Determination of physical parameters of stiffened plates using genetic algorithm

被引:14
作者
Chakraborty, S [1 ]
Mukhopadhyay, M [1 ]
Sha, OP [1 ]
机构
[1] Indian Inst Technol, Dept Ocean Engn & Naval Architecture, Kharagpur 721302, W Bengal, India
关键词
plates; stiffening; algorithm; parameters; model analysis;
D O I
10.1061/(ASCE)0887-3801(2002)16:3(206)
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
An investigation on stiffened isotropic and composite plates has been conducted to determine the geometric and material parameters for the plate, as well as the stiffener from experimental modal data and finite element predictions using a genetic algorithm (GA). The problem is formulated as a global minimization of the error function defined by the difference in undamped eigenvalues and eigenvectors, as predicted from the finite-element modeling to that obtained experimentally. The parameter estimation problem is solved using a GA implementing selection, crossover, and mutation operators to obtain the global minimum solution. Because stiffeners contribute substantially to the overall rigidity of the plate assembly, their position, physical properties, and orientation create considerable variation of the modal properties, as compared to the bare plate with similar construction, This makes each of the stiffened plate identification problems rather unique. GAs have been the subject of considerable interest in providing a robust search procedure for a global optimum solution for such difficult minimization problems. The method is demonstrated on a few simulated examples on stiffened plates to investigate the uniqueness and convergence of results. The methodology, although slow in execution, is found to be very robust, even in the presence of noise. for isolating interesting zones of the search space. Unlike many traditional optimization techniques, it does not get stuck at a particular local minimum due to its parallelism.
引用
收藏
页码:206 / 221
页数:16
相关论文
共 33 条
[1]   VIBRATIONAL ANALYSES OF STIFFENED AND UNSTIFFENED COMPOSITE PLATES SUBJECTED TO INPLANE LOADS [J].
ATTAF, B ;
HOLLAWAY, L .
COMPOSITES, 1990, 21 (02) :117-126
[2]   OPTIMAL WEIGHTED ORTHOGONALIZATION OF MEASURED MODES [J].
BARUCH, M ;
BARITZHACK, IY .
AIAA JOURNAL, 1978, 16 (04) :346-351
[3]   MASS MATRIX CORRECTION USING AN INCOMPLETE SET OF MEASURED MODES [J].
BERMAN, A .
AIAA JOURNAL, 1979, 17 (10) :1147-1148
[4]   IMPROVEMENT OF A LARGE ANALYTICAL MODEL USING TEST DATA [J].
BERMAN, A ;
NAGY, EJ .
AIAA JOURNAL, 1983, 21 (08) :1168-1173
[5]   Free vibration of eccentrically stiffened laminated plates [J].
Chandrashekhara, K ;
Kolli, M .
JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 1997, 16 (10) :884-902
[6]   VIBRATION OF ECCENTRICALLY STIFFENED LAMINATES [J].
CHAO, CC ;
LEE, JC .
JOURNAL OF COMPOSITE MATERIALS, 1980, 14 (JUL) :233-244
[7]   FINITE-ELEMENT FREE-VIBRATION ANALYSIS OF ECCENTRICALLY STIFFENED COMPOSITE PLATES [J].
CHATTOPADHYAY, B ;
SINHA, PK ;
MUKHOPADHYAY, M .
JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 1992, 11 (09) :1003-1034
[8]   ANALYTICAL MODEL IMPROVEMENT USING MODAL TEST-RESULTS [J].
CHEN, JC ;
GARBA, JA .
AIAA JOURNAL, 1980, 18 (06) :684-690
[9]   SIMULTANEOUS ITERATION ALGORITHM FOR SYMMETRIC EIGENVALUE PROBLEMS [J].
CORR, RB ;
JENNINGS, A .
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN ENGINEERING, 1976, 10 (03) :647-663
[10]  
Cunha J, 1999, INT J NUMER METH ENG, V45, P891, DOI 10.1002/(SICI)1097-0207(19990710)45:7<891::AID-NME610>3.0.CO