期刊
PHYSICS OF FLUIDS
卷 34, 期 7, 页码 -出版社
AIP Publishing
DOI: 10.1063/5.0098122
关键词
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资金
- National Natural Science Foundation of China [11972064, 11721202, 92052104]
- Key Laboratory of Computational Aerodynamics, AVIC Aerodynamics Research Institute [YL2022XFX0405]
This paper proposes a nonintrusive reduced basis (RB) method based on dynamic mode decomposition (DMD) for parameterized time-dependent flows. The offline stage involves extracting the reduced basis functions and introducing a novel hybrid DMD regression model for the temporal evolution of the RB coefficients. To enhance stability for complex nonlinear problems, a threshold value is used to modify the DMD eigenvalues and eigenvectors. Additionally, interpolation of the coefficients in parameter space is performed using a feedforward neural network or random forest algorithm. The online stage enables the prediction of the RB solution at a new time/parameter value with low computational cost and complete decoupling from the high-fidelity dimension. The proposed model is demonstrated with two cases, showing reasonable efficiency and robustness.
This paper proposes a nonintrusive reduced basis (RB) method based on dynamic mode decomposition (DMD) for parameterized time-dependent flows. In the offline stage, the reduced basis functions are extracted by a two-step proper orthogonal decomposition algorithm. Then, a novel hybrid DMD regression model that combines windowed DMD and optimized DMD is introduced for the temporal evolution of the RB coefficients. To improve the stability of this method for complex nonlinear problems, we introduce a threshold value to modify the DMD eigenvalues and eigenvectors. Moreover, the interpolation of the coefficients in parameter space is conducted by a feedforward neural network or random forest algorithm. The prediction of the RB solution at a new time/parameter value can be recovered at a low computational cost in the online stage, which is completely decoupled from the high-fidelity dimension. We demonstrate the performance of the proposed model with two cases: (i) laminar flow past a two-dimensional cylinder and (ii) turbulent flow around a three-dimensional SD7003 airfoil. The results show reasonable efficiency and robustness of this novel reduced-order model.
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