Unsymmetric composite laminates morphing via piezoelectric actuators

被引:37
|
作者
Tawfik, Samer A. [1 ]
Dancila, D. Stefan [2 ]
Armanios, Erian [2 ]
机构
[1] Georgia Inst Technol, Sch Aerosp Engn, Atlanta, GA 30332 USA
[2] Univ Texas Arlington, Dept Mech & Aerosp Engn, Arlington, TX 76019 USA
关键词
Buckling; Finite element analysis (FEA); Mechanical testing; SHAPE;
D O I
10.1016/j.compositesa.2011.03.001
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
A composite panel, with a [0/90] unsymmetric layup, exhibits bi-stable anticlastic equilibrium configurations. One way to provide morphing capabilities to such a panel is attained by attaching piezoelectric actuators to its surface. In such a design an electric field is applied to the piezoelectric actuators in order to trigger snap-through behavior of the panel/actuator assembly. A simple cantilever beam configuration is discussed to perform actuator assessment. Results are compared to with predictions from Extended Classical Lamination Theory and finite element analysis. Guidelines are proposed to design a morphing unsymmetric panel/actuator assembly. The panel/actuator(s) assembly is manufactured accordingly. Snap-through experiments are conducted and the ABAQUS finite element software is used to predict snap-through behavior. Analysis predictions are in good agreement with test results. Published by Elsevier Ltd.
引用
收藏
页码:748 / 756
页数:9
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