An Improved Second-Order Finite-Volume Algorithm for Detached-Eddy Simulation Based on Hybrid Grids

被引:3
作者
Zhang, Yang [1 ,2 ]
Zhang, Laiping [1 ,3 ]
He, Xin [1 ,3 ]
Deng, Xiaogang [4 ]
机构
[1] China Aerodynam Res & Dev Ctr, State Key Lab Aerodynam, Mianyang 621000, Sichuan, Peoples R China
[2] China Aerodynam Res & Dev Ctr, Low Speed Aerodynam Inst, Mianyang 621000, Sichuan, Peoples R China
[3] China Aerodynam Res & Dev Ctr, Computat Aerodynam Inst, Mianyang 621000, Sichuan, Peoples R China
[4] Natl Univ Def Technol, Changsha 410073, Hunan, Peoples R China
基金
中国国家自然科学基金;
关键词
Detached-Eddy simulation; second order scheme; self-adaptive dissipation; hybrid grid; finite-volume method; CONSERVATION-LAWS; DG/FV METHODS; VORTEX BREAKDOWN; FORMULATION;
D O I
10.4208/cicp.190915.240216a
中图分类号
O4 [物理学];
学科分类号
0702 ;
摘要
A hybrid grid based second-order finite volume algorithm has been developed for Detached-Eddy Simulation (DES) of turbulent flows. To alleviate the effect caused by the numerical dissipation of the commonly used second order upwind schemes in implementing DES with unstructured computational fluid dynamics (CFD) algorithms, an improved second-order hybrid scheme is established through modifying the dissipation term of the standard Roe's flux-difference splitting scheme and the numerical dissipation of the scheme can be self-adapted according to the DES flow field information. By Fourier analysis, the dissipative and dispersive features of the new scheme are discussed. To validate the numerical method, DES formulations based on the two most popular background turbulence models, namely, the one equation Spalart-Allmaras (SA) turbulence model and the two equation k - omega Shear Stress Transport model (SST), have been calibrated and tested with three typical numerical examples (decay of isotropic turbulence, NACA0021 airfoil at 60 degrees incidence and 65 degrees swept delta wing). Computational results indicate that the issue of numerical dissipation in implementing DES can be alleviated with the hybrid scheme, the resolution for turbulence structures is significantly improved and the corresponding solutions match the experimental data better. The results demonstrate the potentiality of the present DES solver for complex geometries.
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页码:459 / 485
页数:27
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