期刊文献+

碳纤维平纹与斜纹编织复合材料低速冲击多尺度分析与对比 被引量:1

Multi-scale analysis and comparison of low-speed impact of carbon fiber plain and twill woven composite materials
下载PDF
导出
摘要 为了探究平纹与斜纹编织复合材料的冲击响应,构建了多尺度框架来进行二者的分析与比较。首先构造出介观下的平纹与斜纹编织结构几何模型来探究二者的力学性能,然后将平纹与斜纹编织几何模型进行局部均匀化从而转化为等效交叉层合板模型,最后把二者的等效交叉模型拓展为宏观下的低速冲击仿真模型,在6 J能量下做了冲击仿真模拟并与实验结果做了对比。仿真和实验结果显示,二者仿真下的冲击力变化趋势与实验下的冲击力变化趋势相似,说明了该多尺度框架的可行性。斜纹编织复合材料的冲击力峰值、冲击力震荡时间以及吸收能量都要高于平纹编织复合材料。 To explore the impact response of the plain and twill woven composites, a multi-scale framework was constructed to analyze and compare. First, the mesoscale representative volume element(RVE) of plain and twill woven composites were established to explore their mechanical properties, then locally homogeneous the mesoscale representative volume element(RVE) of pain and twill woven composites were transformed into equivalent cross lamination(equivalent cross-ply laminate, ECPL) model. Finally, the ECPL model of both was expanded into a macroscopic low-speed impact model, with numerical simulations at 6 J impact energy and compared with the experimental results. The results show that the impact time curves of plain and twill woven composite are similar to the experiments, verifying the effectiveness of the macroscopic model. The impact peak of twill woven composite, impact shock time and energy absorption are higher than the plain woven composite.
作者 刘乐 时建纬 杨晶晶 李成 LIU Le;SHI Jianwei;YANG Jingjing;LI Cheng(School of Mechanical and Power Engineering,Zhengzhou University,Zhengzhou 450001,China)
出处 《复合材料科学与工程》 CAS 北大核心 2023年第1期16-25,106,共11页 Composites Science and Engineering
基金 国家自然科学基金民航联合基金(U1833116) 国家自科基金面上基金(52175153)。
关键词 编织复合材料 等效交叉层合板模型 多尺度模型 低速冲击 woven composites ECPL multi-scale modeling low-speed impact
  • 相关文献

参考文献6

二级参考文献58

  • 1单忠德,康怀镕,臧勇,刘丰.三维织造层间增强的纤维棒复合材料细观结构模型及力学性能有限元模拟[J].复合材料学报,2015,32(1):138-149. 被引量:14
  • 2郭洪宝,贾普荣,王波,矫桂琼,曾增.基于迟滞行为的2D-SiC/SiC复合材料组份力学性能分析[J].力学学报,2015,47(2):260-269. 被引量:7
  • 3梅志远,朱锡,张立军.FRC层合板抗高速冲击机理研究[J].复合材料学报,2006,23(2):143-149. 被引量:28
  • 4SHEN Guan-lin, HU Geng-kai. Mechanics of Composite Materials [ M] .Beijing: Tsinghua University Press, 2006.
  • 5Mouram, Marques A T. Prediction of Low Velocity Impact Damage in Carbon-epoxy Laminates [ J ]. Composites: Part A, 1999 ( 33 ) : 361-368.
  • 6Mouram, Goncalves J P M. Modelling the Interaction between Matrix Cracking and Delamination in Carbon-epoxy Laminates under Low Velocity Impact [ J ]. Composite Science and Technology, 2004 (64) : 1021-1027.
  • 7Choi H Y, Downs R J, Chang F K. A New Approach Toward Un- derstanding Damage Mechanisms and Mechanics of Laminated Com- posites due to Low-velocity Impact [ J ]. Part I-Experiments Composite Materials, 1991 (25) : 992-1011.
  • 8Hitchen S A, Kemp M J. The Effect of Stacking Sequence on Impact Damage in a Carbon Fiber-epoxy Composite [ J ]. Composites, 1995 (26) : 207-214.
  • 9Rong MZ, Zhang MQ, Liu Y, et al. Effect of Stitching on In-plane and Inter laminar Properties of Sisal-epoxy Laminates [ J ]. Journal of Composite Materials, 2002, 36(12) : 105-126.
  • 10Chang F K, Lessad L B. Damage Tolerance of Laminated Composites Containing an Open Hole and Subjected to Compressive Loadings: Par I -Analysis[ J] .Compos Mater., 1991(25) : 2-43.

共引文献39

同被引文献3

引证文献1

二级引证文献2

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