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Accelerated construction of projection-based reduced-order models via incremental approaches

Eki Agouzal, Tommaso Taddei

Abstract

We present an accelerated greedy strategy for training of projection-based reduced-order models for parametric steady and unsteady partial differential equations. Our approach exploits hierarchical approximate proper orthogonal decomposition to speed up the construction of the empirical test space for least-square Petrov-Galerkin formulations, a progressive construction of the empirical quadrature rule based on a warm start of the non-negative least-square algorithm, and a two-fidelity sampling strategy to reduce the number of expensive greedy iterations. We illustrate the performance of our method for two test cases: a two-dimensional compressible inviscid flow past a LS89 blade at moderate Mach number, and a three-dimensional nonlinear mechanics problem to predict the long-time structural response of the standard section of a nuclear containment building under external loading.

Accelerated construction of projection-based reduced-order models via incremental approaches

Abstract

We present an accelerated greedy strategy for training of projection-based reduced-order models for parametric steady and unsteady partial differential equations. Our approach exploits hierarchical approximate proper orthogonal decomposition to speed up the construction of the empirical test space for least-square Petrov-Galerkin formulations, a progressive construction of the empirical quadrature rule based on a warm start of the non-negative least-square algorithm, and a two-fidelity sampling strategy to reduce the number of expensive greedy iterations. We illustrate the performance of our method for two test cases: a two-dimensional compressible inviscid flow past a LS89 blade at moderate Mach number, and a three-dimensional nonlinear mechanics problem to predict the long-time structural response of the standard section of a nuclear containment building under external loading.
Paper Structure (26 sections, 40 equations, 11 figures, 3 tables, 7 algorithms)

This paper contains 26 sections, 40 equations, 11 figures, 3 tables, 7 algorithms.

Figures (11)

  • Figure 1: inviscid flow past an array of LS89 turbine blades. (a) partition associated with the geometric map. (b)-(c) behavior of the Mach number for two parameter values.
  • Figure 2: compressible flow past a LS89 blade. (a)-(b)-(c) three computational meshes. (d) behavior of the average and maximum error \ref{['eq:grid_error']}.
  • Figure 3: compressible flow past a LS89 blade. Progressive construction of quadrature rule and test space, coarse mesh ($N_{\rm e} = 1827$).
  • Figure 4: compressible flow past a LS89 blade. Progressive construction of quadrature rule and test space; fine mesh ($N_{\rm e} = 16353$).
  • Figure 5: compressible flow past a LS89 blade; sampling. (a) behavior of $E_{n}^{{\rm proj},(i)}$\ref{['eq:proj_error_sampling']} for six different choices of the coarse mesh, and for random samples. (b)-(c) parameters $\{ \mu^{\star,j} \}_j$ selected by Algorithm \ref{['alg:multifidelity_greedy']} for two different coarse meshes.
  • ...and 6 more figures