Shape optimization for fluid flow with parametric level set method and deep neural networks

IF 2.5 3区 工程技术 Q3 COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS
Wrik Mallik , Rajeev K. Jaiman , Jasmin Jelovica
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引用次数: 0

Abstract

This study presents a novel application of the parametric level-set (PLS) method to develop a shape optimization process by directly modifying flow dynamics. The present method employs linear superimposition of polynomial perturbations to traditional PLS as shape optimization parameters. This enables smooth shape changes without any change in topology and limits the design variables to only the number of polynomials required for arbitrary hydrofoil morphing. During optimization, deep convolutional neural networks are integrated with the point clouds of the uniform level set to provide a surrogate model for flow dynamics. The present shape optimization method is employed here to delay stall via mitigation of flow separation on the suction surface of the NACA66 hydrofoil at high angles of attack. Shape optimization mitigates the forward movement of trailing edge flow reversal via changes in hydrofoil thickness and camber forward of the maximum hydrofoil thickness point. The optimized design shows more than two order reductions in mean flow reversal compared to NACA66 under the design condition angle of attack of 11.5. At 14°, NACA66 shows complete flow separation while the optimized design exhibits almost three orders lower mean reversal magnitude of top surface flow than that of NACA66, indicating significantly delayed flow separation characteristics. The surrogate-based optimization is performed at four orders of magnitude lower computation time than full-order flow solvers. The results demonstrate the potential of the proposed PLS and deep neural network methodology to perform fast data-driven (non-intrusive) shape optimization of fluid flow.
基于参数水平集和深度神经网络的流体流动形状优化
本研究提出了一种新的应用参数水平集(PLS)方法,通过直接修改流动动力学来开发形状优化过程。该方法采用多项式扰动对传统PLS的线性叠加作为形状优化参数。这使得平滑的形状变化没有任何变化的拓扑结构和限制设计变量,只有多项式的数量需要任意水翼变形。在优化过程中,将深度卷积神经网络与均匀水平集的点云相结合,为流动动力学提供代理模型。本文采用该形状优化方法,通过减小NACA66型水翼大迎角吸力面流动分离来延迟失速。形状优化通过改变水翼厚度和最大水翼厚度点前方的弧度来减轻尾缘流动反转的前向运动。优化后的设计显示,在11.5°攻角的设计条件下,与NACA66相比,平均气流反转减少了两个以上的数量级。在14°时,NACA66表现出完全的流动分离,而优化设计的顶面流动平均反转幅度比NACA66低近3个数量级,显示出明显的延迟流动分离特性。基于代理的优化比全阶流求解器的计算时间低4个数量级。结果表明,所提出的PLS和深度神经网络方法在执行快速数据驱动(非侵入式)流体流动形状优化方面具有潜力。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Computers & Fluids
Computers & Fluids 物理-计算机:跨学科应用
CiteScore
5.30
自引率
7.10%
发文量
242
审稿时长
10.8 months
期刊介绍: Computers & Fluids is multidisciplinary. The term ''fluid'' is interpreted in the broadest sense. Hydro- and aerodynamics, high-speed and physical gas dynamics, turbulence and flow stability, multiphase flow, rheology, tribology and fluid-structure interaction are all of interest, provided that computer technique plays a significant role in the associated studies or design methodology.
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