Vibration of laminated composite plates embedded with shape memory alloy at elevated temperatures

被引:8
|
作者
Duan, B [1 ]
Tawfik, M [1 ]
Goek, SN [1 ]
Ro, JJ [1 ]
Mei, C [1 ]
机构
[1] Old Dominion Univ, Dept Aerosp Engn, Norfolk, VA 23529 USA
关键词
SMA; vibration; composite plate; material nonlinearity;
D O I
10.1117/12.388179
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A finite element formulation and solution procedure for the free vibration behavior of composite plates with embedded shape memory alloy (SMA) at elevated temperatures is presented. The temperature-dependent material properties of SMA and composite matrix, and the geometrical nonlinearity due to large thermal deflection are considered in the formulation. The solution procedure consists of two steps: large thermal deflection is determined first, then followed by the free vibration analysis about the thermally buckled equilibrium position. Examples of hybrid composite plates are given to show the variation of lowest few frequencies versus temperature and the influence of SMA on the natural frequencies at elevated temperatures. Potential applications to frequency turning and sonic fatigue using SMA are discussed.
引用
收藏
页码:366 / 376
页数:11
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