通过大涡流模拟逐形设计减少湍流阻力的贝叶斯优化里布里特表面设计

Sangjoon Lee, Haris Moazam Sheikh, Dahyun Daniel Lim, Grace X Gu, Philip S. Marcus
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引用次数: 0

摘要

本文介绍了一种计算方法,利用逐形设计(DbM)、大涡模拟(LES)和贝叶斯优化(BO)对湍流通道流中的新型波纹管表面设计进行优化,以减少阻力。使用 DbM 生成的设计空间包括各种新型波纹表面设计,然后使用 LES 对其进行评估,以确定其减少阻力的能力。使用混合变量贝叶斯优化(MixMOBO)算法对波纹表面的几何形状和配置进行优化,以最大限度地减少阻力。共进行了 125 次优化,最终确定了 3 种最佳波纹管表面设计,其阻力降低率与 8% 的参考值相当或更好。贝叶斯优化设计通常建议波纹尺寸为 15 个壁面单位左右,与传统设计相比间距相对较大,波纹尖端为尖形,并带有凹槽。我们的整体优化过程是在合理的物理时间范围内进行的,最多可使用 12 核并行计算,可用于在实现之前需要高保真计算设计的流体工程优化问题。
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Bayesian-Optimized Riblet Surface Design for Turbulent Drag Reduction via Design-by-Morphing with Large Eddy Simulation
A computational approach is presented for optimizing new riblet surface designs in turbulent channel flow for drag reduction, utilizing Design-by-Morphing (DbM), Large Eddy Simulation (LES), and Bayesian Optimization (BO). The design space is generated using DbM to include a variety of novel riblet surface designs, which are then evaluated using LES to determine their drag-reducing capabilities. The riblet surface geometry and configuration are optimized for maximum drag reduction using the mixed-variable Bayesian optimization (MixMOBO) algorithm. A total of 125 optimization epochs are carried out, resulting in the identification of 3 optimal riblet surface designs that are comparable to or better than the reference drag reduction rate of 8 %. The Bayesian-optimized designs commonly suggest riblet sizes of around 15 wall units, relatively large spacing compared to conventional designs, and spiky tips with notches for the riblets. Our overall optimization process is conducted within a reasonable physical time frame with up to 12-core parallel computing and can be practical for fluid engineering optimization problems that require high-fidelity of computational design before materialization.
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