TY - JOUR
T1 - Compression-shear mechanical behavior and damage evolution of needled SiC/C-SiC composites under high temperature
AU - Xu, Qipeng
AU - Zhou, Ziyang
AU - Fan, Xueling
AU - Xu, Jianzheng
AU - Jin, Xiaochao
N1 - Publisher Copyright:
© 2026 Elsevier Ltd
PY - 2026/5
Y1 - 2026/5
N2 - Needled SiC/C-SiC composites are quasi-three-dimensional ceramic matrix composites and candidate materials for extreme temperatures. This study conducted compression experiments on needled SiC/C-SiC composites from room temperature to 1300℃ with loading angles from 0° to 90°. High-precision and total-factor geometric information of the composites was obtained using SEM and X-CT, providing basis for establishing the finite element model. A SiC/SiC fiber bundle damage constitutive model based on micro-mechanical analysis was coupled into the finite element model via ABAQUS UMAT subroutines to simulate the compression-shear process of needled SiC/C-SiC composites, and the simulation and experiment results were compared and analyzed. The results show the decrease in temperature and the increase in normal stress enhance the shear strength of needled SiC/C-SiC composites. The length of pull-out SiC fiber decreases with increasing temperature, indicating that high temperature weaken the toughness and strength of needled SiC/C-SiC composites. The finite element model effectively describes the damage evolution and stress–strain behavior of needled SiC/C-SiC composites. The short C fiber layers and needled regions damage, SiC matrix damage, and SiC/SiC fiber bundles damage occurred sequentially with an increase in compressive stress. These modelling methods can serve as a foundation for the design and strength assessment of ceramic matrix composites.
AB - Needled SiC/C-SiC composites are quasi-three-dimensional ceramic matrix composites and candidate materials for extreme temperatures. This study conducted compression experiments on needled SiC/C-SiC composites from room temperature to 1300℃ with loading angles from 0° to 90°. High-precision and total-factor geometric information of the composites was obtained using SEM and X-CT, providing basis for establishing the finite element model. A SiC/SiC fiber bundle damage constitutive model based on micro-mechanical analysis was coupled into the finite element model via ABAQUS UMAT subroutines to simulate the compression-shear process of needled SiC/C-SiC composites, and the simulation and experiment results were compared and analyzed. The results show the decrease in temperature and the increase in normal stress enhance the shear strength of needled SiC/C-SiC composites. The length of pull-out SiC fiber decreases with increasing temperature, indicating that high temperature weaken the toughness and strength of needled SiC/C-SiC composites. The finite element model effectively describes the damage evolution and stress–strain behavior of needled SiC/C-SiC composites. The short C fiber layers and needled regions damage, SiC matrix damage, and SiC/SiC fiber bundles damage occurred sequentially with an increase in compressive stress. These modelling methods can serve as a foundation for the design and strength assessment of ceramic matrix composites.
KW - Compression-shear mechanical behavior
KW - Damage evolution
KW - Needled SiC/C-SiC composites
KW - Progressive failure analysis
UR - https://www.scopus.com/pages/publications/105034832902
U2 - 10.1016/j.compstruct.2026.120312
DO - 10.1016/j.compstruct.2026.120312
M3 - 文章
AN - SCOPUS:105034832902
SN - 0263-8223
VL - 387
JO - Composite Structures
JF - Composite Structures
M1 - 120312
ER -