您当前的位置:
首页 >
文章列表页 >
A Testing Instrument for the Box Against Pant of Some Turbojet Engine
更新时间:2026-07-07
    • A Testing Instrument for the Box Against Pant of Some Turbojet Engine

    • Vol. 18, Issue 3, (2003)
    • Published:2003

    移动端阅览

  • LI Wen-feng, WANG Yong-sheng, WU Chang-ying. A Testing Instrument for the Box Against Pant of Some Turbojet Engine[J]. 2003, 18(3). 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

368

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

Hardware in the Loop Simulation of Minitype Turbojet Engine Digital Control Regulator
Prediction method on equivalent thermal conductivity coefficient of plain braided C/SiC composites material based on finite element method
Aerodynamic characteristics of design Mach number of 5 two-dimensional inlet with mixed-compression under typical condition
Exhaust gas electrostatic monitoring and gas path fault feature for turbojet engine
Computation of effect of different nozzle parameters on internal performance of convergent-divergent axisymmetric nozzle

Related Author

CHENG Tao
LU Si-da
GAO Xi-guang
SONG Ying-dong
WENG Xiao-chai
GUO Rong-wei
ZHU Dan-dan
LIU Peng-peng

Related Institution

School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics
Department of Power and Propulsion, School of Engineering, Cranfield University, Bedfordshire MK4
State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics
Unit 94710, the Chinese People's Liberation Army
0