Optimization of Laminates for Maximum Buckling Load

被引：0

作者：

Abdelillah Feghoul

Abdelkader Lousdad

Abdelkader Megueni

Azzeddine Belaziz

机构：

[1] University of Sidi Bel Abbes,Laboratory of Mechanics of Structures and Solids (LMSS), Mechanical Engineering Department, Faculty of Technology

[2] University of Sidi Bel Abbes,Laboratory of Materials and Reactive Systems (LMSR), Mechanical Engineering Department, Faculty of Technology

来源：

Journal of Failure Analysis and Prevention | 2019年 / 19卷

关键词：

Optimization; Laminate; Fiber orientation buckling; Loading; Genetic algorithm (GA);

D O I：

暂无

中图分类号：

学科分类号：

摘要：

Objective of this work is to optimize the structural configuration of laminates in terms of design for the maximization of buckling resistance of laminates under the effect of constraints. The predominant design parameter is the orientation of the fibers in the layers of the laminate. High-order deformation theory is used in the mathematical formulation in the buckling analysis of stratified composite plates. For this purpose, we will use the optimization technique genetic algorithm taking into account the various factors: number of fibers, geometric ratio, load ratio and boundary conditions.

引用

页码：177 / 181

页数：4

共 50 条

[1] Optimization of Laminates for Maximum Buckling Load
Feghoul, Abdelillah
Lousdad, Abdelkader
Megueni, Abdelkader
Belaziz, Azzeddine
JOURNAL OF FAILURE ANALYSIS AND PREVENTION, 2019, 19 (01) : 177 - 181
[2] Stacking sequence optimization of composite laminates for maximum buckling load using permutation search algorithm
Jing, Zhao
Fan, Xueling
Sun, Qin
COMPOSITE STRUCTURES, 2015, 121 : 225 - 236
[3] Optimization of symmetric laminates for maximum buckling load including the effects of bending-twisting coupling
Walker, M
Adali, S
Verijenko, V
COMPUTERS & STRUCTURES, 1996, 58 (02) : 313 - 319
[4] Optimisation of symmetric laminates with internal line supports for maximum buckling load
Walker, M
STRUCTURAL ENGINEERING AND MECHANICS, 1998, 6 (06) : 633 - 641
[5] Optimal design of symmetric laminates with cut-outs for maximum buckling load
Walker, M
COMPUTERS & STRUCTURES, 1999, 70 (03) : 337 - 343
[6] Optimization formulations for the maximum nonlinear buckling load of composite structures
Lindgaard, Esben
Lund, Erik
STRUCTURAL AND MULTIDISCIPLINARY OPTIMIZATION, 2011, 43 (05) : 631 - 646
[7] Optimization formulations for the maximum nonlinear buckling load of composite structures
Esben Lindgaard
Erik Lund
Structural and Multidisciplinary Optimization, 2011, 43 : 631 - 646
[8] Optimum design of composite laminates for maximum buckling load capacity using simulated annealing
Erdal, O
Sonmez, FO
COMPOSITE STRUCTURES, 2005, 71 (01) : 45 - 52
[9] Optimization control of composite laminates for maximum thermal buckling and minimum vibrational response
Fares, ME
Youssif, YG
Hafiz, MA
JOURNAL OF THERMAL STRESSES, 2002, 25 (11) : 1047 - 1064
[10] Optimum stacking sequence design of composite laminates for maximum buckling load capacity using parameter-less optimization algorithms
A. Kaveh
A. Dadras
N. Geran Malek
Engineering with Computers, 2019, 35 : 813 - 832

← 1 2 3 4 5 →