Chinese
您当前的位置：
首页 >
文章列表页 >
Unique design method of subsonic inlet with complex cross-sectional shape
更新时间：2026-07-07

    • Unique design method of subsonic inlet with complex cross-sectional shape

    • Vol. 24, Issue 6, (2009)

    • Published：2009

    移动端阅览

  • ZHOU Hui-chen, TAN Hui-jun, LI Xiang-ping. Unique design method of subsonic inlet with complex cross-sectional shape[J]. 2009, 24(6). 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

421

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

Design method and its misaligned contact characteristic of aviation crowned spline
Design and verification of engine air particle separator for vehicle gas turbine engine
A design method for high efficiency propeller
Modified axisymmetric basic flowfield for hypersonic inward turning inlet
Design of hypersonic inward turning inlets base on concept of controllable Mach number distribution

Related Author

Mengru WANG
Zhifei FENG
Yongquan WANG
Mei GUO
Changqing SU
Guang ZHAO
WANG Chang-rong
XIE Mai-xiang

Related Institution

Shenyang Engine Research Institute，Aero Engine Corporation of China
Key Laboratory for Power Transmission Technology of Aero⁃Engine，Aero Engine Corporation of China
School of Energy and Power Engineering，Dalian University of Technology
Unit 66176, the Chinese People's Liberation Army
Hunan Aviation Powerplant Research Institute, Aero Engine(Group) Corporation of China
0