您当前的位置:
首页 >
文章列表页 >
Study of the instability characteristic in the boundary layer of a hypersonic blunt cone at low angle of attack
更新时间:2026-07-07
    • Study of the instability characteristic in the boundary layer of a hypersonic blunt cone at low angle of attack

    • Vol. 26, Issue 12, (2011)
    • Published:2011

    移动端阅览

  • YUAN Xiang-jiang, LI Guo-liang, LIU Zhi-yong, et al. Study of the instability characteristic in the boundary layer of a hypersonic blunt cone at low angle of attack[J]. 2011, 26(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

11

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

Impact of local cavities on evolution of the second-mode disturbances in hypersonic boundary layers
Effect of mass ejection on boundary layers stability
Generation conditions of streamwise vortex in supersonic flat⁃plate boundary layer
Flow and heat transfer characteristics of round⁃hole film cooling with crater
Fluid-thermal coupling on drag and heat reduction induced by spike and jet in hypersonic flow field

Related Author

LI Chuang
DONG Ming
LI Jin
SU Wei
HUANG Zhangfeng
Qian WANG
Zhangfeng HUANG
Hai WANG

Related Institution

Department of Mechanics,School of Mechanical Engineering,Tianjin University
Department of Thermal Science and Energy Engineering,University of Science and Technology of China
Shenyang Engine Research Institute,Aero Engine Corporation of China
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
Aero Engine Academy of China,Aero Engine Corporation of China
0