Volume 20 Issue 2
Apr.  2005
Turn off MathJax
Article Contents
WU Hong-bin, ZHENG Xin-qian, ZHOU Sheng. Frequency Analysis of Three Dimensional Compressor Cascade Unsteady Flow Mechanism Research[J]. Journal of Aerospace Power, 2005, 20(2): 267-272.
Citation: WU Hong-bin, ZHENG Xin-qian, ZHOU Sheng. Frequency Analysis of Three Dimensional Compressor Cascade Unsteady Flow Mechanism Research[J]. Journal of Aerospace Power, 2005, 20(2): 267-272.

Frequency Analysis of Three Dimensional Compressor Cascade Unsteady Flow Mechanism Research

  • Received Date: 2004-05-30
  • Rev Recd Date: 2004-09-09
  • Publish Date: 2005-04-28
  • A simulation using unsteady Reynolds-averaged viscous turbulent equations was carried out.The results show that the flow in the separation region and wake region is characterized as periodic or quasi-periodic vortex shedding and the frequency of vortex shedding is varied with incidence and Mach number.At same Mach number,the frequency of vortex shedding decreases with the increase of incidence.Yet,the frequency increases with the increase of Mach number keeping incidence unchanged.In the same situation,the frequency of vortex shedding differs along the span of the cascades.The frequency is lower at the middle of the span than that at the hub.

     

  • loading
  • 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

    Article Metrics

    Article views (1797) PDF downloads(436) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return