TY - JOUR
T1 - Fault simulation and analysis of the FLPRE test-bed fluid systems
AU - Gao, Fang
AU - Chen, Yang
AU - Zhang, Zhen Peng
AU - Chen, Feng
PY - 2006/4
Y1 - 2006/4
N2 - Starting from the transient pipe flow equation of one dimensional compressible fluid and using finite control volume method, the working process of the fluid piping system for liquid-propellant rocket engine testing was simulated. Through the comparison between calculated data and experimental data, the results illustrate that the method used in this paper describes preferably the working process of the fluid piping for the liquid-propellant rocket engine experiment system and can provide guidance for the design of experiment system, fault diagnosis, optimization and performance analysis of liquid-propellant rocket engine.
AB - Starting from the transient pipe flow equation of one dimensional compressible fluid and using finite control volume method, the working process of the fluid piping system for liquid-propellant rocket engine testing was simulated. Through the comparison between calculated data and experimental data, the results illustrate that the method used in this paper describes preferably the working process of the fluid piping for the liquid-propellant rocket engine experiment system and can provide guidance for the design of experiment system, fault diagnosis, optimization and performance analysis of liquid-propellant rocket engine.
KW - Aerospace propulsion system
KW - Compressible flow
KW - Finite control volume method
KW - Liquid-propellant rocket engine experimental system
KW - One dimensional flow
UR - https://www.scopus.com/pages/publications/33745760774
M3 - 文章
AN - SCOPUS:33745760774
SN - 1000-8055
VL - 21
SP - 417
EP - 420
JO - Hangkong Dongli Xuebao/Journal of Aerospace Power
JF - Hangkong Dongli Xuebao/Journal of Aerospace Power
IS - 2
ER -