Layerwise mechanics and finite element for the dynamic analysis of piezoelectric composite plates

被引:266
作者
Saravanos, DA
Heyliger, PR
Hopkins, DA
机构
[1] Structural Mechanics Branch, NASA Lewis Research Center, MS 49-8, Cleveland, OH 44135
基金
美国国家航空航天局;
关键词
D O I
10.1016/S0020-7683(96)00012-1
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Laminate and structural mechanics for the analysis of laminated composite plate structures with piezoelectric actuators and sensors are presented. The theories implement layerwise representations of displacements and electric potential, and can model both the global and local electromechanical response of smart composite laminates. Finite-element formulations are developed for the quasi-static and dynamic analysis of smart composite structures containing piezoelectric layers. Comparisons with an exact solution illustrate the accuracy, robustness and capability of the developed mechanics to capture the global and local response of thin and/or thick laminated piezoelectric plates. Additional correlations and numerical applications demonstrate the unique capabilities of the mechanics in analyzing the static and free vibration response of composite plates with distributed piezoelectric actuators and sensors. Published by Elsevier Science Ltd.
引用
收藏
页码:359 / 378
页数:20
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