宇航材料工艺2018，Vol.48Issue(1)：67-70,4.DOI:10.12044/j.issn.1007-2330.2018.01.013
缝线粗细对复合材料面内弹性模量的损伤分析
Damage Analysis of Elastic Modulus of Composites by Stitching Diameter
乔志炜 1张方超 1胡方田1
作者信息
- 1. 中材科技股份有限公司,南京 210012
- 折叠
摘要
Abstract
A three-dimensional finite element model with different stitching diameter was established based on carbon fabric with 8/5 warp satin weave.The elastic modulus of the composites was predicted by the total damage and partial damage.The thicker stitch thread make the tensile modulus of the composites decrease,and the thinner stitch thread had little effect on the internal elastic modulus.Compared with unstitching,modulus variation of the different diameter is within 9.6％.The elastic modulus of the composites was verified.The results show that the experimental results were larger than the finite element prediction,and the experimental result agrees with prediction.关键词
八枚五飞经面缎/缝线粗细/三维有限元模型/面内弹性模量Key words
8/5 warp satin weave/Stitching radius/Three-dimensional finite element model/In-plane elastic modulus分类
通用工业技术引用本文复制引用
乔志炜,张方超,胡方田..缝线粗细对复合材料面内弹性模量的损伤分析[J].宇航材料工艺,2018,48(1):67-70,4.
