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液体火箭发动机动态特性仿真技术研究进展

李元启 刘红军 徐浩海 陈宏玉

火箭推进2017,Vol.43Issue(5):1-6,6.
火箭推进2017,Vol.43Issue(5):1-6,6.

液体火箭发动机动态特性仿真技术研究进展

Research progress on numerical simulation technology of liquid rocket engine dynamic characteristics

李元启 1刘红军 1徐浩海 1陈宏玉1

作者信息

  • 1. 液体火箭发动机技术重点实验室, 陕西 西安710100
  • 折叠

摘要

Abstract

The numerical simulation technology is one of the important methods to investigate the dynamic characteristics of liquid rocket engine ( LRE) . A review on numerical simulation technology of LRE dynamic characteristics is done in this paper. Development of the technology can be divided in-to three stages:special simulation program phase, general simulation software phase and multidisci-plinary collaborate simulation phase. Key work of each developing phase is summarized and evalua-ted. Main characteristics of the simulation technology in each stage are analyzed. Based on summary of the research progress, the development direction of the future numerical simulation technology of LRE dynamic characteristics is proposed.

关键词

研究进展/液体火箭发动机/动态特性/仿真技术

Key words

research progress/liquid rocket engine/dynamic characteristic/simulation technology

分类

航空航天

引用本文复制引用

李元启,刘红军,徐浩海,陈宏玉..液体火箭发动机动态特性仿真技术研究进展[J].火箭推进,2017,43(5):1-6,6.

基金项目

装备预研基金项目 (61427040401162704007) (61427040401162704007)

火箭推进

OACSTPCD

1672-9374

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