Volume 43 Issue 2
Feb.  2017
Turn off MathJax
Article Contents
LEI Juanmian, TAN Zhaoming. Numerical simulation for flow around circular cylinder at high Reynolds number based on Transition SST model[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(2): 207-217. doi: 10.13700/j.bh.1001-5965.2016.0098(in Chinese)
Citation: LEI Juanmian, TAN Zhaoming. Numerical simulation for flow around circular cylinder at high Reynolds number based on Transition SST model[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(2): 207-217. doi: 10.13700/j.bh.1001-5965.2016.0098(in Chinese)

Numerical simulation for flow around circular cylinder at high Reynolds number based on Transition SST model

doi: 10.13700/j.bh.1001-5965.2016.0098
Funds:

National Natural Science Foundation of China 11372040

More Information
  • Corresponding author: LEI Juanmian, E-mail:leijm@bit.edu.cn
  • Received Date: 26 Jan 2016
  • Accepted Date: 04 Mar 2016
  • Publish Date: 20 Feb 2017
  • In order to study the boundary layer transition phenomenon and the flow characteristics of flow around circular cylinder at high Reynolds number, the experimental results and the results that are obtained by using the Transition SST model and the SST k-ω model were firstly analyzed at typical Reynolds number, and the advantages of the Transition SST model was verified at high Reynolds number. Meanwhile, the boundary layer transition phenomenon and the flow characteristics were more accurately predicted. Then, the numerical simulations were performed in subcritical, critical, supercritical and over critical regions. The variation of flow field structure and the friction coefficient curve was analyzed under the different Reynolds number. The flow characteristics, flow mechanism of boundary layer transition, and variation of transition positions were studied. Results show that the boundary layer separates laminarly, and the flow does not form a separation bubble and transition phenomenon in subcritical region; in critical and supercritical region, the flow forms a separation bubble, and ultimately turbulent separation happens after transition occurs with the flow; in over critical region, the boundary layer separates turbulently after transition occurs with the flow, and the flow does not form a separation bubble; the more the Reynolds number is, the closer the transition position is to the front stagnation point of cylinder in critical, supercritical and over critical region.

     

  • loading
  • [1]
    伊杰里奇克N E.水力摩阻手册[M].北京:航空发动机编辑部, 1985:256-300.

    YI JIE RITCHIE N E.Hydraulic friction handbook[M].Beijing:Aviation Engine Newsroom, 1985:256-300(in Chinese).
    [2]
    凌国灿.圆柱绕流旋涡运动及离散涡方法[J].力学进展, 1985, 15(4):458-470. http://www.cnki.com.cn/Article/CJFDTOTAL-LXJZ198504004.htm

    LING G C.Vortex flow around a circular cylinder motion and the discrete vortex method[J].Journal of Mechanics, 1985, 15(4):458-470(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-LXJZ198504004.htm
    [3]
    苑明顺.高雷诺数圆柱绕流的二维大涡模拟[J].水动力学研究与进展:A辑, 1992, 7(Suppl.):614-622. http://www.cnki.com.cn/Article/CJFDTOTAL-SDLJ1992S1017.htm

    YUAN M S.High Reynolds number flow around a cylinder of 2-D large eddy simulation[J].Water Dynamics Research and Development:Series A, 1992, 7(Suppl.):614-622(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-SDLJ1992S1017.htm
    [4]
    王亚玲, 刘应中, 缪国平.圆柱绕流的三维数值模拟[J].上海交通大学学报, 2001, 35(10):1464-1469. http://cpfd.cnki.com.cn/Article/CPFDTOTAL-AGLU200104001020.htm

    WANG Y L, LIU Y Z, MIU G P.Three dimensional numerical simulation of viscous flow a round circular cylinder[J].Journal of Shanghai Jiaotong University, 2001, 35(10):1464-1469(in Chinese). http://cpfd.cnki.com.cn/Article/CPFDTOTAL-AGLU200104001020.htm
    [5]
    刘应中, 缪国平.高等流体力学[M].上海:上海交通大学出版社, 2000.

    LIU Y Z, MIU G P.Higher fluid mechanics[M].Shanghai:Shanghai Jiao Tong University Press, 2000(in Chinese).
    [6]
    易家训.流体力学[M].北京:高等教育学出版社, 1982.

    YI J X.Fluid mechanics[M].Beijing:Higher Education Press, 1982(in Chinese).
    [7]
    ESKINAZI S.Principles of fluid mechanics[M].Boston:Allyn and Bacon Inc., 1968.
    [8]
    SCHMIDT R, PANTANKAR S.Simulation boundary layer transition with low-reynolds number k-ε turbulence models:Part 2-An approach to improving the predictions[J].Journal of Tuebomachinery, 1991, 113(1):18-26. doi: 10.1115/1.2927732
    [9]
    VANCOILLIE G, DICK E.A turbulence model for the numerical simulation of the transition zone in a boundary layer[J].International Journal of Engineering Fluid Mechanics, 1988, 1(1):28-49. https://www.researchgate.net/publication/260974831_A_turbulence_model_for_the_numerical_simulation_of_the_transition_zone_in_a_boundary_layer
    [10]
    STEELANT J, DICK E.Modeling of laminar-turbulent transition for high freestream turbulence[J].Journal of Fluids Engineering, 2001, 123(1):22-30. doi: 10.1115/1.1340623
    [11]
    WALTERS K D, LEYLEK J H.Impact of film-cooling jets on turbine areogynamic losses[J].Journal of Turbomachinery, 2000, 122(3):537-545. doi: 10.1115/1.1303818
    [12]
    LANGTRY R B, MENTER F R.Transition modeling for general CFD applications in aeronautics[C]//43rd AIAA Aerospace Sciences Meeting and Exhibit.Reston:AIAA, 2005.
    [13]
    MENTER F R, LANGTRY R B, LIKKI S R, et al.A correlation-based transition model using local variables-Part I:Model formulation[C]//49th International Gas Turbine and Aeroengine Congress and Exhibition.New York:ASME, 2006:413-422.
    [14]
    MENTER F R, LANGTRY R B, LIKKI S R, et al.A correlation-based transition model using local variables-Part II:Test cases and industrial applications[C]//49th International Gas Turbine and Aeroengine Congress and Exhibition.New York:ASME, 2006:423-434.
    [15]
    MENTER F R.Two-equation eddy-viscosity turbulence models for engineering application[J].AIAA Journal, 1994, 32(8):1598-1605. doi: 10.2514/3.12149
    [16]
    CANTWELL B J.A flying hot wire study of the turbulent near wake of a circular cylinder at a Reynolds number of 14, 000[D].Pasadena:California Institute of Technology, 1976.
    [17]
    SCHEWE G.On the force fluctuations acting on a circular cylinder in cross flow from subcritical up to transcritical Reynolds numbers[J].Journal of Fluid Mechanics, 1983, 133(1):265-285. http://adsabs.harvard.edu/abs/1983JFM...133..265S
    [18]
    SQUIRES K D, KRISHNAN V, FORSYTHE J R.Prediction of the flow over a circular cylinder at high Reynolds number using detached-eddy simulation[J].Journal of Wind Engineering and Industrial Aerodynamics, 2008, 96(10-11):1528-1536. doi: 10.1016/j.jweia.2008.02.053
    [19]
    ACHENBACH E.Distribution of local pressure and skin friction around a circular cylinder in cross-flow up to Re=5×106[J].Journal of Fluid Mechanics, 1968, 34(4):625-639. doi: 10.1017/S0022112068002120
    [20]
    凌国灿, 牛家玉, CHWANG A T.圆柱近尾迹流动转捩特征的数值研究[J].空气动力学报, 1997, 15(1):130-138. http://www.cnki.com.cn/Article/CJFDTOTAL-KQDX199701018.htm

    LING G C, ZHU J Y, CHWANG A T.Numerical studies of cylindrical near wake flow transition characteristics[J].Acta Aerodynamica Sinica, 1997, 15(1):130-138(in Chinese). http://www.cnki.com.cn/Article/CJFDTOTAL-KQDX199701018.htm
    [21]
    WALKER J D A, SMITH C R, CERRA A W, et al.The impact of a vortex ring on a wall[J].Journal of Fluid Mechanics, 1987, 181:99-140. doi: 10.1017/S0022112087002027
    [22]
    JONES G W, CINCOTTA J J, WALKER R W.Aerodynamic forces on a stationary and oscillating circular cylinder at high Reynolds numbers:NASA TR R-300[R].Washington, D.C.:NASA, 1969.
  • 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

    Figures(14)  / Tables(2)

    Article Metrics

    Article views(1832) PDF downloads(1159) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return