摘要
本文提出了一个高氯酸铵/硝胺推进剂的复合火焰燃烧模型,该模型不仅适合于任一配比的高氯酸铵/硝胺推进剂,而且也适合于高氯酸铵基推进剂和硝胺基推进剂的燃烧模拟.计算结果和文献值、实验值吻合较好.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.
A combustion model for composite flame of ammonium perchlora-te/nitramine propellant is presented in this paper.This model is available not only to ammonium perchlorate/nitramine propellant with any component ratio, but also to ammonium perchlorate propellant and nitramine propellant.The calculation result is in good accordance with that reported in many papers and with experimental data.It is shown that effects of many factors on combustion rate of propellant can be properly predicted by use of this model.
出处
《推进技术》
EI
CAS
CSCD
北大核心
1990年第4期63-70,共8页
Journal of Propulsion Technology
关键词
固体推进剂
燃烧模型
高氯酸铵
硝胺
Solid propellant, Combustion, Model, Ammonium perchlorate, Nitramine
