THROUGH-THICKNESS FAILURE OF LAMINATED CARBON/EPOXY COMPOSITES UNDER COMBINED STRESS

被引：7
|
作者：
CUI, GY
RUIZ, C
机构：
[1] Department of Engineering Science, University of Oxford, Oxford, OX1 3PJ, Parks Road
来源：
COMPOSITES SCIENCE AND TECHNOLOGY | 1995年 / 53卷 / 03期
关键词：
FAILURE; THROUGH-THICKNESS; COMBINED STRESS; LAMINATE; COMPOSITE;
D O I：
10.1016/0266-3538(95)00064-X
中图分类号：
TB33 [复合材料];
学科分类号：
摘要：
The through-thickness failure of laminated composites has been investigated experimentally by the use of waisted C-specimens. In this configuration, the test section is under in-plane tension or compression combined with interlaminar shear and tension. The results show that the interlaminar shear stress has an important effect when combined with in-plane tension, resulting in delamination. The effect is less pronounced under in-plane compression. Fractographic SEM pictures also reveal very different features for each of the stress states.
引用
收藏
页码：253 / 258
页数：6
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