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

涡轮叶栅外换热系数计算

曾军 卿雄杰

曾军, 卿雄杰. 涡轮叶栅外换热系数计算[J]. 航空动力学报, 2008, 23(7): 1198-1204.
引用本文: 曾军, 卿雄杰. 涡轮叶栅外换热系数计算[J]. 航空动力学报, 2008, 23(7): 1198-1204.
ZENG Jun, QING Xiong-jie. External heat transfer predictions of turbine cascades[J]. Journal of Aerospace Power, 2008, 23(7): 1198-1204.
Citation: ZENG Jun, QING Xiong-jie. External heat transfer predictions of turbine cascades[J]. Journal of Aerospace Power, 2008, 23(7): 1198-1204.

涡轮叶栅外换热系数计算

External heat transfer predictions of turbine cascades

  • 摘要: 采用求解三维雷诺平均Navier-Stokes(N-S)方程和带转捩模型的二方程Shear stress transport(SST)湍流模型,完成了MARKⅡ,VKI两个高压涡轮导叶叶栅及一个VKI高压涡轮动叶叶栅的外换热系数计算.计算结果与试验数据的对比表明,发展的带转捩模型的数值方法明显地提高了外换热系数的计算精度.

     

  • [1] Crawford M E,Kays W M.STAN5 A program for numerical computation of two-dimensional internal/external boundary layer flow[R].NASA-CR-2742,1978.
    [2] Gaugler R E.Some modifications to and operating experience with the two-dimensional finite difference,boundary layer code,STANS[R].ASME Paper 81-GT-89.
    [3] Edlfelt R M C H,Elovic E.A two-dimensional boundary layer program for turbine airfoil heat transfer calculation[R].ASME Paper 82-GT-93.
    [4] Zeng J,Wang B,Kang Y.Numerical simulation of flow field in an annular turbine stator with film-cooled[R].Yokohama,Japan:The 24th ICAS Congress,2004.
    [5] 曾军.涡轮叶栅损失生成和输运的数值模拟[R].成都:中国航空学会动力分会第十二界叶轮机学术会议,2003.
    [6] 程信华,张剑,曾军.微型叶轮机气动设计研究[R].宜昌:中国航空学会动力分会第十三界叶轮机学术会,2005.
    [7] Menter F R.Two-equation eddy-viscosity turbulence models for engineering applications[J].AIAA Journal,1994,32(8):269-289.
    [8] Menter F R,Kuntz M,Langtry R.Ten years of industrial experience with SST turbulence model[M].CT:Turbulence Heat and Mass Transfer 4 Begell House Inc.,2003.
    [9] Menter F R,Langtry R B,Likki S R,et al.A correlation based transition model using local variables Part l-Model formulation[R].ASME-GT2004-53452.
    [10] Hylton L D,Mihelc M S,Turner E R,et al.Analytical and experimental evaluation of the heat distribution over the surfaces of turbine vanes[R].NASA CRl68015,1983.
    [11] Tony Arts.Aero-thermal performance of a two dimensional highly loaded transonic turbine nozzle guide vane[R].ASME 90-GT-358.
    [12] Tony Arts.External heat transfer study on a HP turbine rotor blade[R].Heat Transfer and Cooling in Gas Turbines.AGARD-CP-390:5-132.
  • 加载中
计量
  • 文章访问数:  1820
  • HTML浏览量:  144
  • PDF量:  425
  • 被引次数: 0
出版历程
  • 收稿日期:  2007-07-11
  • 修回日期:  2008-01-25
  • 刊出日期:  2008-07-28

目录

    /

    返回文章
    返回