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含任意分层缝纫正交层合板压缩屈曲分析
引用本文:桂良进,郦正能,章怡宁,杨旭.含任意分层缝纫正交层合板压缩屈曲分析[J].复合材料学报,2001,18(2):97-101.
作者姓名:桂良进  郦正能  章怡宁  杨旭
作者单位:1.北京航空航天大学 飞行器设计与应用力学系, 北京 100083;
基金项目:航空科学基金! (0 0 B5 10 5 2 )
摘    要:建立了分析含任意形状分层的缝纫增强复合材料层合板压缩屈曲问题的连续分析模型。该模型允许缝纫层合板含有一个或多个形状不同的分层。分析结果表明,缝纫针脚在分层区域的分布、缝纫密度和缝线的等效刚度系数对分层子板的压缩屈曲应变均有较大影响。 

关 键 词:复合材料    缝纫    层合板    分层屈曲
文章编号:1000-3851(2001)02-0097-05
收稿时间:2000-03-16
修稿时间:2000-07-12

ANALYSIS ON COMPRESSION BUCKLING OF STITCHED ORTHOTROPIC LAMINATES INCLUDING ARBITRARY DELAMINATION
GUI Liangjin,Li Zhengneng,Zhang Yining,YANG Xu.ANALYSIS ON COMPRESSION BUCKLING OF STITCHED ORTHOTROPIC LAMINATES INCLUDING ARBITRARY DELAMINATION[J].Acta Materiae Compositae Sinica,2001,18(2):97-101.
Authors:GUI Liangjin  Li Zhengneng  Zhang Yining  YANG Xu
Affiliation:1.Dept. of Flight Vehicle Design and Applied Mechanics Beijing University of Aeronautics and Astronautics,Beijing 100083, China;2.Shenyang Institute of Airplane Design, Aviation Industries of China, Shengyang 11035,China
Abstract:A continuous model for determining the buckling strains of stitched laminates including arbitrary embedded delamination is developed. The analysis allows stitched laminates to have a multiple number of delminations of various shapes and sizes, and at any locations. The method treats the discontinuous laminates as a body without delamination but with a force system added at a number of discrete points in the delaminated region so as to make the net interfacial tractions to vanish at these points. Hence, the procedure solves problems of delaminated stitched laminates directly as a continuous system. Numerical results accounting for the effects of location of stitches in the delamination region, stitching density, and equivalent stiffness coefficient of stitching thread on buckling strains are presented.
Keywords:composites  stitching  laminates  delamination buckling
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