Modeling first matrix cracking stress of fiber-reinforced ceramic-matrix composites considering fiber fracture
点击次数:
所属单位:民航学院
发表刊物:THEORETICAL AND APPLIED FRACTURE MECHANICS
关键字:Ceramic-matrix composites (CMCs) Matrix cracking Interface debonding Fiber failure
摘要:In this paper, the first matrix cracking stress (FMCS) of fiber-reinforced ceramic-matrix composites (CMCs) has been investigated using the energy balance approach considering fiber fracture. The shear lag model combined with fiber failure model and interface debonding criteria has been adopted to analyze the stress distributions in CMCs. The relationships between the FMCS, interface debonding and slipping, and fiber fracture have been established. The effects of fiber volume fraction, interface shear stress, interface debonded energy, fiber Weibull modulus, and fiber strength on the FMCS, interface debonded length and fiber broken fraction have been analyzed. The experimental FMCS of three different CMCs, i.e., SiC/borosilicate, SiC/LAS, and C/borosilicate, with different fiber volume fraction have been predicted. It was found that the fiber/matrix interface possesses strong bonding in SiC/borosilicate and SiC/LAS composites, and weak bonding in C/borosilicate composite. (C) 2017 Elsevier Ltd. All rights reserved.
ISSN号:0167-8442
是否译文:否
发表时间:2017-12-01
通讯作者:李龙彪
上一条:Synergistic effects of temperature, oxidation, loading frequency and stress-rupture on damage evolution of cross-ply ceramic-matrix composites under cyclic fatigue loading at elevated temperatures in oxidizing atmosphere
下一条:Modeling strength degradation of fiber-reinforced ceramic-matrix composites under cyclic loading at room and elevated temperatures