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:

In-phase thermomechanical fatigue damage evolution of long fiber-reinforced ceramic-matrix composites using fatigue hysteresis-based damage parameters

点击次数: 所属单位:民航学院 发表刊物:INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES 关键字:Ceramic-matrix composites (CMCs) Thermomechanical fatigue Damage evolution 摘要:Under in-phase (IP) thermomechanical fatigue (TMF) loading, the thermal cyclic temperature changes with decreasing or increasing applied stress upon unloading or loading, and the fiber/matrix interface shear stress in the long fiber-reinforced ceramic-matrix composites (CMCs) changes with applied cycles. In this paper, the in-phase TMF damage evolution of CMCs has been investigated, considering the coupling effects of TMF loading stress level, thermal cyclic temperature and applied cycles. The interface debonding and sliding lengths are determined based the thermomechanical micromechanical stress field and the fracture mechanics approach. The relationships between the TMF hysteresis parameters, interface damage, thermal cyclic temperature and applied cycles have been developed. The damage accumulation processes subjected to in-phase TMF for different fibers volume fraction, peak stress, matrix crack spacing, interface properties and thermal cyclic temperature range have been analyzed. The distinction of the damage evolution between the in-phase TMF and isothermal fatigue (IF) loading at the same applied stress has been analyzed. The damage evolution of cross-ply CMCs subjected to the in-phase TMF and IF loading have been predicted. (C) 2018 Elsevier Ltd. All rights reserved. ISSN号:0020-7403 是否译文: 发表时间:2018-05-01 通讯作者:李龙彪