Hybrid Framework for Reliability-Based Design Optimization of Imperfect Stiffened Shells

被引:107
作者
Hao, Peng [1 ]
Wang, Bo [1 ]
Li, Gang [1 ]
Meng, Zeng [1 ]
Wang, Lipeng [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, Dept Struct Design, Beijing 100076, Peoples R China
基金
中国国家自然科学基金; 中国博士后科学基金;
关键词
COMPOSITE CYLINDRICAL-SHELLS; OPTIMUM DESIGN; AXIAL-COMPRESSION; BUCKLING LOAD; METAMODELING TECHNIQUES; KNOCKDOWN FACTORS; SENSITIVITY; PANELS; FUTURE; UNCERTAINTY;
D O I
10.2514/1.J053816
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Variations of manufacturing process parameters, environment aspects, and imperfections may significantly affect the quality and performance of stiffened shells. The reliability-based design optimization (RBDO) of stiffened shells, considering all these uncertainty factors simultaneously, is extremely time-consuming, even if the surrogate-based technology is used. Therefore, a hybrid bi-stage framework for RBDO of stiffened shells is presented to release the computational burden, where two main sources of uncertainties are considered: variations of material properties and geometric dimensions are described as random variables, while various forms of imperfections of stiffened shells are covered by the single perturbation load approach. The basic idea of the proposed method is to combine the efficiency of smeared stiffener method with the accuracy of finite element method, and then narrow the design window efficiently with little accuracy sacrifice. The adaptive chaos control method is used to ensure the robustness of the search process of the most probable target point. The numerical example illustrates the advantage of the proposed method over other RBDO approaches from the point of view of computational cost, accuracy and robustness of the result.
引用
收藏
页码:2878 / 2889
页数:12
相关论文
共 55 条
[1]   Toward a probabilistic preliminary design criterion for buckling critical composite shells [J].
Arbocz, J ;
Hilburger, MW .
AIAA JOURNAL, 2005, 43 (08) :1823-1827
[2]   COLLAPSE OF AXIALLY COMPRESSED CYLINDRICAL-SHELLS WITH RANDOM IMPERFECTIONS [J].
ARBOCZ, J ;
HOL, JMAM .
AIAA JOURNAL, 1991, 29 (12) :2247-2256
[3]   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
[4]   RELIABILITY ASSESSMENT OF AXIALLY COMPRESSED COMPOSITE CYLINDRICAL SHELLS WITH RANDOM IMPERFECTIONS [J].
Broggi, Matteo ;
Calvi, Adriano ;
Schueller, Gerhart I. .
INTERNATIONAL JOURNAL OF STRUCTURAL STABILITY AND DYNAMICS, 2011, 11 (02) :215-236
[5]   OPTIMUM DESIGN OF COMPOSITE STIFFENED PANELS UNDER COMBINED LOADING [J].
BUSHNELL, D ;
BUSHNELL, WD .
COMPUTERS & STRUCTURES, 1995, 55 (05) :819-856
[6]  
Bushnell D., 1985, FINITE ELEM ANAL DES, V1, P165
[7]  
Calladine C. R., 1983, THOERY SHELL STRUCTU, P473
[8]   UNDERSTANDING IMPERFECTION-SENSITIVITY IN THE BUCKLING OF THIN-WALLED SHELLS [J].
CALLADINE, CR .
THIN-WALLED STRUCTURES, 1995, 23 (1-4) :215-235
[9]   Future structural stability design for composite space and airframe structures [J].
Degenhardt, Richard ;
Castro, Saullo G. P. ;
Arbelo, Mariano A. ;
Zimmerman, Rolf ;
Khakimova, Regina ;
Kling, Alexander .
THIN-WALLED STRUCTURES, 2014, 81 :29-38
[10]   Investigations on imperfection sensitivity and deduction of improved knock-down factors for unstiffened CFRP cylindrical shells [J].
Degenhardt, Richard ;
Kling, Alexander ;
Bethge, Arne ;
Orf, Jana ;
Kaerger, Luise ;
Zimmermann, Rolf ;
Rohwer, Klaus ;
Calvi, Adriano .
COMPOSITE STRUCTURES, 2010, 92 (08) :1939-1946