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 the Monotonic and Cyclic Tensile Stress-Strain Behavior of 2D and 2.5D Woven C/SiC Ceramic-Matrix Composites

点击次数: 所属单位:民航学院 发表刊物:MECHANICS OF COMPOSITE MATERIALS 关键字:woven ceramic-matrix composites tension matrix multicracking interface debonding fiber failure 摘要:The deformation of 2D and 2.5 C/SiC woven ceramic-matrix composites (CMCs) in monotonic and cyclic loadings has been investigated. Statistical matrix multicracking and fiber failure models and the fracture mechanics interface debonding approach are used to determine the spacing of matrix cracks, the debonded length of interface, and the fraction of broken fibers. The effects of fiber volume fraction and fiber Weibull modulus on the damage evolution in the composites and on their tensile stress-strain curves are analyzed. When matrix multicracking and fiber/matrix interface debonding occur, the fiber slippage relative to the matrix in the debonded interface region of the 0A degrees warp yarns is the main reason for the emergance of stress-strain hysteresis loops for 2D and 2.5D woven CMCs. A model of these loops is developed, and histeresis loops for the composites in cyclic loadings/unloadings are predicted. ISSN号:0191-5665 是否译文: 发表时间:2018-05-01 通讯作者:李龙彪