Advanced Search
Volume 40 Issue 12
Dec.  2014
Turn off MathJax
Article Contents
Journal of Beijing University of Aeronautics and Astronautics  > 2014  >  40(12): 1725-1729.
Zheng Weilin, Yan Chao. Influence analysis on grid scale limiter of XY-SAS model[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(12): 1725-1729. doi: 10.13700/j.bh.1001-5965.2013.0742(in Chinese)
Citation: Zheng Weilin, Yan Chao. Influence analysis on grid scale limiter of XY-SAS model[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(12): 1725-1729. doi: 10.13700/j.bh.1001-5965.2013.0742(in Chinese)
shu

Influence analysis on grid scale limiter of XY-SAS model

doi: 10.13700/j.bh.1001-5965.2013.0742

  • School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 08 Jan 2014
  • Publish Date: 20 Dec 2014
    Abstract
  • The Xu & Yan scale adaptive simulation (XY-SAS) model is based on the introduction of the von Karman length scale into the destruction term of spalart-allmaras (SA) turbulence model, which results in a large eddy simulation (LES)-like behavior in unsteady regions of the flowfield without explicit grid dependence. Because the SAS models could not provide sufficient damping of the smallest scales, the grid spacing was introduced as the high wave number damping limitation. Three different XY-SAS models were constructed by using various grid limiters and were tested by the numerical example of circular cylinder at Re=3 900. The numerical results were compared with detached eddy simulation (DES) and experimental data. It is concluded that, the grid limiter has a strong influence on the performance of the model and the minimum grid spacing is a good limitation, under which the XY-SAS model performs as well as DES method.

     

    • FullText(HTML)
  • loading
    • References(15)
  • [1]
    Fröhlich J,von Teryi D.Hybrid LES/RANS methods for the simulation of turbulent flows[J].Progress in Aerospace Sciences,2008,44(5):349-377
    [2]
    阎超,于剑,徐晶磊,等.CFD模拟方法的发展成就与展望[J].力学进展,2011,41(5):562-589 Yan Chao,Yu Jian,Xu Jinglei,et al.On the achievements and prospects for the methods of computational fluid dynamics[J].Advance in Mechanics,2011,41(5):562-589(in Chinese)
    [3]
    Menter F R,Kuntz M,Bender R.A scale-adaptive simulation model for turbulent flow predictions[C]//41st Aerospace Sciences Meeting and Exhibit.Reston,VA:American Institute of Aeronautics and Astronautics Inc,2003-0767
    [4]
    Menter F R,Egorov Y.A scale-adaptive simulation model using two-equation models[C]//43rd AIAA Aerospace Sciences Meeting and Exhibit.Reston,VA:American Institute of Aeronautics and Astronautics Inc,2005：271-283
    [5]
    Menter F R,Egorov Y.The scale-adaptive simulation method for unsteady turbulent flow predictions.Part 1:theory and model description[J].Flow,Turbulence and Combustion,2010,85(1):113-138
    [6]
    Egorov Y,Menter F R,Lechner R,et al.The scale-adaptive simulation method for unsteady turbulent flow predictions.Part 2:application to complex flows[J].Flow,Turbulence and Combustion,2010,85(1):139-165
    [7]
    Menter F R,Schütze J,Kurbatskii K A,et al.Scale-resolving simulation techniques in industrial CFD[C]//6th AIAA Theoretical Fluid Mechanics Conference.Reston,VA:American Institute of Aeronautics and Astronautics Inc,2011-3474
    [8]
    Menter F R.Review of the shear-stress transport turbulence model experience from an industrial perspective[J].International Journal of Computational Fluid Dynamics,2009,23(4):305-316
    [9]
    徐晶磊,阎超.一个一方程Scale-Adaptive Simulation模型的构造[C]//第14届全国计算流体力学会议.贵阳：[s.n.],2009:113-117 Xu Jinglei,Yan Chao.A one-equation scale-adaptive simulation model[C]//14th National Conference on CFD.Guiyang:[s.n. ],2009:113-117(in Chinese)
    [10]
    Spalart P R,Allmaras S R.A one-equation turbulence model for aerodynamic flows[C]//30th AIAA Aerospace Sciences Meeting and Exhibit.Reno,NV:American Institute of Aeronautics and Astronautics Inc,1992-0439
    [11]
    高瑞泽,徐晶磊,赵瑞,等.XY-SAS模型对分离流动的性能分析[J].北京航空航天大学学报,2010,36(4):414-418 Gao Ruize,Xu Jinglei,Zhao Rui,et al.Evaluation of XY-SAS model for separated flows[J].Journal of Beijing University of Aeronautics and Astronautics,2010,36(4):414-418(in Chinese)
    [12]
    Xu J L,Hu N,Gao G.A high-fidelity turbulence length scale for flow simulation[C]//Progress in Hybrid RANS-LES Modelling.Berlin:Springer,2012:141-145
    [13]
    Ong L,Wallace J.The velocity field of the turbulent very near wake of a circular cylinder[J].Exp Fluids,1996,20(6):441-453
    [14]
    Kravchenko A G,Moin P.Numerical studies of flow over a circular cylinder at ReD=3 900[J].Phys Fluids,2000,12(12):403-417
    [15]
    Shim Y M,Sharma R N,Richards P J.Numerical study of the flow over a circular cylinder in the near wake at Reynolds number 3 900[C]//39th AIAA Fluid Dynamics Conference.Reston,VA:American Institute of Aeronautics and Astronautics Inc,2009-4160
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(994) PDF downloads(625) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return