Modular simulation for tank pressurization system of LRE test-bed

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

Modular simulation for tank pressurization system of LRE test-bed

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

^*此作品的通讯作者

宇航学院

Beihang University
Aerospace Research Institute of Special Materials & Technology

科研成果: 期刊稿件 › 文章 › 同行评审

5 引用（Scopus）

摘要

Using the finite element state-variable model for one-dimensional ideal gas flow, a modularized simulation model was established, and then the working process was calculated for the tank pressurization system of LRE test-bed. Detailed distribution curves of state parameters for the pipe net were obtained, which could be used to analyze the working process of the system and the function of every component. The mathematical model and the method of modularized modeling and simulation were validated to be effective and versatile.

源语言	英语
页（从-至）	339-344
页数	6
期刊	Hangkong Dongli Xuebao/Journal of Aerospace Power
卷	20
期	2
出版状态	已出版 - 4月 2005

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引用此

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title = "Modular simulation for tank pressurization system of LRE test-bed",

abstract = "Using the finite element state-variable model for one-dimensional ideal gas flow, a modularized simulation model was established, and then the working process was calculated for the tank pressurization system of LRE test-bed. Detailed distribution curves of state parameters for the pipe net were obtained, which could be used to analyze the working process of the system and the function of every component. The mathematical model and the method of modularized modeling and simulation were validated to be effective and versatile.",

keywords = "Aerospace propulsion system, Liquid propellant rocket engine, Modularized model, Numerical simulation, Tank pressurization system of LRE test-bed",

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

year = "2005",

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AU - Chen, Yang

AU - Gao, Fang

AU - Zhang, Zhen Peng

AU - Chen, Feng

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Y1 - 2005/4

N2 - Using the finite element state-variable model for one-dimensional ideal gas flow, a modularized simulation model was established, and then the working process was calculated for the tank pressurization system of LRE test-bed. Detailed distribution curves of state parameters for the pipe net were obtained, which could be used to analyze the working process of the system and the function of every component. The mathematical model and the method of modularized modeling and simulation were validated to be effective and versatile.

AB - Using the finite element state-variable model for one-dimensional ideal gas flow, a modularized simulation model was established, and then the working process was calculated for the tank pressurization system of LRE test-bed. Detailed distribution curves of state parameters for the pipe net were obtained, which could be used to analyze the working process of the system and the function of every component. The mathematical model and the method of modularized modeling and simulation were validated to be effective and versatile.

KW - Aerospace propulsion system

KW - Liquid propellant rocket engine

KW - Modularized model

KW - Numerical simulation

KW - Tank pressurization system of LRE test-bed

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AN - SCOPUS:19644365671

SN - 1000-8055

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JO - Hangkong Dongli Xuebao/Journal of Aerospace Power

JF - Hangkong Dongli Xuebao/Journal of Aerospace Power

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ER -

Modular simulation for tank pressurization system of LRE test-bed

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