Modular Simulationfor Tank Pressurization System of LRE Test-Bed

CHEN Yang; GAO Fang; ZHANG Zhen-peng; CHEN Feng

Chinese

您当前的位置：

首页 >

文章列表页 >

Modular Simulationfor Tank Pressurization System of LRE Test-Bed

更新时间：2026-07-07

- Modular Simulationfor Tank Pressurization System of LRE Test-Bed
- Vol. 20, Issue 2, (2005)
- 作者机构：
  
  1. 北京航空航天大学宇航学院,北京,100083
  2. 北京航天试验技术研究所,北京,100074
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2005
- 稿件说明：
移动端阅览
CHEN Yang, GAO Fang, ZHANG Zhen-peng, et al. Modular Simulationfor Tank Pressurization System of LRE Test-Bed[J]. 2005, 20(2).
DOI：

CHEN Yang, GAO Fang, ZHANG Zhen-peng, et al. Modular Simulationfor Tank Pressurization System of LRE Test-Bed[J]. 2005, 20(2). DOI：

摘要

采用一维理想气体流动的有限元状态变量模型

运用模块化建模与仿真方法和Fortran90语言进行了某液体火箭发动机试验台贮箱增压系统工作过程的仿真

获得了细致的管网状态参数分布曲线

为分析贮箱增压系统的工作过程及各组件的作用提供了数值依据。数学模型和模块化建模与仿真方法显示出较好的有效性和通用性。

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.

关键词

Keywords

references

Views

438

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Numerical Simulation of Heat Transfer and Fluid Flow in Cooling Channel of the Liquid Rocket Engine Thrust Chamber

General simulation on modularization of liquid rocket engine

Correlation analysis of blade vibration induced by inlet distortion and rotating stall

Preliminary study on hypersonic curved shock two-dimensional inlet

Investigation on hypersonic inward turning inlets with controlled pressure gradient

Related Author

WU Feng

WANG Qiu-wang

LUO Lai-qin

SUN Ji-guo

ZHANG Li-hui

LI Wei

DUAN Na

DU Jian-jian

Related Institution

Beijing Aviation Power Institute

State of Key Laboratory of Multiphase Flow in Power Engineering, Xi’an Jiaotong University

College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics

Department of Aerospace Engineering,School of Mechanical Engineering, Nanjing University of Science and Technology

Aviation Research Institute

AI问答

Postal code：100079
Tel：（010）53879206 Email：tmw@bjxintong.com.cn
Technical support is provided by Beijing Founder electronics co., LTD 京ICP备09082226号-64 京公网安备11010602201714号
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.

⁰