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:

Effect of Matrix Multicracking on the Hysteresis Loops of Carbon-Fiber-Reinforced Cross-Ply 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:ceramic-matrix composites cross-ply composite hysteresis loop matrix multicracking 摘要:The effect of matrix multicracking on the stress-strain hysteresis loops of cross-ply C/SiC ceramic-matrix composites (CMCs) under cyclic loading/unloading was investigated. When matrix multicracking and fiber/matrix interface debonding occur in the 0A degrees plies, fiber slipping relative to the matrix in the debonded region of interface is the mainly reason for occurrence of the loops. The interfacial slip lengths, i.e., the debonded lengths of interface are determined, with consideration of matrix multicracking in the 90A degrees and 0A degrees plies, by using the fracture mechanics approach. The effects of peak stress, fiber volume content, fiber/matrix interfacial shear stress, and number of cycles on the hysteresis loops are analyzed. The stress-strain hysteresis loops of cross-ply C/SiC composites corresponding to different peak stresses and numbers of cycles are predicted. ISSN号:0191-5665 是否译文: 发表时间:2017-01-01 通讯作者:李龙彪