Volume 23 Issue 2
Feb.  2008
Turn off MathJax
Article Contents
Article Navigation >  Journal of Aerospace Power  > 2008  >  23(2): 361-366
JIANG Yong-song, WANG Yong-mei, DU Hui, GUO Jie. Plenum chamber casing treatment——numerical research of internal flow and mechanism of stall margin improvements[J]. Journal of Aerospace Power, 2008, 23(2): 361-366.
Citation: JIANG Yong-song, WANG Yong-mei, DU Hui, GUO Jie. Plenum chamber casing treatment——numerical research of internal flow and mechanism of stall margin improvements[J]. Journal of Aerospace Power, 2008, 23(2): 361-366.
shu

Plenum chamber casing treatment——numerical research of internal flow and mechanism of stall margin improvements

  • Shenyang Aeroengine Research Institute, Shenyang 110015, China

  • Received Date: 2007-01-15
  • Rev Recd Date: 2007-04-09
  • Publish Date: 2008-02-28
    Abstract
  • The influence of plenum chamber casing treatment on the performance of high loaded and high-speed fan rotor was analyzed through steady simulation.The results indicate that the performance of the same casing treatment differs greatly under different rotational speeds.At the design speed,the casing treatment fails to improve the stall margin of fan rotor,and the efficiency declines by 2.8%.at non-design speed,it enhances significantly the stability of the rotor,without impairment of the rotor performance.The in-depth analysis of the flow field in the casing treatment reveals the inherent mechanism of stall margin improvements by the plenum chamber casing treatment.

     

    • FullText(HTML)
  • loading
    • References(6)
  • [1]
    Koch C C.Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor[R].NASA CR-54592,1970.
    [2]
    Rabe D C,Hah C.Application of casing circumferential grooves for improved stall margin in a transonic axial compressor[R].ASME Paper GT-2002-30641.
    [3]
    Wilke I,Kau H P.A numerical investigation of the influence of casing treatments on the tip leakage flow in a HPC front stage[R].ASME Paper GT-2002-30642.
    [4]
    Wilke I,Kau H P.A numerical investigation of the flow mechanisms in a HPC front stage with axial slots[R].ASME Paper GT2003-38481.
    [5]
    Yang H,Nuernberger D,Nicke E,et al.Numerical investigation of casing treatment mechanisms with a conservative mixed-cell approach[R].ASME Paper GT2003-38483.
    [6]
    Madden D S,West M A.Effects of inlet distortion on the stability of an advanced military sweep fan stage with casing treatment[R].ASME Paper GT2005-68693.
    • 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(1113.0KB)
    XML

    Article Metrics

    Article views (1460) PDF downloads(391) 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