摘要
建立了一个描述微孔推进剂燃烧的模型，并得到了推进剂稳定燃烧时的控制方程组。计算了燃烧室压力与初始空隙率等对燃烧过程的影响，分析了稳定燃烧时应满足的一些基本条件，结果与实验值相一致。
The combustion model of micro-void propellant is presented in this paper. The control equations for stable burning of propellant are set up. The effects of both chamber pressure and initial Porosity on combustion process are calculated, and some basic conditions for stable burning are analysed.
出处
《推进技术》
EI
CAS
CSCD
北大核心
1997年第6期75-78,共4页
Journal of Propulsion Technology
关键词
高燃速
推进剂
微孔率
稳定燃烧
燃速
High burning rate propellant, Microporosity, Combustion physics, Stable combustion
