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

复合材料层合板的二次失稳和破坏研究
引用本文:朱菊芬,汪海,成万植.复合材料层合板的二次失稳和破坏研究[J].航空学报,1991,12(9):452-458.
作者姓名:朱菊芬  汪海  成万植
作者单位:大连理工大学 (朱菊芬),沈阳飞机研究所 (汪海),沈阳飞机研究所(成万植)
摘    要: 本文采用考虑横向剪切效应的三角形拟协调罚函数单元,推导了带有初始挠度的复合材料层合板在后屈曲阶段的增量平衡方程和相应的切线刚度矩阵,以及非线性特征方程,并以数值计算研究了单元的精度和收敛性,二次分支点的存在性和边界条件、加载方式及铺层次序对二次失稳和破坏载荷的影响。

关 键 词:复合材料板  二次失稳  破坏载荷  拟协调罚单元  

SECONDARY BIFURCATION AND FAILURE STUDY OF COMPOSITE LAMINATES
Dalian University of Technology Zhu Jufen Shanyang Aircraft Research Instiute Wang Hai and Cheng Wanzhi.SECONDARY BIFURCATION AND FAILURE STUDY OF COMPOSITE LAMINATES[J].Acta Aeronautica et Astronautica Sinica,1991,12(9):452-458.
Authors:Dalian University of Technology Zhu Jufen Shanyang Aircraft Research Instiute Wang Hai and Cheng Wanzhi
Institution:Dalian University of Technology Zhu Jufen Shanyang Aircraft Research Instiute Wang Hai and Cheng Wanzhi
Abstract:A fifteen-variables quasi-conforming triangle element technique including transverse shear effect for penalty-finite element method is used in this paper to work out the postbuckling incremental equilibrium equation the corresponding tangent stiffness matrix and nonlinear eigen-equation of composite laminates with inital imperfection. By using numerical calculations, the precision and convergence of the element, the existence of the secondary bifurcation point the effect of boundary conditions, the loading forms and ply configurations on the secondary buckling and failure load are also studied. An effective method is proposed for engineering designers to analyse the instability and even the failure load of structures.
Keywords:composite laminates  secondary bifurcation  failure load  quasi-conforming penalty-finite element  
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