首页 | 本学科首页   官方微博 | 高级检索  
     检索      

双分层损伤层合板屈曲的有限元分析
引用本文:朱菊芬,郑罡.双分层损伤层合板屈曲的有限元分析[J].航空学报,1999,20(6):562-564.
作者姓名:朱菊芬  郑罡
作者单位:大连理工大学,工程力学研究所,辽宁,大连,116023
基金项目:工业装备结构分析国家重点实验室资助
摘    要: 采用参考面单元技术,建立双分层损伤层合板的有限元模型,研究了不同边界条件下,分层尺寸和位置对层合板压屈载荷的影响。大量计算表明,双分层损伤层合板的压屈载荷完全由其最弱的子层确定。在一定的分层位置范围内,双分层和相应单分层的压屈载荷有极好的一致性。给出的压屈载荷的等值线图可以清晰地描述压屈载荷随分层位置的变化规律。

关 键 词:分层损伤  屈曲  有限元/双分层  参考面单元  

FEM ANALYSIS OF DOUBLE DELAMINATION BUCKLING OF COMPOSITE PLATES
ZHU Ju-fen,ZHENG Gang.FEM ANALYSIS OF DOUBLE DELAMINATION BUCKLING OF COMPOSITE PLATES[J].Acta Aeronautica et Astronautica Sinica,1999,20(6):562-564.
Authors:ZHU Ju-fen  ZHENG Gang
Institution:Dalian University of Technology, Dalian 116023,China
Abstract:The FEM (finite element modal) of double delaminated composite plate is constructed using the technology of reference surface finite element. The effects of size and location of delamination on the buckling of the plate are studied under different boundary conditions. The numerical results show that the buckling loads of the double delaminated laminate depend on the weakest subdelamination thickness within the delaminated region and exhibit that an identity of the buckling loads exists between the double and single delaminated plates under the given region. The variable regularity of buckling loads of the double delaminated plate can be clearly explained from the isoline figure in this paper.
Keywords:delaminated damage  buckling  finite element  double delamination  reference surface element
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号