Evolution behavior of major Poisson's ratio of 2D-C/SiC composites

被引:0
|
作者
Zheng R. [1 ]
Yang C. [1 ]
Qiao C. [2 ]
Jia F. [3 ]
机构
[1] School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an
[2] College of Civil and Resource Engineering, University of Science and Technology Beijing, Beijing
[3] School of Mechano-Electronic Engineering, Xidian University, Xi'an
来源
Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica | 2023年 / 40卷 / 06期
基金
中国国家自然科学基金;
关键词
ceramic matrix composites; Mini composite model; Poisson's ratio; thermal residual stress;
D O I
10.13801/j.cnki.fhclxb.20220913.003
中图分类号
学科分类号
摘要
Poisson's ratio is one of the important parameters in the analysis of mechanical properties of materials and structures. In this paper, the nonlinear evolution behavior of major Poisson's ratio of 2D-C/SiC composites was studied. Firstly, based on Mini composite model and cross-ply laminate model, the thermal residual stress calculation model of 2D-C/SiC composites was established considering the transverse isotropic property of fiber. Secondly, the major Poisson's ratio calculation model of 2D-C/SiC composites was established by using shear-lag theory and classical laminate theory while considering the damage and thermal residual stress release mechanisms of the material. Finally, the strain response and Poisson's ratio evolution of the material were characterized by experiments, and the theoretical model was analyzed and verified. The results show that the internal thermal residual stress of 2D-C/SiC composites is large, and the release of thermal residual stress during tensile damage is responsible for the negative Poisson's ratio. The model prediction results of stress-strain curve and Poisson's ratio evolution curve are in good agreement with the tested curves, which indicates the accuracy and reasonability of the theoretical analysis model. © 2023 Beijing University of Aeronautics and Astronautics (BUAA). All rights reserved.
引用
收藏
页码:3683 / 3694
页数:11
相关论文
共 25 条
  • [1] ZHANG Litong, CHENG Laifei, XU Yongdong, Progress in research work of new CMC-SiC[J], Aeronautical Manufacturing Technology, 1, pp. 24-32, (2003)
  • [2] HE Bolin, SUN Jia, Progress and application of carbon fibers reinforced silicon carbide ceramic matrix composites[J], Bulletin of The Chinese Ceramic Society, 28, 6, pp. 1197-1202, (2009)
  • [3] WILKINS P H, LYNCH S P, THOLE K A, Et al., Effect of a ceramic matrix composite surface on film cooling[J], Journal of Turbomachinery, 144, 8, (2022)
  • [4] CAI Xingrui, WAN Yifei, LI Hanchao, Et al., Digital modeling of the natural microstructures and evaluation of the overall anisotropic moduli of ceramic matrix composites toughened by continuous SiC fiber bundles, Materials Reports, 37, 13, pp. 1-12, (2023)
  • [5] LI Jun, JIAO Guiqiong, WANG Bo, Et al., A non-linear damage constitutive model for 2D woven C/SiC composite material and its application[J], Acta Materiae Compositae Sinica, 30, 1, pp. 165-171, (2013)
  • [6] BASTE S., Inelastic behaviour of ceramic-matrix composites[J], Composites Science and Technology, 61, 15, pp. 2285-2297, (2001)
  • [7] YANG Chengpeng, JIAO Guiqiong, Effects of interface on tensile properties of fiber reinforced ceramic matrix composites, Acta Materiae Compositae Sinica, 27, 3, pp. 116-121, (2010)
  • [8] NARDONE V C, PREWO K M., Tensile performance of carbon-fibre-reinforced glass, Journal of Materials Science, 23, 1, pp. 168-180, (1988)
  • [9] SORENSEN B F, TALREJA R, SORENSEN O T., Micro-mechanical analysis of damage mechanisms in ceramic matrix composites during mechanical and thermal cycling[J], Composites, 24, 2, pp. 129-140, (1993)
  • [10] MEI Hui, CHENG Laifei, ZHANG Litong, Et al., Damage evolution and microstructural characterization of a cross-woven C/SiC composite under tensile loading, Journal of The Chinese Ceramic Society, 35, 2, pp. 137-143, (2007)