Chinese
您当前的位置：
首页 >
文章列表页 >
航空并联混合动力专用涡扇发动机快速设计方法
更新时间：2025-03-14

    • 航空并联混合动力专用涡扇发动机快速设计方法

    • Vol. 38, Issue 8, Pages: 1909-1925(2023)

    • DOI：10.13224/j.cnki.jasp.20230155    

      CLC：

    移动端阅览

  • 刘光璧, 王步宇, 王向阳, et al. 航空并联混合动力专用涡扇发动机快速设计方法[J]. 2023, 38(8): 1909-1925. DOI： 10.13224/j.cnki.jasp.20230155.

  •  
  •  
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

217

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 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
EXERGY ANALYSIS OF AEROENGINE AND ITS SIGNIFICANCE

Related Author

WANG Xiang-yu
YIN Chang-zhi
ZHANG Shao-ji
WANG Xi
KONG Xiang-xing
TANG Shi-jian
TONG Wan-jun
GUI Xing-min

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