Fault simulation and analysis of the FLPRE test-bed fluid systems

Fang Gao; Yang Chen; Zhen Peng Zhang; Feng Chen

Fault simulation and analysis of the FLPRE test-bed fluid systems

Fang Gao^*
, Yang Chen
, Zhen Peng Zhang
, Feng Chen

^*Corresponding author for this work

School of Astronautics

Beihang University
Beijing Institute of Aerospace Testing Technology

Research output: Contribution to journal › Article › peer-review

5 Scopus citations

Abstract

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.

Original language	English
Pages (from-to)	417-420
Number of pages	4
Journal	Hangkong Dongli Xuebao/Journal of Aerospace Power
Volume	21
Issue number	2
State	Published - Apr 2006

Keywords

Aerospace propulsion system
Compressible flow
Finite control volume method
Liquid-propellant rocket engine experimental system
One dimensional flow

Cite this

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title = "Fault simulation and analysis of the FLPRE test-bed fluid systems",

abstract = "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.",

keywords = "Aerospace propulsion system, Compressible flow, Finite control volume method, Liquid-propellant rocket engine experimental system, One dimensional flow",

author = "Fang Gao and Yang Chen and Zhang, \{Zhen Peng\} and Feng Chen",

year = "2006",

month = apr,

language = "英语",

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journal = "Hangkong Dongli Xuebao/Journal of Aerospace Power",

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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 -

Fault simulation and analysis of the FLPRE test-bed fluid systems

Abstract

Keywords

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