Advantages of employing a full characterization method over FORM in the reliability analysis of laminated composite plates

被引:41
作者
Lopez, R. H. [1 ]
Miguel, L. F. F. [1 ]
Belo, I. M. [2 ]
Cursi, J. E. Souza [3 ]
机构
[1] Univ Fed Santa Catarina, Dept Civil Engn, BR-88034000 Florianopolis, SC, Brazil
[2] Univ Tecnol Fed Parana, PostGrad Program Mech & Mat Engn, BR-80230901 Curitiba, Parana, Brazil
[3] Inst Natl Sci Appl, F-76801 St Etienne, France
关键词
Reliability analysis; Laminated composite plates; Full characterization; FORM; OPTIMIZATION;
D O I
10.1016/j.compstruct.2013.08.024
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Predictions of the failure of composite structures under uncertainties have become an important topic of research. In engineering practice, one is usually interested in evaluating the probability of failure of the system under analysis. Hence, reliability methods such as the First Order Reliability Method (FORM) have been widely employed. However, some problems may arise in the application of these reliability methods, such as, lack of precision and convergence issues. From full characterization methods, such as the polynomial chaos representation, any probabilistic or statistical information may be derived, even the ones provided by reliability methods. Sometimes, the solution of this problem is claimed to be very complex, leading to high computational cost. However, as presented by the authors in a previous work, the full characterization may be simple to implement, providing much more information about the random variable under analysis. Thus, the main goal of this paper is to show that this full characterization approach may be applied to the reliability assessment of laminated composite plates overcoming some of the drawbacks of the FORM. Several examples are presented in order to highlight the advantages of the proposed approach. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码:635 / 642
页数:8
相关论文
共 24 条
[1]   Benchmark study of numerical methods for reliability-based design optimization [J].
Aoues, Younes ;
Chateauneuf, Alaa .
STRUCTURAL AND MULTIDISCIPLINARY OPTIMIZATION, 2010, 41 (02) :277-294
[2]   RELIABILITY OF LAMINATED PLATES VIA THE 1ST-ORDER 2ND-MOMENT METHOD [J].
CEDERBAUM, G ;
ELISHAKOFF, I ;
LIBRESCU, L .
COMPOSITE STRUCTURES, 1990, 15 (02) :161-167
[3]   Spectral stochastic finite element analysis for laminated composite plates [J].
Chen, Nian-Zhong ;
Soares, C. Guedes .
COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 2008, 197 (51-52) :4830-4839
[4]   Reliability assessment of post-buckling compressive strength of laminated composite plates and stiffened panels under axial compression [J].
Chen, Nian-Zhong ;
Soares, C. Guedes .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2007, 44 (22-23) :7167-7182
[5]   A comparison between Monte Carlo and FORMS in calculating the reliability of a composite structure [J].
Di Sciuva, M ;
Lomario, D .
COMPOSITE STRUCTURES, 2003, 59 (01) :155-162
[6]   Application of FRP laminates for strengthening of a reinforced-concrete T-beam bridge structure [J].
Hag-Elsafi, O ;
Alampalli, S ;
Kunin, J .
COMPOSITE STRUCTURES, 2001, 52 (3-4) :453-466
[7]  
Jones RM., 1999, MECH COMPOS MATER, P11
[8]   RELIABILITY-ANALYSIS OF NONLINEAR LAMINATED COMPOSITE PLATE STRUCTURES [J].
KAM, TY ;
LIN, SC ;
HSIAO, KM .
COMPOSITE STRUCTURES, 1993, 25 (1-4) :503-510
[9]   Reliability formulation for composite laminates subjected to first-ply failure [J].
Kam, TY ;
Chang, ES .
COMPOSITE STRUCTURES, 1997, 38 (1-4) :447-452
[10]   Special issue on optimization of aerospace structures [J].
Kim, H. A. ;
Kennedy, D. ;
Guerdal, Z. .
STRUCTURAL AND MULTIDISCIPLINARY OPTIMIZATION, 2008, 36 (01) :1-2