MEASUREMENT OF THE STATIC COMPRESSIVE STRENGTH OF CARBON-FIBER EPOXY LAMINATES

被引：87

作者：

SOUTIS, C

机构：

[1] Department of Engineering, University of Leicester, Leicester, LE1 7RH, University Road

来源：

COMPOSITES SCIENCE AND TECHNOLOGY | 1991年 / 42卷 / 04期

关键词：

D O I：

10.1016/0266-3538(91)90064-V

中图分类号：

TB33 [复合材料];

学科分类号：

摘要：

This paper describes an experimental study of the compressive failure of T800/924C carbon-fibre/epoxy composite laminates. Unidirectional laminates loaded parallel to the fibres have compressive strengths that are 70% of the tensile strength and fail by fibre-microbuckling. During microbuckling, the fibre debonds from the matrix, and the fibres break in bending. Multidirectional [(+/- 45/0(2))3]s laminates were also tested in compression, and the critical failure mechanism observed was microbuckling of the 0-degrees piles. The failure strain was almost the same as for the undirectional laminate, which indicated that the +/- 45-degrees piles have no significant influence on the failure strength of the 0-degrees plies.

引用

页码：373 / 392

页数：20

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