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Domain Decomposition for Data-Driven Reduced Modeling of Large-Scale Systems
被引:4
|作者:
Farcas, Ionut-Gabriel
[1
]
Gundevia, Rayomand P.
[2
]
Munipalli, Ramakanth
[3
]
Willcox, Karen E.
[1
]
机构:
[1] Univ Texas Austin, Oden Inst Computat Engn & Sci, Austin, TX 78712 USA
[2] Jacobs Engn Grp Inc, Edwards AFB, CA 93524 USA
[3] Air Force Res Lab, Combust Devices, Beavercreek, OH USA
关键词:
Uncertainty Quantification;
Rotating Detonation Rocket Engine;
Computing Resources;
Supercomputers;
Multidisciplinary Design Optimization;
Combustion;
Domain Decomposition Methods;
Model Order Reduction;
Data-Driven Model;
Multiphysics Simulation;
OPERATOR INFERENCE;
REDUCTION;
APPROXIMATION;
FLOWS;
D O I:
10.2514/1.J063715
中图分类号:
V [航空、航天];
学科分类号:
08 ;
0825 ;
摘要:
This paper focuses on the construction of accurate and predictive data-driven reduced models of large-scale numerical simulations with complex dynamics and sparse training datasets. In these settings, standard, single-domain approaches may be too inaccurate or may overfit and hence generalize poorly. Moreover, processing large-scale datasets typically requires significant memory and computing resources, which can render single-domain approaches computationally prohibitive. To address these challenges, we introduce a domain-decomposition formulation into the construction of a data-driven reduced model. In doing so, the basis functions used in the reduced model approximation become localized in space, which can increase the accuracy of the domain-decomposed approximation of the complex dynamics. The decomposition furthermore reduces the memory and computing requirements to process the underlying large-scale training dataset. We demonstrate the effectiveness and scalability of our approach in a large-scale three-dimensional unsteady rotating-detonation rocket engine simulation scenario with more than 75 million degrees of freedom and a sparse training dataset. Our results show that compared to the single-domain approach, the domain-decomposed version reduces both the training and prediction errors for pressure by up to 13% and up to 5% for other key quantities, such as temperature, and fuel, and oxidizer mass fractions. Lastly, our approach decreases the memory requirements for processing by almost a factor of four, which in turn reduces the computing requirements as well.
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页码:4071 / 4086
页数:16
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