Distributed parameter numerical simulation for the transients of cryogenic propellant tank pressurization system (II) Numerical model and simulation results of pressurization system

Yang Chen; Zhen Peng Zhang; Si Feng Yang; Qian Qu; Feng Chen; Zi Huan Zhu

Distributed parameter numerical simulation for the transients of cryogenic propellant tank pressurization system (II) Numerical model and simulation results of pressurization system

Yang Chen^*
, Zhen Peng Zhang
, Si Feng Yang
, Qian Qu
, Feng Chen
, Zi Huan Zhu

^*Corresponding author for this work

School of Astronautics

Beihang University
Beijing Institute of Aerospace Testing Technology

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

3 Scopus citations

Abstract

Based on the distributed parameter numerical model of cryogenic propellant tank, pressurization of a LO₂ tank pressurization system during engine firing was simulated by employing the liquid rocket engine test-bed modularization modeling and simulation software-gas system (LRETBMMSS-GS). The simulation results agree well with test data and experiential correlation prediction, which shows that the distributed parameter tank model is more accurate and comprehensive than lumped parameter model in describing flow and thermal stratification phenomena in cryogenic tank. Accordingly, the numerical system of finite volume model and corresponding simulation software have a wide applicability and good simulation precision, which are valuable and can be developed further in pipe system simulation field.

Original language	English
Pages (from-to)	329-335
Number of pages	7
Journal	Hangkong Dongli Xuebao/Journal of Aerospace Power
Volume	23
Issue number	2
State	Published - Feb 2008

Keywords

Aerospace propulsion system
Cryogenic tank pressurization system
Liquid propellant rocket engine
Modularization modeling
System dynamic simulation

Cite this

@article{2d9192b53eb84fe39346d1e0b855e05e,

title = "Distributed parameter numerical simulation for the transients of cryogenic propellant tank pressurization system (II) Numerical model and simulation results of pressurization system",

abstract = "Based on the distributed parameter numerical model of cryogenic propellant tank, pressurization of a LO2 tank pressurization system during engine firing was simulated by employing the liquid rocket engine test-bed modularization modeling and simulation software-gas system (LRETBMMSS-GS). The simulation results agree well with test data and experiential correlation prediction, which shows that the distributed parameter tank model is more accurate and comprehensive than lumped parameter model in describing flow and thermal stratification phenomena in cryogenic tank. Accordingly, the numerical system of finite volume model and corresponding simulation software have a wide applicability and good simulation precision, which are valuable and can be developed further in pipe system simulation field.",

keywords = "Aerospace propulsion system, Cryogenic tank pressurization system, Liquid propellant rocket engine, Modularization modeling, System dynamic simulation",

author = "Yang Chen and Zhang, \{Zhen Peng\} and Yang, \{Si Feng\} and Qian Qu and Feng Chen and Zhu, \{Zi Huan\}",

year = "2008",

month = feb,

language = "英语",

volume = "23",

pages = "329--335",

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

issn = "1000-8055",

publisher = "BUAA Press",

number = "2",

}

Distributed parameter numerical simulation for the transients of cryogenic propellant tank pressurization system (II) Numerical model and simulation results of pressurization system. / Chen, Yang; Zhang, Zhen Peng; Yang, Si Feng et al.
In: Hangkong Dongli Xuebao/Journal of Aerospace Power, Vol. 23, No. 2, 02.2008, p. 329-335.

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

TY - JOUR

T1 - Distributed parameter numerical simulation for the transients of cryogenic propellant tank pressurization system (II) Numerical model and simulation results of pressurization system

AU - Chen, Yang

AU - Zhang, Zhen Peng

AU - Yang, Si Feng

AU - Qu, Qian

AU - Chen, Feng

AU - Zhu, Zi Huan

PY - 2008/2

Y1 - 2008/2

N2 - Based on the distributed parameter numerical model of cryogenic propellant tank, pressurization of a LO2 tank pressurization system during engine firing was simulated by employing the liquid rocket engine test-bed modularization modeling and simulation software-gas system (LRETBMMSS-GS). The simulation results agree well with test data and experiential correlation prediction, which shows that the distributed parameter tank model is more accurate and comprehensive than lumped parameter model in describing flow and thermal stratification phenomena in cryogenic tank. Accordingly, the numerical system of finite volume model and corresponding simulation software have a wide applicability and good simulation precision, which are valuable and can be developed further in pipe system simulation field.

AB - Based on the distributed parameter numerical model of cryogenic propellant tank, pressurization of a LO2 tank pressurization system during engine firing was simulated by employing the liquid rocket engine test-bed modularization modeling and simulation software-gas system (LRETBMMSS-GS). The simulation results agree well with test data and experiential correlation prediction, which shows that the distributed parameter tank model is more accurate and comprehensive than lumped parameter model in describing flow and thermal stratification phenomena in cryogenic tank. Accordingly, the numerical system of finite volume model and corresponding simulation software have a wide applicability and good simulation precision, which are valuable and can be developed further in pipe system simulation field.

KW - Aerospace propulsion system

KW - Cryogenic tank pressurization system

KW - Liquid propellant rocket engine

KW - Modularization modeling

KW - System dynamic simulation

UR - https://www.scopus.com/pages/publications/40949097858

M3 - 文章

AN - SCOPUS:40949097858

SN - 1000-8055

VL - 23

SP - 329

EP - 335

JO - Hangkong Dongli Xuebao/Journal of Aerospace Power

JF - Hangkong Dongli Xuebao/Journal of Aerospace Power

IS - 2

ER -

Distributed parameter numerical simulation for the transients of cryogenic propellant tank pressurization system (II) Numerical model and simulation results of pressurization system

Abstract

Keywords

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