Modelling failure of composite specimens with defects under compression loading

被引:68
作者
Lemanski, S. L. [1 ]
Wang, J. [2 ]
Sutcliffe, M. P. F. [1 ]
Potter, K. D. [2 ]
Wisnom, M. R. [2 ]
机构
[1] Univ Cambridge, Dept Engn, Cambridge CB2 1PZ, England
[2] Univ Bristol, Dept Aerosp Engn, Bristol BS8 1TR, Avon, England
基金
英国工程与自然科学研究理事会;
关键词
Carbon fibre; Defects; Damage mechanics; Finite element analysis; FIBER COMPOSITES; DELAMINATION; STRENGTH; DAMAGE;
D O I
10.1016/j.compositesa.2012.12.007
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Composite structures exhibit many different failure mechanisms, but attempts to model composite failure frequently make a priori assumptions about the mechanism by which failure will occur. Wang et al. [I] conducted compressive tests on four configurations of composite specimen manufactured with out-of-plane waviness created by ply-drop defects. There were significantly different failures for each case. Detailed finite element models of these experiments were developed which include competing failure mechanisms. The model predictions correlate well with experimental results - both qualitatively (location of failure and shape of failed specimen) and quantitatively (failure load). The models are used to identify the progression of failure during the compressive tests, determine the critical failure mechanism for each configuration, and investigate the effect of cohesive parameters upon specimen strength. This modelling approach which includes multiple competing failure mechanisms can be applied to predict failure in situations where the failure mechanism is not known in advance. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码:26 / 36
页数:11
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