您当前的位置:
首页 >
文章列表页 >
Investigation on the aerodynamic adjustment between inlet guide-vane,stator,and operating speed of three-stage axial compressor
更新时间:2026-07-07
    • Investigation on the aerodynamic adjustment between inlet guide-vane,stator,and operating speed of three-stage axial compressor

    • Vol. 24, Issue 5, (2009)
    • Published:2009

    移动端阅览

  • GONG Wei, ZHANG Hong-wu, NIE Chao-qun. Investigation on the aerodynamic adjustment between inlet guide-vane,stator,and operating speed of three-stage axial compressor[J]. 2009, 24(5). 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

466

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

Numerical investigation of bleeding effect on performance of multistage axial compressor
Quasi-steady flow model of slot-type casing treatments Ⅰ: modeling method and validation
Plenum chamber casing treatment——numerical research of internal flow and mechanism of stall margin improvements
Research of influence of stator blade suction on the stall margin of axial compressor
Effects of Reynolds Number in a Small Multistage Axial Flow Compressor

Related Author

YAO Ding-fu
CHENG Jin-xin
CHEN Jiang
DU Gang
NING Fang-fei
FAN Lin
JIANG Yong-song
WANG Yong-mei

Related Institution

School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics
School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
Shenyang Aero Engine Research Institute
Nanjing University of Aeronautics &Astronautics
Zhuzhou Aviation Power-Plant Research Institute
0