Stacking sequence optimization of laminated plates

被引：32

作者：

Kim, CW ^{[1
]}

Hwang, W ^{[1
]}

Park, HC ^{[1
]}

Han, KS ^{[1
]}

机构：

[1] Pohang Univ Sci & Technol, Dept Mech Engn, Pohang 790784, South Korea

来源：

COMPOSITE STRUCTURES | 1997年 / 39卷 / 3-4期

关键词：

D O I：

10.1016/S0263-8223(97)00120-7

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

Optimum fiber orientations of laminated composite plates for the maximum strength are found under multiple inplane loading conditions. Tsai-Wu failure criterion is taken as objective function. Based on the state space method, effective optimal design formulation is developed and solution procedure is described with the emphasis on the method of calculations of the design sensitivities. Numerical results are presented for the several test problems. (C) 1998 Published by Elsevier Science Ltd. All rights reserved.

引用

页码：283 / 288

页数：6

共 14 条

[1] OPTIMIZATION OF LAMINATED CYLINDRICAL PRESSURE-VESSELS UNDER STRENGTH CRITERION [J].

ADALI, S ;

SUMMERS, EB ;

VERIJENKO, VE .

COMPOSITE STRUCTURES, 1993, 25 (1-4) :305-312

[2] OPTIMIZATION OF BUCKLING AND YIELD STRENGTHS OF LAMINATED COMPOSITES [J].

CHAO, CC ;

KOH, SL ;

SUN, CT .

AIAA JOURNAL, 1975, 13 (09) :1131-1132

[3] OPTIMUM DESIGN OF COMPOSITE STRUCTURES FOR SHAPE, LAYER ANGLE AND LAYER THICKNESS DISTRIBUTIONS [J].

FUKUNAGA, H ;

SEKINE, H .

JOURNAL OF COMPOSITE MATERIALS, 1993, 27 (15) :1479-1492

[4] STRENGTH OPTIMIZATION OF LAMINATED COMPOSITES WITH RESPECT TO LAYER THICKNESS AND OR LAYER ORIENTATION ANGLE [J].

FUKUNAGA, H ;

VANDERPLAATS, GN .

COMPUTERS & STRUCTURES, 1991, 40 (06) :1429-1439

[5] OPTIMAL-DESIGN OF A COMPOSITE STRUCTURE [J].

GRAESSER, DL ;

ZABINSKY, ZB ;

TUTTLE, ME ;

KIM, GI .

COMPOSITE STRUCTURES, 1993, 24 (04) :273-281

[6]

Haug E.J., 1979, APPL OPTIMAL DESIGN

[7] OPTIMAL-DESIGN OF LAMINATED COMPOSITE PLATES USING A GLOBAL OPTIMIZATION TECHNIQUE [J].

KAM, TY ;

SNYMAN, JA .

COMPOSITE STRUCTURES, 1991, 19 (04) :351-370

[8]

Kim C. W., 1994, Applied Composite Materials, V1, P81, DOI 10.1007/BF00567214

[9]

KIM CW, 1993, ICCM 9 MADR SPAIN

[10] OPTIMUM DESIGN OF COMPOSITE WING STRUCTURES BY A REFINED OPTIMALITY CRITERION [J].

LIU, IW ;

LIN, CC .

COMPOSITE STRUCTURES, 1991, 17 (01) :51-65

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