期刊文献+

复合材料T型接头承载能力设计研究 被引量:4

Research on Load Capacity Design of Composite T-Joint
下载PDF
导出
摘要 应用商业有限元软件ABAQUS中的内聚单元,对复合材料T型接头的缘条/蒙皮界面失效进行分析,计算结果与试验数据吻合良好。基于有限元结果,提取缘条/蒙皮界面内力,研究结构的失效机理。以缘条和蒙皮厚度为参数进行参数化建模,研究缘条/蒙皮刚度比对界面失效乃至承载能力的影响。最后对缘条/蒙皮刚度比提出设计建议。 The failure of flange/skin interface of T-Joint was simulated by using the cohesive element in the com- mercial software ABAQUS, and the simulations agree well with experimental data. The internal forces on the flange/skin interface were extracted from FEM results, and then their failure mechanism was studied. The flange and skin thickness was considered as parameters to build a parameterized model for studying the effect of stiffness ratios of the flange and the skin on the interface debonding. Finally the design parameters of the stiffness ratio between the flange and the skin were suggested for the design.
出处 《民用飞机设计与研究》 2012年第B11期94-98,共5页 Civil Aircraft Design & Research
关键词 复合材料 T型接头 内聚单元 失效机理 刚度比 Composite T-Joint Cohesive for the design. Element Failure Mechanism Stiffness Ratio
  • 相关文献

参考文献10

  • 1Meeks, C.,Greenhalgh, E.,Falzon, B. Stiffener debond-ing mechanism in post buckled CFRP aerospace plates [ J ].Elsevier Ltd, Composites, Part A 36,2005 : 934-946.
  • 2Cosentino, E.,Weaver, P. M.,2009 - A. A Non - linearanalytical approach for sizing of discrete composite stringer ter-minations [J ] - AIAA Journal, Vol. 47,No. 3,March 2009 ;doi: 10.2514/1.37745.
  • 3I. S. Raju, R. Sistla and T. Krishanmurthy. Fracture me-chanics analyses for shin-stiffener debonding [ J] . EngineeringFracture Mechanics, 1996, 54,(3) : 371-385.
  • 4Jeff W. H. Yap, Murray L. Scott, Rodney S. Thomson, eral. The analysis of skin - to - stiffener debonding in compositeaerospace structures [ J]. Composite Structures,2002,57 : 425-435.
  • 5R. Jones, H. Alesi. On the analysis of composite structureswith material and geometric non - linearities [ J ]. CompositeStructures, 2000’ 50:417-431.
  • 6Q.D. Yang, K. L. Rugg, et al. Failure in the junction re-gion of T-stiffeners: 3D-braided vs. 2D tape laminate stiffeners[J] . International Journal of Solids and Structures,2003,40 :1653-1668.
  • 7Ronald Krueger, Pierre J. Mingue. Analysis of compositepanel-stiffener debonding using a shell/3 D modeling technique[R]. NASA CR-214299, 2006.
  • 8Enile Greenhalgh, Aaron Lewis, et al. Evaluation of tough-ening concepts at structural features in CFRP-Part I: Stiffenerpull-off [J]. Composites, part A, 2006.
  • 9John F. Mandell, Daniel D. Samborsky, et al. Selection offiberglass matrix resins for increased toughness and environmen-tal resistance in wind turbine blades [ R ]. AIAA-0057 , 2000.
  • 10Ronald Krueger, Isabelle L. Paris, T. Kevin O'Brien c,el. Comparison of 2D finite element modeling assumptions withresults from 3D analysis for composite skin - stiffener debonding[J]. Composite Structures, 2002,57:161-168.

同被引文献37

引证文献4

二级引证文献8

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