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    Autonomous Uncertainty Quantification for Discontinuous Models Using Multivariate Padé Approximations

    Source: Journal of Turbomachinery:;2018:;volume 140:;issue 004::page 41004
    Author:
    Ahlfeld, Richard
    ,
    Montomoli, Francesco
    ,
    Carnevale, Mauro
    ,
    Salvadori, Simone
    DOI: 10.1115/1.4038826
    Publisher: 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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      Autonomous Uncertainty Quantification for Discontinuous Models Using Multivariate Padé Approximations

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    contributor authorAhlfeld, Richard
    contributor authorMontomoli, Francesco
    contributor authorCarnevale, Mauro
    contributor authorSalvadori, Simone
    date accessioned2019-02-28T11:09:23Z
    date available2019-02-28T11:09:23Z
    date copyright1/23/2018 12:00:00 AM
    date issued2018
    identifier issn0889-504X
    identifier otherturbo_140_04_041004.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4253268
    description abstractProblems 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.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAutonomous Uncertainty Quantification for Discontinuous Models Using Multivariate Padé Approximations
    typeJournal Paper
    journal volume140
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4038826
    journal fristpage41004
    journal lastpage041004-10
    treeJournal of Turbomachinery:;2018:;volume 140:;issue 004
    contenttypeFulltext
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