Chinese
您当前的位置：
首页 >
文章列表页 >
DSI两级斜切后掠唇口对飞机外流的影响
更新时间：2025-03-14

    • DSI两级斜切后掠唇口对飞机外流的影响

    • Vol. 38, Issue 8, Pages: 1926-1936(2023)

    • DOI：10.13224/j.cnki.jasp.20210653    

      CLC：

    移动端阅览

  • 苏嘉殷, 李博, 童佳慧, et al. DSI两级斜切后掠唇口对飞机外流的影响[J]. 2023, 38(8): 1926-1936. DOI： 10.13224/j.cnki.jasp.20210653.

  •  
  •  
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

307

下载量

1

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

Correlation analysis of blade vibration induced by inlet distortion and rotating stall
Preliminary study on hypersonic curved shock two-dimensional inlet
Investigation on hypersonic inward turning inlets with controlled pressure gradient
Design and performance investigation of sidewall compression scramjet inlets operating from Mach 4 to Mach 7
Performance simulation analysis for a hydrogen-rich / oxygen-rich shear coaxial gas-gas injector

Related Author

FANG Li-cheng
LI Shun-ming
DU Jian-jian
XIANG You-zhi
NAN Xiang-jun
WANG Lei
ZHANG Kun-yuan
ZHANG Lin

Related Institution

College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
Department of Aerospace Engineering,School of Mechanical Engineering, Nanjing University of Science and Technology
School of Astronautics, Beijing University of Aeronautics and Astronautics
Beijing Institute of Aerospace Testing Technology
西北工业大学 动力与能源学院
0