您当前的位置:
首页 >
文章列表页 >
Investigation of aero-engine thrust performance deterioration rules based on fractal theory
更新时间:2026-07-07
    • Investigation of aero-engine thrust performance deterioration rules based on fractal theory

    • Vol. 25, Issue 10, (2010)
    • Published:2010

    移动端阅览

  • YU Jin-lu, HE Li-ming, SUN Dong, et al. Investigation of aero-engine thrust performance deterioration rules based on fractal theory[J]. 2010, 25(10). 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

503

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

Method of loading calibration for actual measurement ofaero-engine thrust based on installation structure
Thrust Determination of an Engine with Laval Nozzle with Large Simulated Ambient Pressure Deviation
Mechanism of internal/external flow coupling effects on the performance of distributed ducted fan
Development path and future trend of carrier-based advanced trainer engine
Thermal protection effectiveness of thermal barrier coatings in turbine blade applications

Related Author

HUANG Yi-feng
LIU Ke-ge
YAN Chu-liang
HAN Xiao-jin
LIU Zhi-you
HOU Min-jie
GONG Xiao-qi
GONG Tianyu

Related Institution

Beijing Aircraft Strength Institute, China National Machinery Industry Corporation
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
China Gas Turbine Establishment
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics
北京航空航天大学 能源与动力工程学院
0