期刊文献+

Low-velocity Impact Damage Analysis of Composite Laminates Using Self-adapting Delamination Element Method 被引量:1

基于自适应分层元的复合材料层合板低速冲击损伤分析(英文)
下载PDF
导出
摘要 On the basis ofa 2D 4-node Mindlin shell element method, a novel self-adapting delamination finite element method is presented, which is developed to model the delamination damage of composite laminates. In the method, the sublaminate elements are generated automatically when the delamination damage occurs or extends. Thus, the complex process and state of delamination damage can be simulated practically with high efficiency for both analysis and modeling. Based on the self-adapting delamination method, linear dynamic finite element damage analysis is performed to simulate the low-velocity impact damage process of three types of mixed woven composite laminates. Taking the frictional force among sublaminations during delaminating and the transverse normal stress into account, the analytical results are consistent with those of the experimental data. On the basis ofa 2D 4-node Mindlin shell element method, a novel self-adapting delamination finite element method is presented, which is developed to model the delamination damage of composite laminates. In the method, the sublaminate elements are generated automatically when the delamination damage occurs or extends. Thus, the complex process and state of delamination damage can be simulated practically with high efficiency for both analysis and modeling. Based on the self-adapting delamination method, linear dynamic finite element damage analysis is performed to simulate the low-velocity impact damage process of three types of mixed woven composite laminates. Taking the frictional force among sublaminations during delaminating and the transverse normal stress into account, the analytical results are consistent with those of the experimental data.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2008年第4期313-319,共7页 中国航空学报(英文版)
基金 National Natural Science Foundation of China (50073002)
关键词 self-adapting delamination element method low-velocity impact DELAMINATION composite laminate self-adapting delamination element method low-velocity impact delamination composite laminate
  • 相关文献

参考文献3

二级参考文献34

共引文献13

同被引文献13

  • 1杜善义.先进复合材料与航空航天[J].复合材料学报,2007,24(1):1-12. 被引量:1019
  • 2Hu Huiwen, Sun C T. The characterization of physical aging in polymeric composites [J]. Composites Science and Technology, 2000, 60(14): 2693-2698.
  • 3Jedidia J, Jacqueminb F, Vautrin A. Accelerated hygrothermal cyclical tests for carbon/epoxy laminates [J]. Composites Part A, 2006, 37(4): 636-645.
  • 4Earl J S, Shenoi R A. Hygrothermal ageing effects on FRP laminate and structural foam materials [J].Composites Part A, 2004, 35(11): 1237-1247.
  • 5Thomas S G. On the use of accelerated test methods for characterization of advanced composite materials, NASA/TP- 2003- 212407 [R]. USA: NASA.
  • 6Marco G, Jerome M, Frederic J, Alain V. On the nonlinear deformations of thin unsymmetric 0/90 composite plates under hygrothermal loads [J]. Composites Part A, 2006,37(4): 624-629.
  • 7Onur S. Analysis of multi-layered composite cylinders under hygrothermal loading [J]. Composites Part A, 2005, 36 (7): 923-933.
  • 8Michael W Hyer. Stress of fiber reinforced composite materials[M]. USA: WCB/McGraw-Hill, 1998: 289-307.
  • 9Zinoviev P, Grigoriev S V, Labedeva O V, Tairova L R. Strength of muti- layered composites under plane stress state [J].Composites Science and Technology, 1998, 58(7) : 1209- 1224.
  • 10Solden P D, Kaddour A S, Hinton M J. Recommendations for designers and researchers resulting from the world-wide failure exercise[J]. Composites Science and Technology, 2004, 64(3/4) : 589-604.

引证文献1

二级引证文献11

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