Modeling of piezolaminated composite shells for vibration control

被引：0
|
作者：
Piéfort, V [1 ]
Loix, N [1 ]
Preumont, A [1 ]
机构：
[1] Free Univ Brussels, Act Struct Lab, B-1050 Brussels, Belgium
来源：
EUROPEAN CONFERENCE ON SPACECRAFT STRUCTURES, MATERIALS AND MECHANICAL TESTING, PROCEEDINGS | 1999年 / 428卷
关键词：
vibration control; piezoelectricity;
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
This paper develops the theory of piezolaminated shells. The fundamental equations governing the equivalent piezoelectric loads and sensor output are derived. The reciprocity between piezoactuation and piezosensing is pointed out. Piezoelectric shell finite elements are developed based on Mindlin elements. Different electrical boundary conditions are examined.
引用
收藏
页码：525 / 530
页数：6
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