Volume 23 Issue 7
Jul.  2008
Turn off MathJax
Article Contents
Article Navigation >  Journal of Aerospace Power  > 2008  >  23(7): 1232-1239
SUN Da-wei, QIAO Wei-yang, XU Kai-fu, LI Wei. Influence of different incidences on loss in turbine cascade[J]. Journal of Aerospace Power, 2008, 23(7): 1232-1239.
Citation: SUN Da-wei, QIAO Wei-yang, XU Kai-fu, LI Wei. Influence of different incidences on loss in turbine cascade[J]. Journal of Aerospace Power, 2008, 23(7): 1232-1239.
shu

Influence of different incidences on loss in turbine cascade

  • School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China

  • Received Date: 2007-07-02
  • Rev Recd Date: 2007-12-20
  • Publish Date: 2008-07-28
    Abstract
  • A pressure-correction 3-Dcomputational fluid dynamics(CFD) code was used to simulate numerically the flow fluid of turbine cascade with different incidences.And three turbine loss models of off-design operating condition were analyzed and compared on the basis of the CFDnumerical simulation.The results show that the total pressure loss increases with the increase of incidence,provided that the incidence is positive;the total pressure loss decreases a little and then increases with the increase of incidence,provided that the incidence is negative.Though three turbine loss models of off-design operating condition can show the changing tendency of the total pressure loss with the change of incidence,the prediction results differ a lot.

     

    • FullText(HTML)
  • loading
    • References(12)
  • [1]
    Jouini D B M,Sjolander S A.Midspan flow-field measurements for two transonic linear turbine cascadesat off-design conditions[J].ASME J.Turbomach.,2002,124:176-186.
    [2]
    Jouini D B M,Sjolander S A,Off-design performance of a single-stage transonicturbine.[R].ASME Paper.2000-GT-0482.
    [3]
    Benner M W,Sjolander S A,Moustapha S H.Measurements of secondary flows downstream of a turbine cascade at off-design incidence[R].ASME Paper GT2004-53786.
    [4]
    Benner M W,Sjolander S A,Moustapha S H.Measurements of secondary flows in turbine cascade at off-design incidence[R].ASME Paper 97-Gt-382.
    [5]
    钟兢军,苏杰先,王仲奇.等.不同冲角下弯曲扩压叶栅出口流场的实验研究[J].工程热物理,1995,16(3):284-289.ZHONG Jingjun,SU Jiexian,WANG Zongqi,et al.Experrimetal investigation of compressor cascade exit flow field with curved blades at difeerent incidences[J].Journal of Engineeing Thermophysics,1995,16(3):284-289.(in Chinese)
    [6]
    钟兢军,苏杰先,王仲奇.不同冲角下弯曲扩压叶栅壁面静压的实验研究[J].航空动力学报.1995,10(4):365-368.ZHONG Jingjun,SU Jiexian,WANG Zongqi.Experimental investigation of surface static pressure in curved blade compressor cascade at different incidences[J].Journal of Aerospace Power,1995,10(4):365-368.(in Chinese)
    [7]
    Smith D J L,Johnston I H.Investigations on an experimental single-stage turbine of conservative design[R].Reports and Memoranda No.3541.1967.
    [8]
    Benner M W,Sjolander S A,Moustapha S H.An empirical prediction method for secondary losses in turbines-part I:A new loss breakdown scheme and penetration depth correlation[J].ASME J.Turbomach.2006,128:273-280.
    [9]
    Ainley D G,Mathieson G C R.A method of performance estimation for axial-flow turbine[R].British Aeronautical Research Council,R and M 2974,1951.
    [10]
    Dunham J,Came P M.Improvements to the Ainley-Mathieson method of turbine performance prediction[R].ASME,70-GT-2.
    [11]
    Kacker S C,Okapuu U.A mean line prediction method for axial flow turbine efficiency[R].ASME 81-GT-58.
    [12]
    Moustapha S H,Kacker S C,Tremblay B.An improved incidence losses prediction method for turbine airfoils[R].ASME 89-GT-284.
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 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
    Get Citation
    PDF(2951.0KB)
    XML

    Article Metrics

    Article views (1605) PDF downloads(443) Cited by()
    Proportional views
    Related

    Copyright © 《Journal of Aerospace Power》 All Rights Reserved.

    Supported by: Beijing Renhe Information Technology Co., Ltd.  

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return