A lagrange parametrization for the design of variable stiffness laminates

被引:9
|
作者
de Quadros, Hugo Borges [1 ]
Hernandes, Jose Antonio [1 ]
机构
[1] Inst Tecnol Aeronaut, Praca Marechal Eduardo Gomes 50, Sao Jose Dos Campos, SP, Brazil
关键词
Variable stiffness laminate; Lamination parameters; Buckling load maximization; Lagrange design element; MAXIMUM BUCKLING LOAD; COMPOSITE PLATES; LAYERWISE OPTIMIZATION; PARAMETERS; PANELS; INPLANE;
D O I
10.1007/s00158-017-1882-2
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
A Lagrange parameterization of lamination parameters which are used for optimization of variable stiffness laminates is presented. The advantages of the approach are: a) the design variables become independent of the finite element mesh and, b) the smoothness of the solution is inherently guaranteed. Due to independency of design variables of the finite element mesh, the reduction in the number of design variables is drastic, once variable stiffness laminates usually demand a fine mesh. The lamination parameters formulation allows a more precise and concise approach to laminate design, removing difficulties related to fiber direction and stacking sequence, increasing the chances to find a global optimal solution. In this paper, the Lagrange parameterization is used for the maximization of the buckling load of a variable stiffness composite plate.
引用
收藏
页码:129 / 137
页数:9
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