Surrogate-based optimization of stiffened shells including load-carrying capacity and imperfection sensitivity

被引:45
作者
Hao, Peng [1 ]
Wang, Bo [1 ]
Li, Gang [1 ]
Tian, Kuo [1 ]
Du, Kaifan [1 ]
Wang, Xiaojun [2 ]
Tang, Xiaohan [2 ]
机构
[1] Dalian Univ Technol, Dept Engn Mech, State Key Lab Struct Anal Ind Equipment, Dalian 116023, Peoples R China
[2] Beijing Inst Astronaut Syst Engn, Beijing 100076, Peoples R China
基金
中国国家自然科学基金;
关键词
Stiffened shell; Load-carrying capacity; Imperfection sensitivity; Hyperbolic generatrix shape; Surrogate-based optimization; COMPOSITE CYLINDRICAL-SHELLS; DESIGN OPTIMIZATION; AXIAL-COMPRESSION; OPTIMUM DESIGN; PANELS; SIMULATION; CHALLENGES; CYLINDERS; MODELS;
D O I
10.1016/j.tws.2013.06.004
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
Stiffened shells are very sensitive to initial imperfections, especially for geometrical imperfections. In this study, based on a 3-m-diameter orthogrid stiffened shell, post-buckling and imperfection sensitivity analyses are performed by use of explicit dynamic method. Result indicates that stiffened shell with outward hyperbolic generatrix shape shows a lower imperfection sensitivity as compared to the cylindrical one. Then, a framework of surrogate-based optimization including load-carrying capacity and imperfection sensitivity for stiffened shells is introduced, and the illustrative example demonstrates that the proposed framework has the potential to provide robust optimum design for realistic stiffened shells. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码:164 / 174
页数:11
相关论文
共 41 条
[1]  
[Anonymous], 1968, NASA
[2]  
[Anonymous], 1999, EUR 3 DES STEEL STRU
[3]   Future directions and challenges in shell stability analysis [J].
Arbocz, J ;
Starnes, JH .
THIN-WALLED STRUCTURES, 2002, 40 (09) :729-754
[4]  
Arbocz J, 2005, 46 AIAA ASME ASCE AH
[5]   Reliability-based knockdown factors for composite cylindrical shells under axial compression [J].
Biagi, M. ;
Del Medico, F. .
THIN-WALLED STRUCTURES, 2008, 46 (12) :1351-1358
[6]  
Biagi M., 2008, 49 AIAA ASME ASCE AH
[7]   Approximate method for the optimum design of ring and stringer stiffened cylindrical panels and shells with local, inter-ring, and general buckling modal imperfections [J].
Bushnell, D ;
Bushnell, WD .
COMPUTERS & STRUCTURES, 1996, 59 (03) :489-527
[8]   MINIMUM-WEIGHT DESIGN OF A STIFFENED PANEL VIA PANDA2 AND EVALUATION OF THE OPTIMIZED PANEL VIA STAGS [J].
BUSHNELL, D ;
BUSHNELL, WD .
COMPUTERS & STRUCTURES, 1994, 50 (04) :569-602
[9]  
Bushnell D., 2006, 47 AIAA ASME ASCE AH
[10]   Analysis and optimum design of composite grid structures [J].
Chen, HJ ;
Tsai, SW .
JOURNAL OF COMPOSITE MATERIALS, 1996, 30 (04) :503-534