Evaluation of tensile properties of a compositemetal joint with a novel metal insert design by experimental and numerical methods
Evaluation of tensile properties of a compositemetal joint with a novel metal insert design by experimental and numerical methods作者机构:School of Aeronautic Science and EngineeringBeihang UniversityBeijing 100083China A VIC China Helicopter Research and Development InstituteJingdezhen 333001China
出 版 物:《Chinese Journal of Aeronautics》 (中国航空学报(英文版))
年 卷 期:2017年第30卷第3期
页 面:1004-1011页
核心收录:
学科分类:08[工学] 0825[工学-航空宇航科学与技术]
基 金:the National Natural Science Foundation of China(No.11472024)for financial support
主 题:Composite structure Failure mode Joints Metal insert Tensile properties
摘 要:Composite-metal joints with a metal insert are one kind of connecting *** this paper,tensile experimental tests were carried out to investigate tensile properties of a compositemetal joint with a novel metal insert *** element models of the joint were established,and strain distribution and tensile strength were *** numerical results are in good agreement with the experimental *** show that the joint failure is dominated by shear properties of the resin *** the resin layer thickness in a certain range will improve the tensile strength of the joint,while increasing the radius of the fillet on the ending side of the metal insert will decrease the joint *** the resin layer plasticity will improve the joint *** effect of the embedded depth of the metal insert can be ignored.