Volume 21 Issue 3
Jun.  2006
Turn off MathJax
Article Contents
Article Navigation >  Journal of Aerospace Power  > 2006  >  21(3): 455-460
GONG Zhi-qiang, LU Yajun, GE Jing-dong. Investigation of Unsteady Flow Control in an Annular Compressor Cascade Using PIV[J]. Journal of Aerospace Power, 2006, 21(3): 455-460.
Citation: GONG Zhi-qiang, LU Yajun, GE Jing-dong. Investigation of Unsteady Flow Control in an Annular Compressor Cascade Using PIV[J]. Journal of Aerospace Power, 2006, 21(3): 455-460.
shu

Investigation of Unsteady Flow Control in an Annular Compressor Cascade Using PIV

  • National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • Received Date: 2005-06-08
  • Rev Recd Date: 2005-10-28
  • Publish Date: 2006-06-28
    Abstract
  • A synthetic jet generator was used as an active control method to control the flow in an annular compressor cascade.It was found that the total pressure loss of the cascade could be reduced effectively.2D Particle Image Velocimetry(PIV) was used to measure the flow field around the blades.Flow fields were acquired under different incidences,jet frequencies and intensities.It was found that synthetic jet had huge impact on the flow field.With proper jet frequency and intensity,flow separation on the blade suction surface was suppressed evidently,and the blade wake intensity and width were reduced.Streamlines around the blade were smoother.These changes were consistent with the decrease of total pressure loss.The mechanism of this active control method was analyzed.

     

    • FullText(HTML)
  • loading
    • References(6)
  • [1]
    Ahuja K K,Burrin R H.Control of Separation by Sound[R].AIAA-84-2298,1984.
    [2]
    McManus K,Magill J.Airfoil Performance Enhancement Using Pulsed Jet Separation Control[R].AIAA-97-1971,1997.
    [3]
    钟芳源,董国平,罗次申.扰动来流下声控机翼分离流动的研究[J].航空动力学报,1998,13(2):113～118.Zhong Fang-yuan,Dong Guo-ping,Luo Ci-shen.Acoustic Control of Separated Flow over a 2-Dimensional Airfoil at Disturbed Incoming Flow[J].Journal of Aerospace Power,1998,13(2):113～118.
    [4]
    闻学,李志平,周海,葛敬东.对环形叶栅内非定常流动特征参数的实验研究[J].航空动力学报,2002,17(5):561～566.Wen Xue,Li Zhiping,Zhou Hai,Ge Jingdong.Research of the Unsteady-Fluid Characteristic Parameter in an Annular Cascade[J].Journal of Aerospace Power,2002,17 (5):561 ～566.
    [5]
    邱亚希,葛敬东,周海,陆亚钧.环形叶栅内利用非定常激励减少分离区损失的研究[J].流体力学实验与测量,2003,17(1):18～23.Qiu Yaxi,Ge Jingdong,Zhou Hai,Lu Yajun.Research on the Effects of Unsteady Excitation on Enhancing Performance of Annular Cascade[J].Experiments and Measurements in Fluid Mechanics,2003,17(1):18～23.
    [6]
    刘宝杰,严明,刘胤,王同庆.跨音风扇转子尖部非定常流场的PIV初步测量[J].航空动力学报,2001,16(2):147～152.Liu Baojie,Yan Ming,Liu Yin,Wang Tongqing.Preliminary PIV Measurement of Unsteady Tip Flow in a Transonic Fan Rotor[J].Journal of Aerospace Power,2001,16 (2):147 ～152.
    • 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(1232.0KB)
    XML

    Article Metrics

    Article views (1824) PDF downloads(478) 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