摘要
为了进一步提升水冲压发动机比冲性能,基于涡耗散燃烧模型,建立了高金属含量镁基推进剂水冲压发动机3D多相流掺混燃烧反应模型,获得了不同进水比例对补燃室内温度分布、组分变化以及发动机比冲等参数的影响规律,计算结果与地面试验基本吻合。研究结果表明,一次水燃比对高金属含量水冲压发动机的性能影响明显,随着一次水燃比的不断增大,发动机比冲呈现出先增后减的情况,存在某个最佳的一次水燃比,发动机比冲性能最高。
To improve specific impulse performance of a water ramjet, based on eddy-dissipation combust ion model, a 3D mult i-phase flow non-premixed combust ion react ion model was established for the water ramjet with high metal content magnesium-based propel lant. Further, the effects of water-to-fuel ratio on such parameters as temperature dis-tribution and variation of composit ion in afterburning chamber as well as specific impulse of the water ramjet were ob-tained, and the calculations are in good agreement with the experiment results. It is shown that the primary water-to-fuel ratio is more important to performance improvement of the water ramjet, and the specific impulse of the water ramjet firstly increases then decreases with the increase of primary water-to-fuel ratio, showing an optimum primary water-to-fuel ratio, at which the water ramjet gains the highest specific impulse.
出处
《水下无人系统学报》
2017年第2期52-56,63,共6页
Journal of Unmanned Undersea Systems
关键词
水冲压发动机
高金属含量推进剂
一次水燃比
比冲
water ramjet
high metal content propel lant
primary water-to-fuel ratio
specific impulse