Autonomous Uncertainty Quantification for Discontinuous Models Using Multivariate Padé ApproximationsSource: Journal of Turbomachinery:;2018:;volume 140:;issue 004::page 41004DOI: 10.1115/1.4038826Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Problems in turbomachinery computational fluid dynamics (CFD) are often characterized by nonlinear and discontinuous responses. Ensuring the reliability of uncertainty quantification (UQ) codes in such conditions, in an autonomous way, is challenging. In this work, we suggest a new approach that combines three state-of-the-art methods: multivariate Padé approximations, optimal quadrature subsampling (OQS), and statistical learning. Its main component is the generalized least-squares multivariate Padé–Legendre (PL) approximation. PL approximations are globally fitted rational functions that can accurately describe discontinuous nonlinear behavior. They need fewer model evaluations than local or adaptive methods and do not cause the Gibbs phenomenon like continuous polynomial chaos methods. A series of modifications of the Padé algorithm allows us to apply it to arbitrary input points instead of optimal quadrature locations. This property is particularly useful for industrial applications, where a database of CFD runs is already available, but not in optimal parameter locations. One drawback of the PL approximation is that it is nontrivial to ensure reliability. To improve stability, we suggest to couple it with OQS. Our reasoning is that least-squares errors, caused by an ill-conditioned design matrix, are the main source of error. Finally, we use statistical learning methods to check smoothness and convergence. The resulting method is shown to efficiently and correctly fit thousands of partly discontinuous response surfaces for an industrial film cooling and shock interaction problem using only nine CFD simulations.
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contributor author | Ahlfeld, Richard | |
contributor author | Montomoli, Francesco | |
contributor author | Carnevale, Mauro | |
contributor author | Salvadori, Simone | |
date accessioned | 2019-02-28T11:09:23Z | |
date available | 2019-02-28T11:09:23Z | |
date copyright | 1/23/2018 12:00:00 AM | |
date issued | 2018 | |
identifier issn | 0889-504X | |
identifier other | turbo_140_04_041004.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4253268 | |
description abstract | Problems in turbomachinery computational fluid dynamics (CFD) are often characterized by nonlinear and discontinuous responses. Ensuring the reliability of uncertainty quantification (UQ) codes in such conditions, in an autonomous way, is challenging. In this work, we suggest a new approach that combines three state-of-the-art methods: multivariate Padé approximations, optimal quadrature subsampling (OQS), and statistical learning. Its main component is the generalized least-squares multivariate Padé–Legendre (PL) approximation. PL approximations are globally fitted rational functions that can accurately describe discontinuous nonlinear behavior. They need fewer model evaluations than local or adaptive methods and do not cause the Gibbs phenomenon like continuous polynomial chaos methods. A series of modifications of the Padé algorithm allows us to apply it to arbitrary input points instead of optimal quadrature locations. This property is particularly useful for industrial applications, where a database of CFD runs is already available, but not in optimal parameter locations. One drawback of the PL approximation is that it is nontrivial to ensure reliability. To improve stability, we suggest to couple it with OQS. Our reasoning is that least-squares errors, caused by an ill-conditioned design matrix, are the main source of error. Finally, we use statistical learning methods to check smoothness and convergence. The resulting method is shown to efficiently and correctly fit thousands of partly discontinuous response surfaces for an industrial film cooling and shock interaction problem using only nine CFD simulations. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Autonomous Uncertainty Quantification for Discontinuous Models Using Multivariate Padé Approximations | |
type | Journal Paper | |
journal volume | 140 | |
journal issue | 4 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.4038826 | |
journal fristpage | 41004 | |
journal lastpage | 041004-10 | |
tree | Journal of Turbomachinery:;2018:;volume 140:;issue 004 | |
contenttype | Fulltext |