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个人信息Personal Information
副教授
招生学科专业:
航空宇航科学与技术 -- 【招收硕士研究生】 -- 航空学院
机械 -- 【招收硕士研究生】 -- 航空学院
毕业院校:南京航空航天大学
学历:南京航空航天大学
学位:工学博士学位
所在单位:航空学院
办公地点:南京航空航天大学明故宫校区 A18-306
联系方式:13913812250;shzhu@nuaa.edu.cn
电子邮箱:
Buckling and Postbuckling Experiments of Integrally Stiffened Panel Under Compression–Shear Loads
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发表刊物:Journal of Aircraft
摘要:Experiments have been conducted to investigate the buckling and postbuckling behavior of aluminum alloy 7050-T7651 integrally stiffened panel under a combined compression–shear load. A new combined-load test fixture was designed and used in these experiments. There were a total of six large rectangular stiffened panels in the size of 960 by 850 mm, which were classified in two groups according to the cross section and layout of their stiffeners. Three panels, named J panels, were designed in four parallel J-shaped stiffeners. Another three panels, named X panels, were designed in eight orthogonal blade-shaped stiffeners. Strain rosettes bonded back-to-back on the skin were used to measure the strains of skin at their locations in three directions (0, 45, and 90 deg), whereas the strain gauges installed on the stiffeners were used to measure the strains of stiffeners in a single direction. The integrally stiffened panels were loaded up to a sudden drop of the applied load and an accompa
论文类型:期刊论文
学科门类:工学
一级学科:航空宇航科学与技术
文献类型:J
卷号:52
期号:2
页面范围:680-691
是否译文:否
发表时间:2015-03-01
合写作者:Jiayi Yan,Yuequan Wang,Mingbo Tong