Volume 24 Issue 1
Jan.  2009
Turn off MathJax
Article Contents
ZHOU Bin, WANG Xue-song, WANG Guo-yu, XIAO Shun-ping. Fast modeling method for aircraft wake vortices[J]. Journal of Aerospace Power, 2009, 24(1): 110-115.
Citation: ZHOU Bin, WANG Xue-song, WANG Guo-yu, XIAO Shun-ping. Fast modeling method for aircraft wake vortices[J]. Journal of Aerospace Power, 2009, 24(1): 110-115.

Fast modeling method for aircraft wake vortices

  • Received Date: 2008-05-07
  • Rev Recd Date: 2008-11-01
  • Publish Date: 2009-01-28
  • The mass,velocity and wing shape of the aircraft decide the intensity of wake vortex.The passive conservative model can better depict the movement evolution rule of water vapor and potential temperature in wake vortices.Since parametric studies are computationally expensive to the large amount of CPU time per simulation.In addition,it can't forecast the state distribution characteristic of any aircraft wake vortex in a real-time manner.Therefore,a fast modeling method for aircraft wake vortex was presented.It has solved the problems,such as the high request for computer time,long simulation time and lack of real time simulation.This can provide a theoretical basis to avoid former airplane's wake vortex and reduce the wake accident.

     

  • 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 (1778) PDF downloads(473) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return