您当前的位置:
首页 >
文章列表页 >
Experimental study on bird damage of vortex vane in the particle separator
更新时间:2026-07-07
    • Experimental study on bird damage of vortex vane in the particle separator

    • Vol. 22, Issue 12, (2007)
    • Published:2007

    移动端阅览

  • GUAN Yu-pu, ZHANG Zai-kun, ZHAO Zhen-hua, et al. Experimental study on bird damage of vortex vane in the particle separator[J]. 2007, 22(12). 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

483

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

Loading method on fatigue test of propeller hub
Prediction method on equivalent thermal conductivity coefficient of plain braided C/SiC composites material based on finite element method
Aerodynamic characteristics of design Mach number of 5 two-dimensional inlet with mixed-compression under typical condition
Optimization design of vaneless inlet particle separator based on hybrid algorithm
Integrated flow field characteristics of helicopter/particle separator: Part 2 influence of rotor disk load

Related Author

YANG Lei
SU Jun
WANG Hong-bin
LU Si-da
GAO Xi-guang
SONG Ying-dong
WENG Xiao-chai
GUO Rong-wei

Related Institution

Shenyang Engine Design and Research Institute, Aviation Industry Corporation of China
Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics
Department of Power and Propulsion, School of Engineering, Cranfield University, Bedfordshire MK4
State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics
Unit 94710, the Chinese People's Liberation Army
0