Non-linear finite element modeling of THUNDER piezoelectric actuators

被引:21
|
作者
Taleghani, BK [1 ]
Campbell, JF [1 ]
机构
[1] NASA, Langley Res Ctr, Vehicle Technol Ctr, Army Res Lab, Hampton, VA 23681 USA
来源
SMART STRUCTURES AND MATERIALS 1999: SMART STRUCTURES AND INTEGRATED SYSTEMS, PTS 1 AND 2 | 1999年 / 3668卷
关键词
NASTRAN; finite element; non-linear; THUNDER; piezoelectric; actuator;
D O I
10.1117/12.350733
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
A NASTRAN non-linear finite element model has been developed for predicting the dome heights of THUNDER (THin Layer UNimorph Ferroelectric DrivER) piezoelectric actuators. To analytically validate the finite element model, a comparison was made with a non-linear plate solution using Von Karmen's approximation. A 500 volt input was used to examine the actuator deformation. The NASTRAN finite element model was also compared with experimental results. Four groups of specimens were fabricated and tested. Four different input voltages, which included 120, 160, 200, and 240 Vp-p with a 0 volts offset, were used for this comparison.
引用
收藏
页码:555 / 566
页数:12
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