摘要
推导了十六节点胶单元、二节点钉单元和基于一阶剪切变形理论的八节点等参板单元 ,并通过坐标变换使之用于壳体结构 ,还将相对坐标系内求解法与修正型虚拟的转动刚度法相结合 ,有效地克服了平面单元分析壳体结构所固有的方程病态问题 .对旋转壳体的混合连接节点 ,采用了旋转周期对称理论 ,简化了计算过程 .在此基础上 ,开发出了用于复合材料平板结构和壳体结构中混合连接件的有限元分析软件 .通过算例 ,对复合材料旋转壳体混合连接件中的应力分布进行了分析和讨论 ,得到了一些有益的结果 .
The formulation of sixteen nodded adhesive element,two nodded bolt element and eight nodded isoparametric plate element based on the first order transverse shear effect theory is deduced,which can be used to analyze the laminated shell joint structures by means of the coordinates transformation scheme.Meanwhile the relative coordinate system and modified virtual rotation stiffness techniques are also employed to overcome the ill condition problem of total stiffness matrix of the structures during analysis process successfully. Furthermore,the whole adhesive bolted laminated joint structures can be divided into several repeat subdomains because of the cyclic symmetry characteristic of the joints,therefore,the whole analysis procedure can be greatly simplified.On the basis of the theories and methods described above,a computational program for stress analysis of the adhesive bolted joints of the plate and shell structures has been developed.As numerical examples,some typical laminated joints are studied,and the stress distributions of the joint structures are presented.The discussion conclusions drawn in the paper are useful for researchers and designers of the engineering composite structures.
出处
《大连理工大学学报》
CAS
CSCD
北大核心
2000年第3期280-284,共5页
Journal of Dalian University of Technology
关键词
复合材料
旋转壳体
胶-铆混合连接件
层合板
composite materials
rotary shell
finite element methods/adhesive bolted joint
