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

复合材料、蜂窝夹层和/或金属结构有限元分析
引用本文:刘夏石.复合材料、蜂窝夹层和/或金属结构有限元分析[J].航空学报,1987,8(4):147-156.
作者姓名:刘夏石
作者单位:中国直升机研究设计所
摘    要: 本文针对复合材料层钣的特点发展一种新的层钣有限元分析方法,建立了等参体元、超参壳元、体-壳过渡元及元外节点元的刚度矩阵。这些元素适用于各向同性材料、正交异性材料、蜂窝夹层和/或复合材料层钣的有限元分析,可以逼真地描述形状复杂的结构;还可以用来解决当前复合材料层钣研究的重大课题——层间应力计算问题。从工程应用出发,探讨了上述各种结构的最大承载能力,利用增量变刚度法提出一种解决复合材料这一非线性问题的分析方法。文中给出了一些算例,计算结果表明,所述方法是十分有效的。

关 键 词:
收稿时间:1985-11-17;

FINITE ELEMENT ANALYSIS FOR COMPOSITE HONEYCOMB SANDWICH AND/OR METAL STRUCTURE
Liu Xiashi.FINITE ELEMENT ANALYSIS FOR COMPOSITE HONEYCOMB SANDWICH AND/OR METAL STRUCTURE[J].Acta Aeronautica et Astronautica Sinica,1987,8(4):147-156.
Authors:Liu Xiashi
Institution:Chinese Helicopter Research and Development
Abstract:This report,aiming at laminated plates made of composite material,has developed a new finite clement analysis method by establishing stiffness matrixes of isoparametric, solid elements, superparametric shell elements, solid-shell trasi-tion elements and elements with out-element ncdes.These elements are available to analysing isotropic/orthotropic material,honeycomb sandwich and/or composite plates. They are able to represent complex structures distinctly and solve the significant subject in composite material research--inter-layer stress analysis. From an engineering application point of view.the maximum strength of, various structures mentioned above is studied and a method solving non-lin,ear problem of composite material is suggested.Also,some of the analysed examples are given at the end of the article.It is shown that the method is very effective.
Keywords:
本文献已被 CNKI 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