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 of fatigue hysteresis behavior in carbon fiber-reinforced ceramic-matrix composites under multiple loading stress levels

点击次数: 所属单位:民航学院 发表刊物:JOURNAL OF COMPOSITE MATERIALS 关键字:Ceramic-matrix composites fatigue hysteresis loops matrix cracking 摘要:The fatigue hysteresis behavior in fiber-reinforced ceramic- matrix composites under multiple loading stress levels has been investigated. Based on the fatigue damage mechanism of fiber slipping relative to matrix in the interface debonded region upon unloading/reloading, the fatigue hysteresis loops models corresponding to different interface slip cases under multiple loading stress levels have been derived. The fatigue hysteresis loss energy and interface slip corresponding to single/multiple loading stress levels and different loading sequences have been investigated. The fatigue hysteresis loops of unidirectional SiC/CAS-II composite under multiple loading stress levels have been predicted. ISSN号:0021-9983 是否译文: 发表时间:2017-03-01 通讯作者:李龙彪