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Research Article | Publishing Language: Chinese | Open Access

Prediction modeling of unsteady flow field aimed at high-order DG numerical scheme

MIIT Key Laboratory of Pattern Analysis and Machine Intelligence, College of Computer Science and Technology, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China
State Key Laboratory of Aerodynamics, Mianyang 621000, China
Key Laboratory of Aerodynamics Noise Control, Mianyang 621000, China
Collaborative Innovation Center of Noval Software Technology and Industrialization, Nanjing 210023, China
College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
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Abstract

As a numerical method, the high-order discontinuous Galerkin (DG) method has the characteristics of high precision and is suitable for complex geometries. Meanwhile, due to its good dispersion and dissipation properties, the high-order DG method is well suited for implicit large eddy simulations. However, it usually takes a long time for solving unsteady flow fields, and how to reduce the computation cost is still a challenge. To tackle this issue, a deep neural network consisted with the three-dimensional convolution, the two-dimensional residual network and the attention mechanism has been proposed, which can extract the implied spatio-temporal characteristics of the flow field from the data. The numerical simulation for flow around a cylinder at different Reynolds numbers is carried out to obtain the data set for training, which is then used to predict the flow field for the future period. The results show that the deep neural network has a satisfactory ability of modeling the flow around a cylinder. The flow fields predicted by the deep neural network is in good agreement with those directly calculated by the CFD solver.

CLC number: TP181;V211.3 Document code: A

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Acta Aerodynamica Sinica
Pages 51-63

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Cite this article:
DING Z, AN W, LIU X, et al. Prediction modeling of unsteady flow field aimed at high-order DG numerical scheme. Acta Aerodynamica Sinica, 2022, 40(6): 51-63. https://doi.org/10.7638/kqdlxxb-2021.0174

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Received: 12 August 2021
Revised: 10 September 2021
Published: 29 December 2021
© The journal of Acta Aerodynamica Sinica.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).