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首页> 外文期刊>Journal of computational science >Aerodynamic shape optimization by variable-fidelity computational fluid dynamics models: A review of recent progress
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Aerodynamic shape optimization by variable-fidelity computational fluid dynamics models: A review of recent progress

机译:可变保真度计算流体动力学模型对空气动力学形状的优化:近期进展综述

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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.
机译:简要回顾了一些最近的可变保真空气动力学形状优化方法。我们讨论了三种技术,这些技术通过利用嵌入在低保真度计算流体动力学(CFD)模型中的信息能够以较低的计算成本产生令人满意的设计,通常对应于对原始的,高保真度的CEO模型的一些评估。优化。这里考虑的特定技术包括多级设计优化,空间映射和形状保留响应预测。它们都使用相同的预测校正方案,但是它们在构造替代模型时使用的低保真模型信息的方式不同。使用跨音速翼型设计的三种特定情况(包括升力最大化和阻力最小化)说明了提出的技术。 (C)2015 Elsevier B.V.保留所有权利。

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