A very fast high-order flux reconstruction for Finite Volume schemes for Computational Aeroacoustics

被引:0
作者
Ramirez, Luis [1 ]
Fernandez-Fidalgo, Javier [2 ]
Paris, Jose [1 ]
Deligant, Michael [3 ]
Khelladi, Sofiane [3 ]
Nogueira, Xesus [1 ]
机构
[1] Univ A Coruna, Ctr Technol Innovat Construct & Civil Engn CITEEC, Civil Engn Sch, Grp Numer Methods Engn GMNI, Campus Elvina, La Coruna 15071, Spain
[2] Univ Politecn Madrid, Dept Ingn Geol & Min, ETSI Minas & Energia, Calle Rios Rosas 21, Madrid 28003, Spain
[3] LIFSE, Arts & Metiers Inst Technol CNAM, F-75013 Paris, France
关键词
High-order methods; Finite volume; Mean preserving moving least squares; Computational aeroacoustics; ESSENTIALLY NONOSCILLATORY SCHEMES; UNSTRUCTURED MESHES; DIFFERENCE SCHEMES; FLOW; INTERPOLATION; ALGORITHM; SOLVERS;
D O I
10.1007/s00366-024-02039-2
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
Given the small wavelengths and wide range of frequencies of the acoustic waves involved in Aeroacoustics problems, the use of very accurate, low-dissipative numerical schemes is the only valid option to accurately capture these phenomena. However, as the order of the scheme increases, the computational time also increases. In this work, we propose a new high-order flux reconstruction in the framework of finite volume (FV) schemes for linear problems. In particular, it is applied to solve the Linearized Euler Equations, which are widely used in the field of Computational Aeroacoustics. This new reconstruction is very efficient and well suited in the context of very high-order FV schemes, where the computation of high-order flux integrals are needed at cell edges/faces. Different benchmark test cases are carried out to analyze the accuracy and the efficiency of the proposed flux reconstruction. The proposed methodology preserves the accuracy while the computational time relatively reduces drastically as the order increases.
引用
收藏
页码:667 / 680
页数:14
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