Bending Behavior and Failure Mode of 3D Needle-Punched C/C-SiC Composites: Multi-scale Analysis and Experimental Investigation

被引:0
作者
Tang, Kejun [1 ]
Zhang, Peng [1 ]
Tong, Yonggang [1 ]
Liang, Xiubing [2 ]
Zhang, Mingjun [1 ]
Li, Yang [3 ]
Lan, Hao [4 ]
Hu, Yongle [1 ]
Xing, Yue [2 ]
机构
[1] Changsha Univ Sci & Technol, Coll Mech & Vehicle Engn, Changsha 410114, Peoples R China
[2] Acad Mil Sci PLA China, Natl Inst Def Technol Innovat, Beijing, Peoples R China
[3] Cent South Univ, State Key Lab Powder Met, Changsha 410083, Peoples R China
[4] Chinese Acad Sci, Key Lab Rare Earths, Beijing, Peoples R China
基金
中国国家自然科学基金;
关键词
bending behavior; finite element method (FEM); progressive damage analysis; three-dimensional needle-punched C/C-SiC composites; C/SIC COMPOSITE; DAMAGE; MICROSTRUCTURE; FATIGUE;
D O I
10.1007/s11665-025-10962-8
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The failure mode of three-dimensional (3D) needle-punched C/C-SiC composites (NP-C/C-SiCs) is complex because they are heterogeneous and demonstrate multi-scale characteristics. It is generally difficult for macroscopic experiments to fully capture the fracture mechanism of the material at a small scale. This paper presents a multi-scale methodology to examine the flexural behavior of NP ceramic-matrix composites (CMCs) considering their real microstructure. The mechanical parameters of the NP-CMCs across different scales are evaluated based on the finite element method (FEM) combined with the progressive damage analysis. Bending properties of the composite material are acquired at the macro-scale, and the damage evolution law at the meso-scale is revealed through transferring the stress history back into the low-scale model. Finally, the flexural test is performed to verify the presented method. The result indicates that the stress-deflection curve and the fracture mode obtained through the FEM simulation agree well with the experimental outcome. The dominant failure mode of 3D NP-C/C-SiCs undergoing the bending load contains matrix cracking, interface debonding, fiber/fiber bundle pull-out, and fiber fracture. The fracture of 0 degrees fiber bundles is the main reason that causes the material to lose its load-carrying capacity.
引用
收藏
页数:17
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