个人信息Personal Information
副教授
博士生导师
硕士生导师
性别:男
毕业院校:北京航空航天大学
学位:博士
所在单位:力学与航空航天学院
学科:飞行器设计. 航空航天力学与工程. 工程力学
办公地点:综合实验1号楼409B
联系方式:+86 411 84706213
电子邮箱:yangl@dlut.edu.cn
考虑纤维随机分布的复合材料热残余应力分析及其对横向力学性能的影响
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发表时间:2016-01-01
发表刊物:复合材料学报
所属单位:运载工程与力学学部
期号:3
页面范围:525-534
ISSN号:1000-3851
摘要:A micromechanical numerical model was established for composites, including the interface and taking into account random fiber distribution, to simulate the thermal residual stress of glass fiber/epoxy composites during the curing process. By comparison with the calculation results of model with periodic fiber distribution, it is found that the fiber array form has great influence on the thermal residual stress of composites, with the maximum thermal residual stress of random fiber distribution much greater than that of periodic fiber distribution. The damage and failure process of composites subjected to transverse tension and compression load including thermal residual stress were also investigated. The results indicate that the existence of thermal residual stress significantly affects the damage initiation location and progressing path of composites, weakening the transverse tensile and compressive strength of the composites. Under transverse tension load, after including thermal residual stress, the strength of the composite decreases somewhat, and the fracture strain decreases greatly; under transverse compression load, after including thermal residual stress, the strength of the composite decreases slightly, but the failure strain almost remains unchanged. Due to the effect of thermal residual stress, the transverse tensile and compressive strength of the composites decrease by 10.5% and 5.2%, respectively. © 2016, BUAA Culture Media Group Ltd. All right reserved.
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