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 thermomechanical fatigue hysteresis loops of long-fiber-reinforced ceramic-matrix composites under out-of-phase cyclic loading condition

点击次数: 所属单位:民航学院 发表刊物:INTERNATIONAL JOURNAL OF FATIGUE 关键字:Ceramic-matrix composites (CMCs) Airworthiness Thermomechanical fatigue Hysteresis loops Interface shear stress 摘要:In this paper, the thermomechanical fatigue hysteresis loops of long-fiber-reinforced ceramic -matrix composites(CMCs) subjected to out-of-phase (OP) cyclic loading have been investigated using the micromechanical approach. The fiber/matrix interface shear stress is determined as a function of the testing temperature and material properties, which affects the matrix multicracIdng and fiber/matrix interface debonding and sliding upon unloading and reloading. The relationships between the cyclic temperature and stress level, matrix multicracking, interface debonding and sliding, and the shape, location and the area of the thermomechanical fatigue hysteresis loops have been established. The effects of the fiber volume fraction, fatigue peak stress, matrix cracking space, fiber/matrix interface debonded energy and cyclic temperature range on the thermomechanical fatigue hysteresis loops subjected to out-of-phase cyclic loading have been analyzed. The differences of the thermomechanical fatigue hysteresis loops, interface debonding and sliding between the out-of-phase (OP) and in-phase (IF) thermomechanical cyclic loading have been analyzed. The thermomechanical fatigue hysteresis loops of cross ply SiC/MAS composite under out-of-phase tension-tension cyclic loading have been predicted. (C) 2017 Elsevier Ltd. All rights reserved. ISSN号:0142-1123 是否译文: 发表时间:2017-12-01 通讯作者:李龙彪