solid propellant combustion 固体推进剂燃烧
propellant combustion property 推进剂燃烧性能
propellant combustion mechanism 推进剂燃烧机理
solid propellant combustion rate 固体推进剂燃速
solid propellant combustion model 固体推进剂燃烧模型
double-base propellant combustion 双基推进剂燃烧
propellant t combustion 推进剂燃烧
Liquid propellant combustion processes are quite complicated and defy precise analytical description.
液体推进剂燃烧过程是相当复杂的，很难对其进行严谨的分析描述。
It is shown that effects of many factors on combustion rate of propellant can be properly predicted by use of this model.
结果表明，该模型能正确地预测许多因素对推进剂燃烧速率的影响。
In this paper, a new parameter named slurry combustion effect was induced for applying solid propellant BDP model for prediction of pasty propellant and slurry propellant steady combustion behavior.
在固体推进剂bdp燃烧模型基础上，引入膏体推进剂燃烧热效应这一新参数将模型推广于膏体推进剂和固体推进剂药浆燃烧研究。
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