您当前的位置:
首页 >
文章列表页 >
EXPERIMENTAL INVESTIGATION ON BLADE LOSS TRANSIENT RESPONSE OF ROTOR WITH FLEXIBLE DAMPED SUPPORT
更新时间:2026-07-07
    • EXPERIMENTAL INVESTIGATION ON BLADE LOSS TRANSIENT RESPONSE OF ROTOR WITH FLEXIBLE DAMPED SUPPORT

    • Vol. 7, Issue 2, (1992)
    • Published:1992

    移动端阅览

  • Li Qihan, Zhao Fuan, Zhang Shiping. EXPERIMENTAL INVESTIGATION ON BLADE LOSS TRANSIENT RESPONSE OF ROTOR WITH FLEXIBLE DAMPED SUPPORT[J]. 1992, 7(2). 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

488

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

Experimental verification on bidirectional sequential method to solve dynamical response caused by aerodynamic loads
Assessment research on damage degree of blade in aero-engine based on back-propagation artificial neural networks
Parametrical FE modeling of blade and design optimization of its gravity center eccentricity
Laser shock processing and aluminizing compound technology used on steel blade
Fracture Analysis of the 2nd Stage Compressor Blade in an Aeroengine

Related Author

ZHANG Da-yi
MA Yan-hong
HONG Jie
CHEN Lu-lu
QIAN Zheng-wen
CHENG Li
ZHAO Bing-bing
LI Ying-hong

Related Institution

School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
State Key Laboratory for Manufacturing Systems Engineering, School of Mechanical Engineering, Xi'an Jiaotong University
The Engineering Institute, Air Force Engineering University
Airforce First Research Institute
th Dept.Beijing University of Aeronautics and Astronautics
0