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:

Mechanical hysteresis and damage evolution in C/SiC composites under fatigue loading at room and elevated temperatures

点击次数: 所属单位:民航学院 发表刊物:INTERNATIONAL JOURNAL OF APPLIED CERAMIC TECHNOLOGY 关键字:ceramic matrix composites (CMCs) fatigue hysteresis loops interface debonding interface shear stress matrix cracking 摘要:In this paper, the mechanical hysteresis and damage evolution in C/SiC ceramic matrix composites (CMCs) under cyclic tension-tension fatigue loading at room and elevated temperatures in air and in inert atmosphere and different loading frequencies are investigated. The fatigue hysteresis loops models considering multiple matrix cracking modes are developed to establish the relationships between fatigue hysteresis loops, fatigue hysteresis dissipated energy, and fiber/matrix interface shear stress. The evolution of fatigue hysteresis dissipated energy and interface shear stress vs applied cycles is analyzed. It was found that the interface shear stress degradation rate increases with fatigue peak stress, and loading frequency from 40 to 375 Hz. ISSN号:1546-542X 是否译文: 发表时间:2019-11-01 合写作者:Reynaud, Pascal,Fantozzi, Gilbert 通讯作者:李龙彪