Aerodynamic shape optimization by variable-fidelity computational fluid dynamics models: A review of recent progress

被引:37
|
作者
Leifsson, Leifur [1 ]
Koziel, Slawomir [2 ]
机构
[1] Iowa State Univ, Ames, IA 50011 USA
[2] Gdansk Univ Technol, Fac Elect Telecommun & Informat, PL-80233 Gdansk, Poland
关键词
Surrogate-based optimization; Variable-fidelity modeling; Aerodynamics; Computational fluid dynamics; Airfoil shape design; FRAMEWORK; DESIGN;
D O I
10.1016/j.jocs.2015.01.003
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
A brief review of some recent variable-fidelity aerodynamic shape optimization methods is presented. We discuss three techniques that by exploiting information embedded in low-fidelity computational fluid dynamics (CFD) models are able to yield a satisfactory design at a low computational cost, usually corresponding to a few evaluations of the original, high-fidelity CEO model to be optimized. The specific techniques considered here include multi-level design optimization, space mapping, and shape-preserving response prediction. All of them use the same prediction-correction scheme, however, they differ in the way the low-fidelity model information it utilized to construct the surrogate model. The presented techniques are illustrated using three specific cases of transonic airfoil design involving lift maximization and drag minimization. (C) 2015 Elsevier B.V. All rights reserved.
引用
收藏
页码:45 / 54
页数:10
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