Goal-oriented adaptive sampling for projection-based reduced-order models

IF 2.5 3区 工程技术 Q3 COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS
Donovan Blais, Siva Nadarajah, Calista Biondic
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引用次数: 0

Abstract

Modern aircraft design involves a large number of design parameters from a multitude of disciplines. Obtaining high-fidelity solutions for all combinations of such parameters is computationally unfeasible. Although the solution to a large-scale system of equations is generally an element of a large-dimensional space, the solution may actually lie on a reduced-order subspace induced by parameter variation. In order to capture this subspace, samples of the high-dimensional system called snapshots are used to build a reduced-order model. These models have generated interest as a means to compute high-fidelity solutions at a much lower computational cost. However, little value can be placed in a reduced-order solution without some quantification of its error. The dual-weighted residual can be used to obtain error estimates between the outputs of different models. Using dual-weighted residual error estimates in conjunction with a radial basis function interpolation, this work introduces a novel adaptive sampling method that chooses snapshots iteratively such that a prescribed output error tolerance is estimated to be met on the entirety of a parameter space. The adaptive sampling procedure is demonstrated on a one-dimensional Burgers’ equation and two-dimensional inviscid flows.
基于投影的降阶模型的目标导向自适应采样
现代飞机设计涉及来自众多学科的大量设计参数。对于这些参数的所有组合,获得高保真度的解在计算上是不可实现的。虽然大尺度方程组的解通常是一个大维空间的元素,但其解实际上可能位于由参数变化引起的降阶子空间上。为了捕获该子空间,使用称为快照的高维系统样本来构建降阶模型。这些模型作为一种以更低的计算成本计算高保真度解决方案的方法而引起了人们的兴趣。然而,如果没有对其误差进行量化,那么在降阶解中几乎没有价值。双加权残差可以用来获得不同模型输出之间的误差估计。利用双加权残差估计与径向基函数插值相结合,本工作引入了一种新的自适应采样方法,该方法迭代地选择快照,从而估计在整个参数空间上满足规定的输出容差。在一维Burgers方程和二维无粘流上演示了自适应采样过程。
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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