Chinese
您当前的位置：
首页 >
文章列表页 >
爬升阶段涡扇发动机核心流道吸鸟适航审定
更新时间：2025-03-14

    • 爬升阶段涡扇发动机核心流道吸鸟适航审定

    • Vol. 38, Issue 4, Pages: 1017-1024(2023)

    • DOI：10.13224/j.cnki.jasp.20210497    

      CLC：

    移动端阅览

  • 吴晶峰, 侯亮, 宋建宇, et al. 爬升阶段涡扇发动机核心流道吸鸟适航审定[J]. 2023, 38(4): 1017-1024. DOI： 10.13224/j.cnki.jasp.20210497.

  •  
  •  
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

151

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

Research and experiment on improved sectional combination control scheme for civil turbofan engine's startup process
Geared turbofan engine transient modeling research based on CMF method
Two-dimensional numerical simulation of a turbofan engine with air bleeding in compressor
Modeling Turbofan Engine Startup Based on Component Matching Principles
某民用飞机辅助动力装置进气受地面尾风影响研究

Related Author

KONG Xiang-xing
WANG Xi
ZHANG Shao-ji
YIN Chang-zhi
WANG Xiang-yu
TONG Wan-jun
TANG Shi-jian
JIN Dong-hai

Related Institution

Shenyang Engine Design and Research Institute, Aviation Industry Corporation of China
School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics
Academy of Aeronautic Propulsion Technology, Aviation Industry Corporation of China
Gas Turbine Establishment of China, Aviation Industry Corporation of China
School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
0