欢迎光临《计算力学学报》官方网站!
冯世宁,陈浩然,叶林.含界面脱粘压电复合材料层合板的非线性动力稳定性分析[J].计算力学学报,2009,26(2):193~198
本文二维码信息
码上扫一扫!
含界面脱粘压电复合材料层合板的非线性动力稳定性分析
Nonlinear dynamic stability analysis for piezoelectric composite laminates with debonded interfaces
投稿时间:2007-03-14  
DOI:10.7511/jslx20092008
中文关键词:  压电层合板  界面脱粘损伤  高阶剪切变形理论  动力稳定性  参数振动  牵引
英文关键词:piezoelectric composite laminates  interfacial debonding damage  high order shear deformation theory  dynamic stability  parametric vibration  traction
基金项目:国家自然科学基金(10672017);重大基础研究计划(973)项目(2006CB601205)资助项目.
作者单位
冯世宁 大连理工大学 工业装备结构分析国家重点实验室,大连 116023 
陈浩然 大连理工大学 工业装备结构分析国家重点实验室,大连 116023 
叶林 悉尼大学 航天、机械和微电子工程学院,澳大利亚 NSW2006 
摘要点击次数: 1398
全文下载次数: 1134
中文摘要:
      基于Reddy提出的板高阶剪切变形简化理论,研究了含界面脱粘损伤压电复合材料层合板非线性动力稳定性问题。首先,建立了分层模型,推导了考虑几何非线性、阻尼效应、纵向惯性力和力-电耦合效应的Mathieu方程,并且给出了该方程解的解析表达式。其次,通过典型算例讨论了界面脱粘损伤以及反馈控制力对该层合板动力不稳定区域、纵向、横向共振频率和最大"牵引"深度的影响。由典型算例讨论可知:随着层合板界面脱粘损伤的扩大,其动力稳定性能逐渐减弱,其中在损伤较小时,反馈控制力对智能结构几乎没有影响;而在损伤比较大的情况下,反馈控制力将能有效地减少动力不稳定区域重合面积。
英文摘要:
      Nonlinear instability associated with piezoelectric composite laminates with debonded interfaces under dynamic loads has been studied. On basis of Reddy’s simple higher order shear deformation theory, a dynamic instability equation, called Mathieu equation, was deduced, which as considered nonlinear elastic, damping, axial inertia force and electromechanical interaction effects and the corresponding analytical solution was given. From some typical examples, it is clear that the effects of interfacial debonding length and feed-back control on the instability regions, axial and transverse resonance frequency and the maximum deepness of "traction" were discussed. Some typical examples indicate that the dynamic instability behavior of the laminates gradually decreases with increasing interfacial debonding length; However, the effects of feed-back control on the case of laminates with short interfacial debonding damage is rather weakness, while for the case of laminates with long length interfacial debonding damage, with increasing debonding length, feed-back control on the laminates could decreases the interaction regions between axial and transverse parameter vibrations.
查看全文  查看/发表评论  下载PDF阅读器
您是第12829889位访问者
版权所有:《计算力学学报》编辑部
本系统由 北京勤云科技发展有限公司设计