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Research Article | Publishing Language: Chinese | Open Access

On the stability of a split form CPR scheme in under-resolved flows

Feiran JIA1,2Huajun ZHU2Hong YAN1Zhenguo YAN2( )Jingchang SHI1
School of Power and Energy, Northwestern Polytechnical University, Xian 710000, China
State Key Laboratory of Aerodynamics, Mianyang 621000, China
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Abstract

The correction procedure via reconstruction (CPR) method is a compact and efficient high-order method suitable for unstructured grids. However, when discretizing the nonlinear convection term, it is easy to cause numerical instability due to the accumulation of aliasing errors. In the present work, we study the stability of the split form CPR method based on LG (Legendre-Gauss) points in under-resolved flows, and combine the method with the subcell limiting technique to solve under-resolved flows with shock waves. First, numerical tests are carried out to verify that the split form CPR method based on LG points with the boundary flux correction can satisfy the discrete conservation law, and such conservation is still preserved under subcell limiting. In the simulation of under-resolved flows without shock waves, compared to the divergence form CPR method, the split form significantly improves the stability of the calculation, and has smaller numerical errors than the split form CPR method using LGL (Legendre-Gauss-Lobatto) points. When solving under-resolved flows with shock waves, compared to the subcell limiting strategy of discontinuous Galerkin spectral element method based on LGL points, the subcell limiting strategy of split form CPR scheme based on LG points developed in this paper has higher resolution and less oscillation.

CLC number: V211.3 Document code: A

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Acta Aerodynamica Sinica
Pages 103-115

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Cite this article:
JIA F, ZHU H, YAN H, et al. On the stability of a split form CPR scheme in under-resolved flows. Acta Aerodynamica Sinica, 2023, 41(11): 103-115. https://doi.org/10.7638/kqdlxxb-2022.0128

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Received: 01 August 2022
Revised: 08 October 2022
Published: 07 February 2023
© 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/).