A general global-local modelling framework for the deterministic optimisation of composite structures

被引:19
|
作者
Picchi Scardaoni, Marco [1 ,2 ]
Montemurro, Marco [1 ]
机构
[1] Univ Bordeaux, Arts & Metiers Inst Technol, CNRS, INRA,Bordeaux INP,HESAM Univ,I2M UMR 5295,Esplana, F-33405 Talence, France
[2] Univ Pisa, Dept Civil & Ind Engn, Aerosp Div, Via G Caruso 8, I-56124 Pisa, Italy
基金
欧盟地平线“2020”;
关键词
Composites; Anisotropy; Polar method; Deterministic optimisation; Buckling; Global; local modelling approach; SHEAR DEFORMATION-THEORY; TOPOLOGY OPTIMIZATION; MULTISCALE APPROACH; LAMINATED PLATES; SANDWICH PLATES; OPTIMUM DESIGN; PANELS; CONSTRAINTS; PARAMETERS; STRATEGY;
D O I
10.1007/s00158-020-02586-4
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
This work deals with the multi-scale optimisation of composite structures by adopting a general global-local (GL) modelling strategy to assess the structure responses at different scales. The GL modelling approach is integrated into the multi-scale two-level optimisation strategy (MS2LOS) for composite structures. The resulting design strategy is, thus, called GL-MS2LOS and aims at proposing a very general formulation of the design problem, without introducing simplifying hypotheses on the laminate stack and by considering, as design variables, the full set of geometric and mechanical parameters defining the behaviour of the composite structure at each pertinent scale. By employing a GL modelling approach, most of the limitations of well-established design strategies, based on analytical or semi-empirical models, are overcome. The GL-MS2LOS makes use of the polar formalism to describe the anisotropy of the composite at the macroscopic scale (where it is modelled as an equivalent homogeneous anisotropic plate). In this work, deterministic algorithms are exploited during the solution search phase. The challenge, when dealing with such a design problem, is to develop a suitable formulation and dedicated operators, to link global and local models physical responses and their gradients. Closed-form expressions of structural responses gradients are rigorously derived by taking into account for the coupling effects when passing from global to local models. The effectiveness of the GL-MS2LOS is proven on a meaningful benchmark: the least-weight design of a cantilever wing subject to different design requirements. Constraints include maximum allowable displacements, maximum allowable strains, blending, manufacturability requirements and buckling factor.
引用
收藏
页码:1927 / 1949
页数:23
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