留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

基于应变不变量失效理论的复合材料损伤模拟

李星 关志东 刘璐 黎增山

李星, 关志东, 刘璐, 等 . 基于应变不变量失效理论的复合材料损伤模拟[J]. 北京航空航天大学学报, 2013, 39(2): 190-195.
引用本文: 李星, 关志东, 刘璐, 等 . 基于应变不变量失效理论的复合材料损伤模拟[J]. 北京航空航天大学学报, 2013, 39(2): 190-195.
Li Xing, Guan Zhidong, Liu Lu, et al. Damage simulation of composite materials based on strain invariant failure theory[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(2): 190-195. (in Chinese)
Citation: Li Xing, Guan Zhidong, Liu Lu, et al. Damage simulation of composite materials based on strain invariant failure theory[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(2): 190-195. (in Chinese)

基于应变不变量失效理论的复合材料损伤模拟

基金项目: 国家重点基础研究发展计划(973计划)资助项目(2010CB631103)
详细信息
  • 中图分类号: V257;TB33

Damage simulation of composite materials based on strain invariant failure theory

  • 摘要: 应变不变量失效理论基于物理失效模式判断纤维和基体的损伤,适于研究纤维与基体的细观相互作用及固化残余应力的影响.介绍了应变不变量失效理论的物理背景,建立了正方形、六边形和钻石型细观代表体积单元模型,给出了宏观应变到细观应变的转换方法,提出了相应的失效模式和损伤演化准则.基于应变不变量失效理论求得了CCF300/5228材料体系的机械应变放大系数和热应变放大系数,对CCF300/5228复合材料开孔层合板的拉伸破坏过程进行了模拟,分析了纤维和基体的失效过程.计算与试验结果取得了较好的一致性,证明了该理论的适用性.

     

  • [1] Hinton M J,Kaddour A S,Soden P D.Failure criteria in fibre-reinforced-polymer composites:the world-wide failure exercise [M].London:Elsevier Ltd,2004
    [2] Committee on New Materials for Advanced Civil Aircraft National Materials.New materials for next-generation commercial transports[M].Washington D C:National Academy Press,1996
    [3] Hahn G L.Accelerated insertion of materials-composites(AIM-C) Methodology[M].St Louis:Boeing,2004
    [4] Gosse J H,Christensen S.Strain invariant failure criteria for polymers in composite materials[C]//American Inst Aeronautics and Astronautics Inc.Soatlle:AIAA,2001:45-55
    [5] Li R,Kelly D,Crosky A.An evaluation of failure criteria for matrix induced failure in composite materials[J].Composite Structures,2002,57(1):385-391
    [6] Gosse J H.A damage functional methodology for assessing post-damage initation environments in composite structure[C]//American Inst Aeronautics and Astronautics Inc.Palm Springs:AIAA,2004:1788-1793
    [7] Tay T,Tan V B C,Liu G.A new integrated micro-macro approach to damage and fracture of composites[J].Materials Science and Engineering B:Solid-State Materials for Advanced Technology,2006,132(1/2):138-142
    [8] Jasso A J M,Goodsell J E,Ritchey A J,et al.A parametric study of fiber volume fraction distribution on the failure initiation location in open hole off-axis tensile specimen[J].Composites Science and Technology,2011,71 (16):1819-1825
    [9] Cai H,Miyano Y,Nakada M.Long-term open-hole compression strength of CFRP laminates based on strain invariant failure theory[J].Journal of Thermoplastic Composite Materials,2009,22(1):63-81
    [10] Asp L E,Berglund L A,Talreja R.A criterion for crack initiation in glassy polymers subjected to a composite-like stress state[J].Composites Science and Technology,1996,56(11): 1291- 1301
    [11] Li R,Kelly D,Ness R.Application of a first invariant strain criterion for matrix failure in composite materials[J].Journal of Composite Materials,2003,37(22):1977-2000
    [12] 黎增山,关志东,何为.国产碳纤维增强树脂基复合材料应变不变量性能[J].复合材料学报,2011,28(5):192-196 Li Zengshan,Guan Zhidong,He Wei.Strain invariant failure theory invariant properties of domestic carbon fiber/resin composites[J].Acta Matriae Sinica,2011,28(5):192-196(in Chinese)
    [13] Ng S J,Felsecker A,Meilunas R,et al.SIFT analysis of IM7/5250-4 composites[C]//Soc for the Advancement of Material and Process Engineering.San Diego: [s.n.],2004:129-141
  • 加载中
计量
  • 文章访问数:  1796
  • HTML全文浏览量:  71
  • PDF下载量:  725
  • 被引次数: 0
出版历程
  • 收稿日期:  2011-11-10
  • 网络出版日期:  2013-02-28

目录

    /

    返回文章
    返回
    常见问答