留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

高超声速热流计算湍流模型性能评估

张翔 阎超

张翔, 阎超. 高超声速热流计算湍流模型性能评估[J]. 北京航空航天大学学报, 2015, 41(2): 337-342. doi: 10.13700/j.bh.1001-5965.2014.0109
引用本文: 张翔, 阎超. 高超声速热流计算湍流模型性能评估[J]. 北京航空航天大学学报, 2015, 41(2): 337-342. doi: 10.13700/j.bh.1001-5965.2014.0109
ZHANG Xiang, YAN Chao. Property evaluation on turbulence models calculation in hypersonic heat transfer simulation[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(2): 337-342. doi: 10.13700/j.bh.1001-5965.2014.0109(in Chinese)
Citation: ZHANG Xiang, YAN Chao. Property evaluation on turbulence models calculation in hypersonic heat transfer simulation[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(2): 337-342. doi: 10.13700/j.bh.1001-5965.2014.0109(in Chinese)

高超声速热流计算湍流模型性能评估

doi: 10.13700/j.bh.1001-5965.2014.0109
详细信息
    作者简介:

    张翔(1989—), 男, 陕西宝鸡人, 硕士生, zx906@126.com

    通讯作者:

    阎超(1962—), 男, 江苏徐州人, 教授, yanchao@buaa.edu.cn, 主要研究方向为计算流体力学.

  • 中图分类号: V211.3

Property evaluation on turbulence models calculation in hypersonic heat transfer simulation

  • 摘要: 采用计算流体力学方法,通过对高超声速来流下双椭球热流计算,综合分析了影响壁面热流预测精度的因素.针对工程上4种常用的湍流模型:BL(Baldwin-Lomax)模型、SA(Spalart-Allmaras)模型、k-ω模型及SST(Shear-Stress Transport)模型,评估了其在高超声速热流预测中的性能,获得了湍流模型下壁面法向网格雷诺数对热流计算的影响规律.此外,对高马赫数下不同后掠角钝舵模型进行热流计算,获得了后掠角对钝舵前缘热流峰值的影响规律.研究表明,两方程湍流模型相比一方程和零方程模型更适合高超声速气动热计算,其中SST模型对热流预测精度更高,总体性能更为优异;钝舵驻点线最大热流随后掠角增大呈非单调变化,在后掠角约为22°时热流达到峰值.

     

  • [1] Bertin J J, Cummings R M.Critical hypersonic aerothermodynamic phenomena[J].Annual Review of Fluid Mechanics, 2006,38:129-157.
    [2] 姜振华, 阎超.高超声速热流高精度数值模拟方法[J].北京航空航天大学学报,2011,37(12):1529-1533. Jiang Z H,Yan C. High order accurate methods in numerical simulation of hypersonic heat transfer[J].Journal of Beijing University of Aeronautics and Astronautics,2011,37(12):1529-1533(in Chinese).
    [3] 潘沙,冯定华, 丁国昊,等.气动热数值模拟中的网格相关性及收敛[J].航空学报,2010,31(3):493-499. Pan S,Feng D H,Ding G H,et al.Grid dependency and convergence of hypersonic aerothermal simulation[J].Acta Aeronautica et Astronautica Sinica, 2010,31(3):493-499(in Chinese).
    [4] 李君哲, 阎超.气动热CFD计算的格式效应研究[J].北京航空航天大学学报,2003,29(11):1022-2025. Li J Z,Yan C.Research on scheme effect of computational fluid dynamics in aerothermal[J].Journal of Beijing University of Aeronautics and Astronautics,2003,29(11):1022-2025(in Chinese).
    [5] Klopfer G H, Yee H C.Viscous hypersonic shock/shock interaction on blunt line cowl lips,AIAA-1988-0233[R].Reston:AIAA,1988.
    [6] Hoffmann K A, Siddiqui M S,Chiang S T.Difficulties associated with the heat flux computations of high speed flow by the Navier-Stokes equations,AIAA-1991-0457[R].Reston:AIAA,1991.
    [7] Benard E, Cooper R K,Sidorenko A.Transitional and turbulent heat transfer of swept cylinder attachment line in hypersonic flow[J].International Journal of Heat and Mass Transfer,2006,49(5-6): 836-843.
    [8] 朱辉玉, 王刚, 孙泉华, 等.高超声速飞行器气动热数值模拟的几个关键因素[C]//第三届高超声速科技学术会议会议文集.北京:中国力学学会, 2010:0056-1-8. Zhu H Y,Wang G,Sun Q H,et al.Some critical factors in hypersonic aerothermal simulation[C]//Proceedings of Third Hypersonic Technology Academic Conference.Beijing:CSTAM,2010:0056-1-8(in Chinese).
    [9] 贺旭照, 赵慧勇,乐嘉陵.吸气式高超声速飞行器气动力气动热的数值模拟方法及应用[J].计算物理,2008,25(5):555-560. He X Z,Zhao H Y,Le J L.Aerodynamic force and heat of hypersonic laminar and turbulent flow[J].Chinese Journal of Computational Physics, 2008,25(5):555-560(in Chinese).
    [10] 李素循. 激波与边界层主导的复杂流动[M].北京:科学出版社,2007:11-51, 146-148. Li S X.The complex flow caused by shock/boundary interaction[M].Beijing:Science Press,2007:11-51, 146-148(in Chinese).
    [11] Wilcox D C. Turbulence modeling for CFD[M].3rd ed.California:DCW Industries Inc,2006:243-249.
    [12] 阎超. 计算流体力学方法与应用[M].北京:北京航空航天大学出版社,2006:221-223. Yan C.The methods and application of computational fluid dynamics[M].Beijing:Beihang University Press,2006:221-223(in Chinese).
    [13] van Leer B. Towards the ultimate conservative difference scheme.V.A second-order sequel to Godunov's method[J].Journal of Computational Physics,1997,135(2):227-248.
    [14] 耿云飞, 阎超,徐晶磊,等.高超声速流动湍流模式评估[J].北京航空航天大学学报,2011,37(8):907-911. Geng Y F,Yan C,Xu J L,et al.Turbulent modeling validation in hypersonic flow[J].Journal of Beijing University of Aeronautics and Astronautics,2011,37(8):907-911(in Chinese).

  • 加载中
计量
  • 文章访问数:  1135
  • HTML全文浏览量:  14
  • PDF下载量:  621
  • 被引次数: 0
出版历程
  • 收稿日期:  2014-03-11
  • 网络出版日期:  2015-02-20

目录

    /

    返回文章
    返回
    常见问答