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

含孔有限大各向异性板的应力集中
引用本文:许希武,章怡宁,杨旭.含孔有限大各向异性板的应力集中[J].航空学报,1995,16(3):115-120.
作者姓名:许希武  章怡宁  杨旭
作者单位:南京航空航天大学飞行器系,沈阳飞机研究所
摘    要: 利用经典层板理论,将复合材料层板的弹性问题化归为均匀各向异性板求解,采用各向异性体平面弹性理论中的复势方法,以Faber级数和最小二乘边界配置技术为工具,提出了含孔有限大层板应力集中问题的级数解,详细探讨铺层形式、层板大小、椭圆度等诸参数的影响。

关 键 词:结构  

STRESS CONCENTRATION OF FINITE ANISOTROPIC PLATE WITH ELLIPTICAL HOLE
Xu Xiwu.STRESS CONCENTRATION OF FINITE ANISOTROPIC PLATE WITH ELLIPTICAL HOLE[J].Acta Aeronautica et Astronautica Sinica,1995,16(3):115-120.
Authors:Xu Xiwu
Institution:1. Department of Aircraft, Nanjing University of Aeronautics and Astronautics, Nanjin, 210016;2. Shenyang Aircraft Research Institute, Shenyang, 110035
Abstract:Based on the classical laminated plate theory, a finite composite laminated plate with an elliptical hole is treated as an anisotropic multiple connected plate. Using the complex potential method in the plane theory of elasticity of an anisotropic body, an analytical solution concerned with the stress concentration around an elliptical hole in a finite composite laminated plate is obtained with the help of the Faber series expansion and the least square boundary collocation technique. The effects of hole sizes, layups and loading conditions on stress concentration are studied in detail.
Keywords:laminates  stress concentration  holes(mechanics)
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