Volume 25 Issue 7
Jul.  2010
Turn off MathJax
Article Contents
TANG Hong-fei, HUANG Hong-yan, WANG Zhen-feng, HAN Wan-jin. Investigation on root blade profile of a large meridional expansion turbine[J]. Journal of Aerospace Power, 2010, 25(7): 1602-1608.
Citation: TANG Hong-fei, HUANG Hong-yan, WANG Zhen-feng, HAN Wan-jin. Investigation on root blade profile of a large meridional expansion turbine[J]. Journal of Aerospace Power, 2010, 25(7): 1602-1608.

Investigation on root blade profile of a large meridional expansion turbine

  • Received Date: 2009-05-20
  • Rev Recd Date: 2010-04-04
  • Publish Date: 2010-07-28
  • The investigation focused on the design characteristic of root blade profile in the large meridional expansion turbines.And,the effect of root blade profile optimized design on the flow separation at vane inlet and radial pressure distribution at vane outlet was also studied.With the commercial numerical simulation solver,NUMECA,optimized design of root blade profile was applied into a large meridional expansion turbine.Then full three-dimensional numerical simulations on the original and optimized profiles were carried out.The numerical results show that,wider profile and convergent-divergent root profile would adjust radial distribution of massflow at inlet,weaken or even eliminate incoming flow separation at the upper endwall,hence controlling the flow loss in shroud;meanwhile,such profiles could improve mach number distribution and radial distribution of pressure at outlet,weaken or even eliminate radial flow of S1 section separation in the suction side at exit,thereby reducing flow loss in 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 (1668) PDF downloads(502) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return