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含激波的湍流流动高精度大涡数值模拟方法

D.V. Kotov H.C. Yee A. Wray A. Hadjadj B. Sj(o)green

空气动力学学报2016，Vol.34Issue(2)：190-203,14.

空气动力学学报2016，Vol.34Issue(2)：190-203,14.DOI:10.7638/kqdlxxb-2016.0009

含激波的湍流流动高精度大涡数值模拟方法

High Order Numerical Methods for LES of Turbulent Flows with Shocks

D.V. Kotov ¹H.C. Yee ²A. Wray ²A. Hadjadj ³B. Sj(o)green⁴

作者信息

1. Center for Turbulence Research, Stanford University, Stanford, CA 94305, USA
2. NASA Ames Research Center, Moffett Field, CA, 94035, USA
3. CORIA UMR 6614 & INSA de Rouen, 76800 St Etienne du Rouvray, France
4. Lawrence Livermore National Laboratory, Box 808, L-422, Livermore, CA 94551, USA
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摘要

关键词

高阶低耗散格式/Germao模型/大涡模拟滤波/直接数值模拟方法/亚单元分辨格式/激波湍流干扰

Key words

High order low dissipative scheme/Germano model/LES filtering/DNS/Subcell resolution scheme/Shock/turbulence interaction

引用本文复制引用

D.V. Kotov,H.C. Yee,A. Wray,A. Hadjadj,B. Sj(o)green..含激波的湍流流动高精度大涡数值模拟方法[J].空气动力学学报,2016,34(2):190-203,14.

基金项目

The support of the DOE/SciDAC SAP grant DE-AI02-06ER25796 is acknowledged.The authors are grateful to J.Larsson for providing the turbulent inflow and selected input data.The work has been performed with the first author as a postdoctoral fellow at the Center for Turbulence Research,Stanford University.Financial support from the NASA Aerosciences/RCA program for the second author is gratefully acknowledged.Work by the fifth author was performed under the auspices of the U.S.Department of Energy at Lawrence Livermore National Laboratory under Contract DE-AC52-07NA27344. （）

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