作者其他论文
文献详情
Experiment and design methods of composite scarf repair for primary-load bearing structures
文献类型:期刊
作者:Liu, Bin[1]  Xu, Fei[2]  Feng, Wei[3]  Yan, Rui[4]  Xie, Wei[5]  
机构:[1]School of Aeronautics, Northwestern Polytechnical University, Postbox 118, 127# Youyixi Road, Xi'an, Shaanxi Province, China
[2]School of Aeronautics, Northwestern Polytechnical University, Postbox 118, 127# Youyixi Road, Xi'an, Shaanxi Province, China
[3]School of Aeronautics, Northwestern Polytechnical University, Postbox 118, 127# Youyixi Road, Xi'an, Shaanxi Province, China
[4]School of Aeronautics, Northwestern Polytechnical University, Postbox 118, 127# Youyixi Road, Xi'an, Shaanxi Province, China
[5]School of Aeronautics, Northwestern Polytechnical University, Postbox 118, 127# Youyixi Road, Xi'an, Shaanxi Province, China
通讯作者:Xu, F (reprint author), Northwestern Polytech Univ, Sch Aeronaut, Postbox 118,127 Youyixi Rd, Xian, Shaanxi Provinc, Peoples R China.
年:2016
期刊名称:COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING影响因子和分区
卷:88
页码范围:27-38
增刊:正刊
学科:材料科学
收录情况:SCI(E)(WOS:000380081600004)  EI(20162302453954)  
所属部门:航空学院
被引频次:12
人气指数:996
浏览次数:972
关键词:Scarf bonding repair; Scarf joint; CDM; MAM
摘要:
A relative thick plate of composite being repaired by scarf bonding was substituted as the scarf joints and studied under tensile load in this paper. The experimental investigation told us the ultimate capability of load and failure mechanism of composite scarf joints. In order to explain failure mechanism for scarf bonding repair of composite structures distinctly, FEM based on continuum damage mechanics (CDM) was carried out. CDM equations were derived by adding the delamination mode and 3D Ha ...More
0
评论(0 条评论)
登录