期刊文献+

Z-pins增强层合梁后屈曲分层扩展数值模拟研究 被引量:1

NUMERICAL ANALYSIS OF DELAMINATED BEAM THROUGH-THICKNESS REINFORCED BY Z-PINS
原文传递
导出
摘要 分层损伤是层合复合材料结构的一种最主要的损伤形式,层合板内一旦存在分层损伤,这些分层就会在较低的面内压缩应变下发生失稳和扩展,从而引起结构失效,因此必须采取有效的措施来抑制分层的产生和扩展.目前,一种方法是在层合板内沿厚度方向嵌入Z-pins,以提高其较弱的层间断裂韧性.论文采用考虑一阶剪切的梁单元,结合Z-pins增强体单元,建立了Z-pins横向增强的含对称穿透分层的复合材料层合梁有限元模型,利用数值模拟分析了含分层的层合梁在压缩载荷作用下发生对称失稳时,Z-pins增强体对分层扩展的抑制作用,为进一步的实验研究做出预测.结果表明,复合材料层合梁在对称失稳的情况下,Z-pins增强体能够有效地抑制分层的扩展. Delamination is a major damage occurring in the laminated composite structures due to its weak interlaminar properties.The delamination may propagate at a low in-plane compressive strain,which results in structural failure.Consequently,it is necessary to improve the delamination toughness to retard its imitation and propagation.With through-thickness Z-pins insertion,the delamination toughness of Zpinned laminates can be improved significantly.In this paper,a finite element model of through-width symmetrically delaminated composite beam reinforced by Z-pins was proposed by using beam element with shear effect and Z-pin element.The delaminated composite beam was assumed to buckle in a symmetrical mode under in-plane compression.Numerical analysis was carried out to demonstrate the enhancement of Zpins in delamination propagation.Numerical results showed that Z-pins can effectively improve the in-plane compressive strain of delaminated composite beam.
出处 《固体力学学报》 CAS CSCD 北大核心 2013年第S1期270-275,共6页 Chinese Journal of Solid Mechanics
基金 中央高校基本科研业务费专项资金(2009QN053)资助
关键词 层合板 分层 Z-PINS 后屈曲 扩展 laminated plate delamination Z-pins post buckling propagation
  • 相关文献

参考文献15

  • 1孙先念,刘书田.Z-pins对层合复合材料非对称分层增韧作用参数分析——Ⅰ型层间韧性[J].复合材料学报,2009,26(5):186-192. 被引量:6
  • 2孙先念,郑长良.层合复合材料z-pinning增强技术的力学进展[J].航空学报,2006,27(6):1194-1202. 被引量:27
  • 3H. Ghasemnejad,L. Occhineri,D.T. Swift-Hook.Post-buckling failure in multi-delaminated composite wind turbine blade materials[J]. Materials and Design . 2011 (10)
  • 4Ping Tan,Liyong Tong,Xiannian Sun.Effective properties for plain weave composites through-thickness reinforced with carbon nanotube forests[J]. Composite Structures . 2007 (1)
  • 5MSRao Parlapalli,Dongwei Shu.Buckling analysis of two layer delaminated beams with bridging[J]. European Journal of Mechanics / A Solids . 2005 (5)
  • 6Yao Dai,Chang-qing Sun,Zhong Wu,Wei Tan,Jiawen He.Semi-analytical method of wedge-shaped interface transition layer model in laminated composites[J]. Engineering Fracture Mechanics . 2005 (8)
  • 7Ivana K. Partridge,Denis D.R. Cartié.Delamination resistant laminates by Z-Fiber ? pinning: Part I manufacture and fracture performance[J]. Composites Part A . 2004 (1)
  • 8Xiannian Sun,Liyong Tong,Michael D.K Wood,Yiu-Wing Mai.Effect of stitch distribution on mode I delamination toughness of laminated DCB specimens[J]. Composites Science and Technology . 2004 (7)
  • 9Marcello Grassi,Xiang Zhang.Finite element analyses of mode I interlaminar delamination in z-fibre reinforced composite laminates[J]. Composites Science and Technology . 2003 (12)
  • 10Wenyi Yan,Hong-Yuan Liu,Yiu-Wing Mai.Numerical study on the mode I delamination toughness of z-pinned laminates[J]. Composites Science and Technology . 2003 (10)

二级参考文献31

  • 1韩立军,李铁虎,刘建军,邱海鹏,丁海英.采用Z-Pin增强体的3D炭/炭复合材料层间断裂行为(英文)[J].新型炭材料,2004,19(2):97-102. 被引量:5
  • 2Serge A.Impact on laminated composites:recent advances[J].Applied Mechanics Review,1994,47:517-544.
  • 3范赋群.复合材料损伤与断裂的研究进展[M]∥沈真.复合材料及其结构力学进展.武汉:武汉工业大学出版社,1992.
  • 4陈浩然,孙先念.层合复合材料低速冲击损伤研究[M]∥复合材料结构的力学设计与评估.北京:中国力学学会,1998:96-111.
  • 5Dransfield K A,Baillie C,Mai Y W.Improving the de lamination resistance of CFRP by stitching-a review[J].Composites Science and Technology,1994,50:305-317.
  • 6Mouritz A P,Leong K H,Herszberg.A review of the effect of stitching on the in plane mechanical properties of fibre-reinforced polymer composites[J].Composites,Part A,1997,28:979-991.
  • 7Mouritza A P,Bannister M K,Falzon P J,et al.Review of applications for advanced three dimensional fibre textile composites[J].Composites,Part A,1999,30:1445-1461.
  • 8Emile G,Matthew H.The assessment of novel materials and processes for the impact tolerant design of stiffened composite aerospace structures[J].Composites,Part A,2003,34(2):151-161.
  • 9Freitas G,Magee C,Dardzinski P,et al.Fiber insertion process for improved damage tolerance in aircraft laminates[J].Journal of Advanced Materials,1994,25:36-43.
  • 10Partridge I K,Cartie D D R.Delamination resistant laminates by z-fiber pinning:Part I manufacture and fracture performance[J].Composites,Part A,2005,36 (1):55-64.

共引文献31

同被引文献12

引证文献1

二级引证文献4

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部