摘要
过氧化氢是现代液体火箭推进剂的重要发展方向。针对过氧化氢发动机试验中出现的低频振荡现象,通过建立发动机系统模型,对这种振荡现象进行了仿真和分析,成功实现了发动机的稳定工作。本文将有利于结合仿真和试验,促进过氧化氢发动机的研制。
Hydrogen peroxide is one of the most important directions of liquid rocket propellant. Considering the low-frequency oscillation phenomenon which occurs in experiment of hydrogen peroxide engine, simulation and analysis of the phenomenon based on the propulsion system models were made, and a stable engine was achieved. The current research is helpful for linking system simulation to experiment in hydrogen peroxide engine development.
出处
《国防科技大学学报》
EI
CAS
CSCD
北大核心
2007年第5期23-25,53,共4页
Journal of National University of Defense Technology
基金
国家部委基金资助项目
关键词
过氧化氢发动机
低频
振荡
仿真
试验
hydrogen peroxide engine
low frequency
oscillation
simulation
experiment
