The DGDD method for reduced-order modeling of conservation laws
Creators
- 1. INRIA Bordeaux Sud-Ouest, Team MEMPHIS, 33400 Talence (France)
- 2. IMB, UMR 5251, Univ. Bordeaux, 33400 Talence (France)
- 3. Institute for Computational and Mathematical Engineering, Stanford University, Stanford, CA 94305 (United States)
- 4. Department of Mechanical Engineering, Stanford University, Stanford, CA 94305 (United States)
- 5. Department of Aeronautics and Astronautics, Stanford University, Stanford, CA 94305 (United States)
Description
Highlights: • A new domain decomposition method for reduced-order models is proposed. • ROMs approximate the flow in low-fidelity regions, while the HDM is used elsewhere. • The discontinuous Galerkin method offers a simple way to couple the HDM and ROMs. • The integrals of the DG formulation are efficiently evaluated by the ECSW method. • Unsteady flows in presence of shocks are accurately predicted by the proposed method. The discontinuous Galerkin domain decomposition (DGDD) method couples subdomains of high-fidelity polynomial approximation to regions of low-dimensional resolution for the numerical solution of systems of conservation laws. In the low-fidelity regions, the solution is approximated by empirical modes constructed by Proper Orthogonal Decomposition and a reduced-order model is used to predict the solution. The high-dimensional model instead solves the system of conservation laws only in regions where the solution is not amenable to a low-dimensional representation. The coupling between the high-dimensional and the reduced-order models is then performed in a straightforward manner through numerical fluxes at discrete cell boundaries. We show results from application of the proposed method to parametric problems governed by the quasi-1D and 2D compressible Euler equations. In particular, we investigate the prediction of unsteady flows in a converging-diverging nozzle and over a NACA0012 airfoil in presence of shocks. The results demonstrate the stability and the accuracy of the proposed method and the significant reduction of the computational cost with respect to the high-dimensional model.
Availability note (English)
Available from http://dx.doi.org/10.1016/j.jcp.2021.110336Additional details
Identifiers
- DOI
- 10.1016/j.jcp.2021.110336;
- PII
- S002199912100231X;
Publishing Information
- Journal Title
- Journal of Computational Physics (Print)
- Journal Volume
- 437
- Journal Page Range
- vp.
- ISSN
- 0021-9991
- CODEN
- JCTPAH
INIS
- Country of Publication
- Netherlands
- Country of Input or Organization
- International Atomic Energy Agency (IAEA)
- INIS RN
- 54001720
- Subject category
- S71: CLASSICAL AND QUANTUM MECHANICS, GENERAL PHYSICS; S97: MATHEMATICAL METHODS AND COMPUTING;
- Descriptors DEI
- AIRFOILS; COMPUTERIZED SIMULATION; CONSERVATION LAWS; NOZZLES; NUMERICAL SOLUTION; POLYNOMIALS; RESOLUTION; UNSTEADY FLOW
- Descriptors DEC
- FLUID FLOW; FUNCTIONS; MATHEMATICAL SOLUTIONS; SIMULATION
Optional Information
- Copyright
- Copyright (c) 2021 Elsevier Inc. All rights reserved.