Liquid propellantcombustion 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。
2
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。
3
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.