerwise Analysis of Composite Beams with Embedded Piezoelectric Sensors and Actuators , 1995 .

[19]  John Anthony Mitchell,et al.  A refined hybrid plate theory for composite laminates with piezoelectric laminae , 1995 .