Autonomous Uncertainty Quantification for Discontinuous Models Using Multivariate Padé Approximations

Author:

Ahlfeld Richard1,Montomoli Francesco2,Carnevale Mauro3,Salvadori Simone4

Affiliation:

1. Uncertainty Quantification Lab, Department of Aeronautics Imperial College London, London SW7 2AZ, UK e-mail:

2. Uncertainty Quantification Lab, Department of Aeronautics Imperial College London, London SW7 2AZ, UK

3. Osney Thermo-Fluids Laboratory, Department of Engineering Science, University of Oxford, Oxford OX2 0ES, UK

4. Department of Industrial Engineering, University of Florence, Florence 50121, Italy

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

ASME International

Subject

Mechanical Engineering

Reference30 articles.

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3. Lin, G., and Tartakovsky, A. M., 2007, “An Efficient, High-Order Multi-Element Probabilistic Collocation Method on Sparse Grids for Three-Dimensional Flow in Random Porous Media,” American Geophysical Union, Washington, DC, AGU Fall Meeting Abstracts, Vol. 1, p. 1318.http://abstractsearch.agu.org/meetings/2007/FM/H23B-1318.html

4. Uncertainty Quantification Given Discontinuous Model Response and a Limited Number of Model Response Evaluations;SIAM J. Sci. Comput.,2012

5. Lucor, D., Witteveen, J., Constantine, P., Schiavazzi, D., and Iaccarino, G., 2012, “Comparison of Adaptive Uncertainty Quantification Approaches for Shock Wave-Dominated Flows,” Summer Program Center for Turbulence Research, Stanford, CA, June 24–July 20, pp. 219–228.https://web.stanford.edu/group/ctr/Summer/SP12/03.04_lucor.pdf

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