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:大连理工大学
学位:博士
所在单位:力学与航空航天学院
学科:工程力学. 固体力学. 计算力学
办公地点:综合实验1号楼508
联系方式:邮件或手机壹伍玖零肆玖伍陆贰捌陆
电子邮箱:zhisun@dlut.edu.cn
Buckling response of advanced grid stiffened carbon-fiber composite cylindrical shells with reinforced cutouts
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论文类型:期刊论文
发表时间:2013-01-01
发表刊物:COMPOSITES PART B-ENGINEERING
收录刊物:SCIE、EI
卷号:44
期号:1
页面范围:26-33
ISSN号:1359-8368
关键字:Carbon fiber; Buckling; Finite Element Analysis (FEA); Reinforcing design
摘要:In this paper, we present the initial buckling and post-buckling responses of axial loaded advanced grid stiffened (AGS) composite cylindrical shells with reinforced rectangular or circular cutouts. The AGS cylindrical shells were reinforced by various local grid configurations near the cutout areas. The effects of different reinforcing grid configurations on critical loads were then examined and compared to those of different skin-reinforcing designs using Finite Element Analysis (FEA) simulations. A high-fidelity non-linear analysis procedure was proposed to predict the non-linear buckling response of the shell structures. The simulation results indicated that the grid reinforcements can reduce or eliminate the risk of local buckling response near the cutout areas and increase the critical load of the shell more effectively than the skin reinforcements. Furthermore, those results showed that an optimum grid reinforcement configuration exists, which significantly improved the initial buckling and post-buckling resistance of the cylindrical shells under axial loading. The above findings can potentially be useful to the analysis and optimum design of AGS composite cylindrical shells with cutouts. (C) 2012 Elsevier Ltd. All rights reserved.