您当前的位置:
首页 >
文章列表页 >
Experimental Study of RCS Reduction for a Helicopter Inlet
更新时间:2026-07-07
    • Experimental Study of RCS Reduction for a Helicopter Inlet

    • Vol. 19, Issue 2, (2004)
    • Published:2004

    移动端阅览

  • HAN Dong, GUO Rong-wei, YI Hai-yun, et al. Experimental Study of RCS Reduction for a Helicopter Inlet[J]. 2004, 19(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

442

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

Research on RCS of airplane duct based on SBR method
An Experimental Investigation of Combining Stealth Device in Air Duct with Turbofan Engine
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
Analysis and evaluation on RCS characteristics of helicopter considering modulated effect of rotor

Related Author

WAN Shun-sheng
LUO Yi-jie
GUO Ron-wei
LI Wen-feng
CHENG Bang-qin
WANG Yong-sheng
LU Si-da
GAO Xi-guang

Related Institution

Research Institute of Pilotless Aircraft, NUAA
Northwestern Polytechnical University
The Air Force University of Engineering
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
0