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基于熵限制的Baldwin-Lomax湍流模型

赵瑞 阎超 于剑

赵瑞, 阎超, 于剑等 . 基于熵限制的Baldwin-Lomax湍流模型[J]. 北京航空航天大学学报, 2012, (2): 175-179,190.
引用本文: 赵瑞, 阎超, 于剑等 . 基于熵限制的Baldwin-Lomax湍流模型[J]. 北京航空航天大学学报, 2012, (2): 175-179,190.
Zhao Rui, Yan Chao, Yu Jianet al. New kind Baldwin-Lomax turbulence model under the limit of entropy[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (2): 175-179,190. (in Chinese)
Citation: Zhao Rui, Yan Chao, Yu Jianet al. New kind Baldwin-Lomax turbulence model under the limit of entropy[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (2): 175-179,190. (in Chinese)

基于熵限制的Baldwin-Lomax湍流模型

基金项目: 国家973计划资助项目(2009CB724104)
详细信息
  • 中图分类号: V 211.3

New kind Baldwin-Lomax turbulence model under the limit of entropy

  • 摘要: 针对Baldwin-Lomax(BL)模型在模拟超声速复杂流动中的不足,提出一种基于熵限制的新型修正方式.分别采用原始的BL模型(BL-origin)、修正后的BL模型(BL-entropy)以及Wilcox k-ω两方程模型对超声速平板、超声速二维压缩拐角以及膨胀-压缩拐角3个典型算例进行计算,结果表明BL-entropy 能够较好地获取长度尺度进而得到均匀合理的涡粘性分布.同时,该修正方式简单高效并且适用于其他与超声速边界层有关的模型,具有较大的发展潜力.

     

  • [1] Baldwin B S, Lomax H. Thin layer approximation and algebraic model for seperated turbulent flows[R]. AIAA-78-257, 1978
    [2] Degani D, Schiff L B. Computation of supersonic viscous flows around pointed bodies at large incidence[R]. AIAA-83-0034, 1983
    [3] Panaras A G, Steger J L. A thin-layer solution of the flow about a prolate spheroid [J]. Z Flugwiss, 1988(12):173-180
    [4] Panaras A G. Algebraic turbulence modeling for swept shock-wave/turbulent boundary-layer interactions [J]. AIAA Journal, 1997,35(2):456-463
    [5] Shang J S, Hankey W L, Jr. Numerical solution for supersonic turbulent flow over a compression ramp[J]. AIAA Journal, 1975,13(10):1368-1374
    [6] Wilcox D C. Reassessment of the scale determining equation for advanced turbulence models[J]. AIAA Journal, 1988, 26(11): 1299-1310
    [7] Gao H, Fu D X, Ma Y W, et al. Direct numerical simulation of supersonic turbulent boundary layer flow[J]. Chinese Physics Letters, 2005, 22(7): 1709-1712
    [8] Settles G S, Dodson L J. Hypersonic shock/boundary-layer interaction database[R]. NASA-CR-177577, 1991
    [9] Visbal M, Knight D. The Baldwin-Lomax turbulence model for two-dimensional shock-wave/boundary-layer Interactions[J]. AIAA Journal, 1984,22(7):921-928
    [10] Forsythe R, Hoffmann A, Damevin M. An assessment of several turbulence models for supersonic compression ramp flow[R]. AIAA 98-2648, 1998
    [11] Knight D. RTO WG 10: test cases for CFD validation of hypersonic flight[R]. AIAA 2002-0433, 2002
    [12] Knight D, ran H, Panaras A, et al. RTO WG 10: CFD validation for shock wave turbulent boundary layer interactions[R]. AIAA 2002-0437, 2002
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  • 被引次数: 0
出版历程
  • 收稿日期:  2010-11-12
  • 网络出版日期:  2012-02-29

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