Volume 21 Issue 6
Dec.  2006
Turn off MathJax
Article Contents
Article Navigation >  Journal of Aerospace Power  > 2006  >  21(6): 1027-1032
YANG Zi-feng, WANG Xiao-yu, SUN Xiao-feng. Effect of finite-length casing treatment on cascade aero-elastic stability[J]. Journal of Aerospace Power, 2006, 21(6): 1027-1032.
Citation: YANG Zi-feng, WANG Xiao-yu, SUN Xiao-feng. Effect of finite-length casing treatment on cascade aero-elastic stability[J]. Journal of Aerospace Power, 2006, 21(6): 1027-1032.
shu

Effect of finite-length casing treatment on cascade aero-elastic stability

  • School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • Received Date: 2005-11-28
  • Rev Recd Date: 2006-03-07
  • Publish Date: 2006-12-28
    Abstract
  • The application of casing treatment to the control of blade flutter may have advantages particularly compared with the existing methods of suppressing blade flutter.In the present paper,a novel method,which is called transfer element method,has been proposed to establish an aero-elastic model,which considers the effect of finite-length casing treatment on the blade flutter inception. The present model avoids the difficulty of solving eigenvalue due to impedance wall condition effectively.In particular,the numerical results show that the value of impedance of lining wall has a marked effect on the aero-elastic stability.The possibility of using finite-length casing treatment to suppress the blade flutter has been concluded.

     

    • FullText(HTML)
  • loading
    • References(9)
  • [1]
    Sun Xiao-feng,Jing Xiao-dong,Zhao Hong-wu.Control of blade flutter by smart-casing treatment[J].Journal of Propulsion and Power,March-April 2001,17(2):248-255.
    [2]
    Watanabe T,Kaji S.Possibility of cascade flutter suppression by use of nonrigid duct wall[A].Proceedings Third International Symposium on Aeroelasticity in Turbomachines[C].Cambridge Univ.,Cambridge,Engla-nd,U.K.,1984,pp.261-276.
    [3]
    Namb M,Yamsaki N,Kurihara Y.Some three-di-mensional effects on unsteady aerodynamic forces on oscillating cascades[A].Proceeding of the Third Internat-ional Symposium on Aeroelasticity in Turbomachines[C].Cambridge Univ.,Cambridge,England,U.K.,1984,pp.217-230.
    [4]
    Namba M,Fukushige K.Application of the equivalent surface source method to the acoustic of duct systems with non-uniform wall impedance[J].Journal of Sound and Vibration 1982,73:125-146.
    [5]
    Sun X,Kaji S.Control of blade flutter using casing with Acoustic Treatment[J].Journal of Fluids and Structure,2002,16(5):627-648.
    [6]
    Sun Xiao-feng,Kaji Shojiro.Effects of wall admittance changes on aeroelastic stability of turbomachin es[J].AIAA Journal,September 2000,38(9):1 525-1 533.
    [7]
    王晓宇,孙晓峰.等价分布源的新发展[J].工程热物理学报,2006,增刊27(1):109-112.
    [8]
    王晓宇,杜林,孙晓峰.考虑变截面影响的航空发动机短舱声学模型及数值结果[J].航空学报,2006,27(6):1073-1079.
    [9]
    Smith S N.Discrete Frequency Sound Generation in Axial Flow Turbomachines[R].ARC Reports and Mem-oranda,1972,No.3709.
    • 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(813.0KB)
    XML

    Article Metrics

    Article views (1578) PDF downloads(467) 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