Predicting progressive delamination of composite material specimens via interface elements

被引:129
作者
Chen, J
Crisfield, M
Kinloch, AJ
Busso, EP
Matthews, FL
Qiu, Y
机构
[1] Univ London Imperial Coll Sci Technol & Med, Dept Aeronaut, Ctr Composite Mat, London SW7 2BY, England
[2] Univ London Imperial Coll Sci Technol & Med, Dept Mech Engn, London, England
来源
MECHANICS OF COMPOSITE MATERIALS AND STRUCTURES | 1999年 / 6卷 / 04期
关键词
D O I
10.1080/107594199305476
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This article describes the application of interface elements to the prediction of progressive delamination in composite materials. The work has been implemented in two separate commercial finite-element computer packages, ABAQUS [1] and LUSAS [2]. In the former case, this has been achieved via a "user subroutine," while in the latter case the elements are embedded directly within the system, either in the standard "release version" of the code or in a research version, to which the authors have access and in which they have implemented various algorithms directly. Comparisons are made with a range of experimental results for composite material specimens. In addition to the finite-element solutions, closed-form results are also presented that are based on a corrected beam theory.
引用
收藏
页码:301 / 317
页数:17
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