微裂纹损伤对纤维复合材料层合板强度的影响

刘军; 邱家宏; 黄宝宗

doi:10.13204/j.gyjz200510015

微裂纹损伤对纤维复合材料层合板强度的影响

doi: 10.13204/j.gyjz200510015

1.
1. 东北大学?理学院?沈阳?110004;
2.
2. 中冶集团建筑研究总院?北京?100088

基金项目:

辽宁省自然科学基金项目(编号:20032026);沈阳市自然科学基金项目(编号:104103610603)。

详细信息

作者简介:
刘军,第一作者,女,1969年6月出生,博士研究生,副教授

中图分类号: TU599
计量
- 文章访问数: 62
- HTML全文浏览量: 3
- PDF下载量: 117
- 被引次数: 0
出版历程
- 收稿日期: 2005-04-01
- 刊出日期: 2005-10-20

INFLUENCE OF MICRO-CRACK DAMAGE ON THE STRENGTH OF FIBER COMPOSITE LAMINATE

1.
1. School of Sciences,Northeastern University Shenyang 110004;
2.
2. Central Research Institute of Building and Construction,MCC Group Beijing 100088

摘要

摘要: 基于连续损伤理论及Hoffman强度准则，采用多标量连续损伤模型和有限元法，对复合材料层合板在横向均布载荷下的损伤破坏过程进行了研究，分析中考虑了几何非线性的影响及单层板失效前由微裂纹损伤所引起的刚度下降。研究表明：微裂纹损伤对破坏区域的演化过程有较大影响；用损伤Hoffman准则得到的层板破坏荷载高于无损Hoffman准则的破坏荷载，提高程度受铺层方式的影响。
- 复合材料层板 /
- 逐步损伤 /
- 多标量 /
- 有限元法
Abstract: Based on the continuous damage theory and Hoffman strength criterion,utilizing multi-scalar damage model and finite element method,the damage and failure of composite laminate under transverse even load are researched.The geometric nonlinear influence and stiffness deduction caused by micro-crack damage before failure of laminate are considered.Results show that evolvement of failure regions is obviously affected by micro-crack;load-carrying capacity of laminate calculated by Hoffman criterion for damage is higher than that by Hoffman criterion for non-damage, the degree is depended on the fiber direction.
- composite laminate /
- progressive damage /
- multi-scalar /
- finite element method

HTML全文

参考文献(8)

Chang F K,Chang K Y.A Progressive Damage Model for Laminated Composites Containing Stress Concentration.Composite Material,1987,21:834～855;

[2] Gotsis P K,Chamis C C,Minnetyan L.Prediction of Composite Laminate Fracture:Micromechanics and Progressive Fracture.Composites Science and Technology,1998,58:1 137～1 149;

[3] Singh S B,Kumar A.Postbuckling Response and Strength of Laminates under Combined In-Plane Loads.Composites Science and Technology,1999,59:727～736;

[4] Sun C T,Tao J.Prediction of Failure Envelopes and Stress/Strain Behavior of Composite Laminates.Composites Science and Technology,1998,58:1 125～1 136;

[5] Hakan K,Rami H A.Progressive Damage and Nonlinear Analysis of Pultruded Composite Structures.Composites,2003,34:235～250;

[6] 华玉,荷庆芝,罗晓东.含圆孔复合材料层板在拉伸载荷下损伤破坏过程的模拟.计算结构力学及其应用,1994,11(40):366～373;

[7] 杨光松.损伤力学与复合材料损伤.北京:国防工业出版社,1995.168～181;

[8] Huang B Z,Zhang F P.Delamination Analysis Based on A Multi-Scalar Damage Model.In:Microstructures and Mechanical Properties of New Engineering Materials.ln:Proceedings of IMMM99.Beijing:Academic Press,1999.135～140

施引文献

资源附件(0)

访问统计