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 IN-PHASE THERMOMECHANICAL FATIGUE HYSTERESIS LOOPS OF FIBER-REINFORCED CERAMIC-MATRIX COMPOSITES

点击次数: 所属单位:民航学院 发表刊物:CERAMICS-SILIKATY 关键字:Ceramic-matrix composites (CMCs) Thermomechanical fatigue Hysteresis loops Interface shear stress 摘要:In this paper, the in-phase thermomechanical fatigue hysteresis loops of fiber-reinforced ceramic-matrix composites (CMCs) have been investigated. The relationships between the thermal cyclic temperatures, fiber/matrix interface shear stress, fiber/matrix interface debonding/sliding and the stress/strain hysteresis loops have been established. The effects of fiber volume fraction, fatigue peak stress, matrix cracking space, fiber/matrix interface debonded energy and thermal cyclic temperature range on the in phase thermomechanical fatigue hysteresis loops have been analyzed. The in-phase thermomechanical fatigue hysteresis loops of cross-ply SiC/MAS composite have been predicted for different applied cycle number. ISSN号:0862-5468 是否译文: 发表时间:2018-08-01 通讯作者:李龙彪