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Three-dimensional numerical modeling of a rocket engine with solid fuel
Acta Astronautica ( IF 3.5 ) Pub Date : 2021-01-22 , DOI: 10.1016/j.actaastro.2021.01.028
A.G. Kushnirenko , L.I. Stamov , V.V. Tyurenkova , M.N. Smirnova , E.V. Mikhalchenko

This paper presents three-dimensional numerical modeling of the processes occurring in the combustion chamber of a hybrid engine. Numerical simulation using verified author's code was carried out. The distributions of temperature, pressure, longitudinal and transverse velocities were analyzed. The characteristic features of the regression rate were studied. The influence of the reaction kinetics on the nature of the processes in the combustion chamber was determined. The obtained numerical results were compared with experimental data.



中文翻译:

固体燃料火箭发动机的三维数值模拟

本文提出了混合动力发动机燃烧室中发生的过程的三维数值模型。使用验证过的作者代码进行了数值模拟。分析了温度,压力,纵向和横向速度的分布。研究了回归率的特征。确定了反应动力学对燃烧室内过程性质的影响。将获得的数值结果与实验数据进行比较。

更新日期:2021-01-22
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