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

基于应变不变量失效理论的复合材料损伤模拟

北京航空航天大学航空科学与工程学院, 北京 100191

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
计量
- 文章访问数: 2008
- HTML全文浏览量: 95
- PDF下载量: 738
- 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

Damage simulation of composite materials based on strain invariant failure theory

School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

摘要

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.
- 复合材料 /
- 应变不变量 /
- 失效模式 /
- 损伤演化
Abstract: Strain invariant failure theory (SIFT) estimates failure in fiber and matrix based on mechanical failure modes, which is suitable to study meso-interaction between fiber and matrix, and to evaluate influence of curing residual stress. Mechanical theory background of SIFT was introduced. Square, hexagon and diamond representative volume element(RVE) model in meso level were established. Transition method between macro and meso level was given. Failure mode and damage evolution criteria were proposed. Based on this theory, mechanical strain amplification factors and thermal strain amplification factors of CCF300/5228 were obtained, open hole tensile performance of CCF300/5228 was calculated, fracture process of fiber and matrix was analyzed. Good agreement between numerical results and experiments is observed, which demonstrates the applicability of this theory.
- composite material /
- strain invariant failure theory /
- failure mode /
- damage evolution

HTML全文

参考文献(13)

[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