Simulation of progressive damage development in braided composite tubes under axial compression

被引：88
|
作者：
McGregor, Carla J. [1 ,2 ]
Vaziri, Reza [1 ,2 ]
Poursartip, Anoush [1 ,2 ]
Xiao, Xinran [3 ]
机构：
[1] Univ British Columbia, Dept Civil Engn, Composites Grp, Vancouver, BC V6T 1Z4, Canada
[2] Univ British Columbia, Dept Mat Engn, Composites Grp, Vancouver, BC V6T 1Z4, Canada
[3] GM Corp, Res & Dev, MC 480 106 710, Warren, MI 48090 USA
来源：
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING | 2007年 / 38卷 / 11期
基金：
加拿大自然科学与工程研究理事会;
关键词：
carbon fibre; damage mechanics; finite element analysis (FEA); crashworthiness;
D O I：
10.1016/j.compositesa.2006.10.007
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
A continuum damage mechanics based model for composite materials (CODAM), which has been implemented as a user material model in an explicit finite element code (LS-DYNA), is used to capture the complete tensile and compressive response of a braided composite material. Model parameters are related to experimentally observed behaviour to ensure a physical basis to the model and a crack band scaling approach is used to minimize mesh sensitivity (or lack of objectivity) of the numerical results. The predictive capability of the model is validated against the results from dynamic tube crush experiments. The damage propagation, failure morphology and energy absorption predictions correlate well with the experimental results. (c) 2006 Elsevier Ltd. All rights reserved.
引用
收藏
页码：2247 / 2259
页数：13
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