Thermal buckling load optimization of laminated composite plates

被引：57

作者：

Topal, U. ^{[1
]}

Uzman, Ue. ^{[1
]}

机构：

[1] Karadeniz Tech Univ, Dept Civil Engn, TR-29000 Gumushane, Turkey

来源：

THIN-WALLED STRUCTURES | 2008年 / 46卷 / 06期

关键词：

laminated composite plates; thermal buckling; Modified Feasible Direction method; optimal designs;

D O I：

10.1016/j.tws.2007.11.005

中图分类号：

TU [建筑科学];

学科分类号：

0813 ;

摘要：

In this study, the applicability of the Modified Feasible Direction (MFD) method on the thermal buckling optimization of laminated plates subjected to uniformly distributed temperature load is investigated. The objective function is to maximize the critical temperature capacity of laminated plates and the fiber orientation is considered as design variable. The first-order shear deformation theory is used in the mathematical formulation. For this purpose, a program based on FORTRAN is used for the optimization of laminated plates. Finally, the effect of aspect ratio, antisymmetric lay-up, boundary condition, material anisotropy, ratio of coefficients of thermal expansion, and hybrid laminates on the results is investigated and the results are compared. (C) 2007 Elsevier Ltd. All rights reserved.

引用

页码：667 / 675

页数：9

共 16 条

[1] OPTIMAL-DESIGN OF ANTISYMMETRIC HYBRID LAMINATES AGAINST THERMAL BUCKLING [J].

ADALI, S ;

DUFFY, KJ .

JOURNAL OF THERMAL STRESSES, 1990, 13 (01) :57-71

[2] Optimization of coupled thermal-structural problems of laminated plates with lamination parameters [J].

Autio, M .

STRUCTURAL AND MULTIDISCIPLINARY OPTIMIZATION, 2001, 21 (01) :40-51

[3]

Chen BS, 2003, J THERM STRESSES, V26, P479, DOI [10.1080/713855939, 10.1080/01495730390192287]

[4]

DEFARIA AR, 2004, INV PROBL DES OPT S

[5] Multiobjective design and control optimization for minimum thermal postbuckling dynamic response and maximum buckling temperature of composite laminates [J].

Fares, ME ;

Youssif, YG ;

Hafiz, MA .

STRUCTURAL AND MULTIDISCIPLINARY OPTIMIZATION, 2005, 30 (02) :89-100

[6] Structural and control optimization for maximum thermal buckling and minimum dynamic response of composite laminated plates [J].

Fares, ME ;

Youssif, YG ;

Hafiz, MA .

INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2004, 41 (3-4) :1005-1019

[7] THERMAL BUCKLING OF CLAMPED SYMMETRICAL LAMINATED PLATES [J].

HUANG, NN ;

TAUCHERT, TR .

THIN-WALLED STRUCTURES, 1992, 13 (04) :259-273

[8] Thermal buckling response of shear flexible laminated anisotropic plates using a three-node isoparametric element [J].

Kabir, HRH ;

Askar, H ;

Chaudhuri, RA .

COMPOSITE STRUCTURES, 2003, 59 (02) :173-187

[9] Optimal design of thick laminated composite plates for maximum thermal buckling load [J].

Lee, YS ;

Lee, YW ;

Yang, MS ;

Park, BS .

JOURNAL OF THERMAL STRESSES, 1999, 22 (03) :259-273

[10]

MOHAN RAR, 2005, COMPOS STRUCT, V70, P383

← 1 2 →