您当前的位置:
首页 >
文章列表页 >
Influence of different incidences on loss in turbine cascade
更新时间:2026-07-07
    • Influence of different incidences on loss in turbine cascade

    • Vol. 23, Issue 7, (2008)
    • Published:2008

    移动端阅览

  • SUN Da-wei, QIAO Wei-yang, XU Kai-fu, et al. Influence of different incidences on loss in turbine cascade[J]. 2008, 23(7). DOI:

  •  
  •  
icon
试读结束,您可以激活您的VIP账号继续阅读。
去激活 >
icon
试读结束,您可以通过登录账户,到个人中心,购买VIP会员阅读全文。
已是VIP会员?
去登录 >

0

Views

441

下载量

0

CSCD

Alert me when the article has been cited
提交
Tools
Download
Export Citation
Share
Add to favorites
Add to my album

Related Articles

Experiment of Reynolds number effects on subsonic compressor plane cascade
Investigation on the first passage shock loss with bump control inside a supersonic compressor cascade
Experiment and numerical simulation on characteristic of front variable area bypass injector
Numerical simulation of total pressure loss on vortex-reducer with bafflers
Effects of percent pitch on performance of high load tandem cascade

Related Author

Siyuan REN
Husheng MA
Xuechen LI
Youhai ZONG
Wei WEI
MA Yingqun
XU Qiangren
LIU Yongzhen

Related Institution

Aerospace Technology Institute,China Aerodynamics Research and Development Center
北京工业大学 机械工程与应用电子技术学院
先进航空发动机协同创新中心
北京航空航天大学 能源与动力工程学院 航空发动机气动热力国家级重点实验室
中国航空发动机集团有限公司 沈阳发动机研究所
0