Stress and failure analysis of composite laminates with an inclusion under multiaxial compression-tension loading

被引：22

作者：

Berbinau, P ^{[1
]}

Filiou, C ^{[1
]}

Soutis, C ^{[1
]}

机构：

[1] Univ London Imperial Coll Sci Technol & Med, Dept Aeronaut, London SW7 2BY, England

来源：

APPLIED COMPOSITE MATERIALS | 2001年 / 8卷 / 05期

基金：

英国工程与自然科学研究理事会;

关键词：

composite laminates; multi-axial loading; open-hole; filled-hole; inclusion; stress distributions; complex variable mapping; compression; fibre microbuckling; strength prediction;

D O I：

10.1023/A:1011279721719

中图分类号：

TB33 [复合材料];

学科分类号：

摘要：

The present paper investigates the failure of orthotropic laminates with a filled hole subjected to biaxial compression-tension loading. This is an idealised case that simulates a situation where the impact damaged laminate has been repaired by drilling a hole and then plugging the hole with a perfect-fit core made of a dissimilar material. The exact stress distribution in the laminate has been determined using the complex variable mapping method. These stresses are then employed in a fracture mechanics failure model to predict the failure load of a laminate with a filled hole under in-plane compression-dominated multi-axial loading. Failure strength predictions are compared to open hole results and experimental data.

引用

页码：307 / 326

页数：20

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