期刊文献+

缝纫复合材料层合板面内弹性模量分析 被引量:6

ON IN-PLANE ELASTIC MODULUS OF STITCHED COMPOSITE LAMINATES
下载PDF
导出
摘要 基于对缝纫孔附近局部细观结构的分析,提出了一种预测缝纫复合材料层合板面内力学性能的理论模型.从分析缝孔单胞的纤维弯曲几何特征入手,最终得到单向板及层合板的弹性常数.通过有限元分析研究了缝纫参数对复合材料层合板面内等效模量的影响.研究结果表明,缝纫造成单向板及层合板面内材料性质的不均匀,随着缝纫密度和缝纫线直径的增加,层合板的等效模量逐渐降低. A theoretical approach is presented for analyzing the in-plane mechanical properties of the stitched composite laminates based on the microstructures of fibers near the stitch holes. The geometrical characteristics of the distorted fibers in the stitch unit cells are considered. The elastic constants and stiffness matrices of lamina and laminate are obtained finally. The effects of stitching parameters on the equivalent elastic modulus of the laminates are studied using the finite element analysis. The results show that the material properties of stitched composite laminates are inhomogeneous due to stitching, and the equivalent elastic modulus of the laminates decreases with the increase of the stitch density and thread diameter.
出处 《力学与实践》 CSCD 北大核心 2005年第1期36-38,共3页 Mechanics in Engineering
关键词 板面 缝纫线 纤维 细观结构 弹性模量 降低 局部 单向板 等效模量 内力 stitch, composite, laminates, elastic modulus
  • 相关文献

参考文献8

  • 1Dransfield KA,Jain LK,Mai Y-W.Onthe effects of stitching in CFRPs-I. Mode I delamination toughness. Comp Sci Tech, 1998, 58(7): 815~827 被引量:1
  • 2Farley GL. A mechanism responsible for reducing compression strength of through-the-thickness reinforced composite material. Comp Mater, 1992, 26:1784~1795 被引量:1
  • 3Mouritz AP, Gallagher J, Goodwin AA. Flexural and inerlaminar shear properties of stitched GRP laminates following repeated impacts. Com Sci Technol, 1996, 57(8):509~522 被引量:1
  • 4Reed JR. Stitching vs a toughened matrix: compression strength effects. Comp Mater, 1995, 29(18): 2464~2487 被引量:1
  • 5Pang F, Wang CH, Bathgate RG. Creep response of woven fibre composites and the effect of the stitching. Comp Sci and Tech, 1997, 57:91~98 被引量:1
  • 6汪海 刘书田 程耿东.缝纫复合材料板的破坏机理[J].固体力学学报,2002,23:108-113. 被引量:1
  • 7Enboa Wu, Jyue Wang. Behavior of stitched laminates under in-plane tensile and transverse impact loading. Comp Mater, 1995, 29(17): 2254~79 被引量:1
  • 8Larsson F. Damage tolerance of a stitched carb/epoxy laminate. Composites, Part A, 1997, 28:923~934 被引量:1

同被引文献46

引证文献6

二级引证文献25

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