摘要
利用建立的以准一维气相反应流为基础的推进剂稳态燃烧模型,计算了推进剂配方组成对催化燃烧性能的影响,从化学结构的角度分析了平台燃烧的影响因素,由此解释了平台燃烧全过程的化学本质和推进剂燃速压强指数的化学本质,提出了平台推进剂配方和燃速优化设计的原则,为燃速和燃速压强指数的调节提供了理论依据,其结论与国内外实践结果相一致。
The influence of main chemical components of double base plateau propellant on its combustion property was investigated by theoretical computation,which was based on one-dimensional gaseous phase reaction flow model. The computation results were not only in agreement with domestic and international practical experience, but also could explain the chemical essence of propellant burning process. So through optimizing propellant formula, the results might be used to adjust the burning rate and pressure exponent of double base plateau propellants.
出处
《火炸药学报》
EI
CAS
CSCD
2004年第4期55-58,共4页
Chinese Journal of Explosives & Propellants
基金
国防基础研究项目(DJ00014)
