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

具有不同翼刀的压气机叶栅二次流结构分析

刘艳明 钟兢军 王保国 刘淑艳

刘艳明, 钟兢军, 王保国, 刘淑艳. 具有不同翼刀的压气机叶栅二次流结构分析[J]. 航空动力学报, 2008, 23(7): 1240-1245.
引用本文: 刘艳明, 钟兢军, 王保国, 刘淑艳. 具有不同翼刀的压气机叶栅二次流结构分析[J]. 航空动力学报, 2008, 23(7): 1240-1245.
LIU Yan-ming, ZHONG Jing-jun, WANG Bao-guo, LIU Shu-yan. Analysis of secondary flow structures of compressor cascade with different fences[J]. Journal of Aerospace Power, 2008, 23(7): 1240-1245.
Citation: LIU Yan-ming, ZHONG Jing-jun, WANG Bao-guo, LIU Shu-yan. Analysis of secondary flow structures of compressor cascade with different fences[J]. Journal of Aerospace Power, 2008, 23(7): 1240-1245.

具有不同翼刀的压气机叶栅二次流结构分析

基金项目: 国家自然科学基金(50076009);973项目和全国优秀博士学士论文作者专项基金(199932)

Analysis of secondary flow structures of compressor cascade with different fences

  • 摘要: 给出了具有端壁翼刀、吸力面翼刀和组合翼刀的可控扩散叶型(CDA)压气机叶栅的二次流结构简图.端壁翼刀和吸力面翼刀分别通过阻断端壁横向流动和展向流动来对栅内二次流进行控制,不同程度上可使叶栅总损失得到降低;组合翼刀叶栅兼顾了端壁翼刀、吸力面翼刀叶栅中二次流的特点;最佳组合翼刀并不是最佳端壁翼刀和最佳吸力面翼刀的简单组合,它需要一个更详细的优化过程.不同翼刀在不同程度上改善栅内流动状况的同时,也伴随着端壁翼刀涡、吸力面翼刀涡和类通道涡的形成和发展,这使栅内旋涡结构较常规叶栅更为复杂.

     

  • [1] Betz A.Uber die vorgange an den schaufelenden yon Kaplan-turbinen[R].Berlin:Hydraulishe Problem,VDI-Verlag,1926:161-179.
    [2] Cater A D,Cohen E M.Preliminary investigation into the three-dimensional flow through a cascade of aerofoils[R].Aeronautical Research Council Reports and Memoraanda,No.2339,1946.
    [3] Denton J D.Loss mechanism in turbomachines[R].ASME Paper 93-GT-435.
    [4] Sieverding C H.Recent progress in the understanding of basic aspects of secondary flows in turbine blade passages[J].ASME J.of Eng.for Gas Turbines and Power,1985,107(2):248-257.
    [5] Harthone W R.The application of secondary flow analysis to internal flow problems[J].Fluid Mechanics of Internal Flow,Elsevier,G.Sovran,1974:391-401.
    [6] Herizig H Z,Hanson A G.A visualization of secondary flows in cascade[R].NASA Report 116,1953.
    [7] Klein A.Investigation of the entry boundary layer on the secondary flow in the blading of axial turbine[R].BHRA T-1004,1996.
    [8] Langston L S.Cross flow in a turbine cascade passage[J].ASME Journal of Engineering for Power,1980,102:866-874.
    [9] Sharma O P,Butler T L.Prediction of end wall losses and secondary flows in axial flow turbine cascade[J].ASME Journal of Turbomachinery,1987,109:229-236.
    [10] Goldstein R J,Spores R A.Turbulent transport on the end wall in the region between adiacent turbine blades[J].ASME Journal of Heat Transfer,1988,110:862-869.
    [11] Shakaba I M,Bradshaw P.Turbulent flow measurement in an idealized wing-body jounction[J].AIAA J,1981,19:131-132.
    [12] Terual M F N.An experimental and computational study of flow in the endwall region of a turbine cascade passage[D].Calnifornia:PhD Dissertation,Dept.of Mechanical Engineering,Stanford University,1995.
    [13] Wang H P.Flow Visualization in a linear turbine cascade of high performance turbine blade[R].ASME Paper 95-GT-7.
    [14] Tatsuo KAWAI,Shuji SHINOKI,Tsutomu ADACHL.Visualization study of three-dimensional flows in a turbine cascade endwall region[J].JSME International Journal,Series Ⅱ,1990,33(2):256-262.
    [15] 钟兢军,刘艳明,冯国泰.端壁翼刀控制压气机叶栅二次流的数值研究[J].航空动力学报,2004,19(6):817-821.ZHONG Jingjun,LIU Yanming,FENG Guotai.Numerical investigation of the secondary flow control in a compressor cascade using endwall fences[J].Journal of Aerospace Power,2004,19(6):817-821.(in Chinese)
    [16] 刘艳明,钟兢军,黄洪雁,等.不同高度端壁翼刀对压气机叶栅二次流影响的数值研究[J].航空动力学报,2004,19(6):828-833.LIU Yanming,ZHONG Jingjun,HUANG Hongyan,et al.Numerical simulation of the influence of endwall fence height on the secondary flow in compressor cascade[J].Journal of Aerospace Power,2004,19(6):828-833.(in Chinese)
    [17] 刘艳明,钟兢军,王松涛,等.不同冲角下端壁翼刀最佳位置变化规律的数值研究[J].航空动力学报,2004,19(6):811-815.LIU Yanming,ZHONG Jingjun,WANG Songtao,et al.Numerical investigation of the optimal endwall fence location with the variation of Incidences[J].Journal of Aerospace Power,2004,19(6):811-815.(in Chinese)
    [18] 刘艳明,钟兢军,李海滨,等.不同长度端壁翼刀对压气机叶栅_二次流影响的数值研究[J].航空动力学报,2004,19(5):197-201.LIU Yanming,ZHONG Jingjun,LI Haibin,et al.The influence of endwall wing fence length on secondary flow in compressor cascade[J].Journal of Aerospace Power.2004,19(5):197-201.(in Chinese)
    [19] 刘艳明,钟兢军,伍耐明,等.吸力面翼刀对压气机叶栅内二次的影响[J].推进技术,2006,27(4);316-320.LIU Yanming,ZHONG Jingjun,WU Naiming,et al.Effect of using blade boundary layer fences on the secondary flow in compressor cascade[J].Journal of Propulsion Technology,2006,27(4):316-320.(in Chinese)
    [20] 刘艳明.翼刀控制压气机叶栅二次流的数值研究[D].哈尔滨:哈尔滨工业大学,2004.LIU Yanming.Numerical simulation on compressor cascade secondary flow with different fences.[D].Harbin:Harbin Institute of Technology,2004.(in Chinese)
    [21] 刘艳明.钟兢军,伍耐明,等.组合翼刀压气机叶栅的气动特性及其寻优过程[R].中国工程热物理学会,2005年第十一届学术会议.编号:052011,2005.LIU Yanming,ZHONG Jingjun,WU Naiming,et al.Aerodynamic performance and its optimization of compressor cascade with combined fences[R].The 11th Chinese Engineering Thermophysics Academy,No.052011,2005.(in Chinese)
    [22] 刘艳明.可控扩散叶型压气机叶栅气动特性的实验研究[D].哈尔滨:哈尔滨工业大学,2001.LIU Yanming.Experimental investigation of aerodynamic performance in compressor cascade with controlled diffusion airfoils[D].Harbin:Harbin Institute of Technology,2001.(in Chinese)
    [23] 田夫.端壁翼刀控制压气机叶栅二次流的实验研究[D].哈尔滨:哈尔滨上业大学,2002.TIAN Fu.Experimental investigation of compressor cascade secondary flow control with endwall fences[D],Harbin:Harbin Institute of Technology,2002.(in Chinese)
    [24] 朱东保.不同参数的翼刀对CDA叶栅端壁流动控制的实验研究[D].哈尔滨:哈尔滨工业大学,2003.ZHU Dongbao.Experimental investigation of CDA cascade endwall flow control using different fences[D].Harbin:Harbin Institute of Technology,2003.(in Chinese)
  • 加载中
计量
  • 文章访问数:  1448
  • HTML浏览量:  3
  • PDF量:  435
  • 被引次数: 0
出版历程
  • 收稿日期:  2007-08-09
  • 修回日期:  2007-12-17
  • 刊出日期:  2008-07-28

目录

    /

    返回文章
    返回