个人信息
李龙彪
学位:工学博士学位

个人信息 Personal information

学历:南京航空航天大学 所在单位:民航学院 电子邮箱:

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: 发表时间:2017-12-01 通讯作者:李龙彪