Simulation of the processes of spraying and combustion of kerosene and liquid oxygen in the chamber of a liquid-propellant rocket engine

Autor: M. N. Senchev, I. A. Zubrilin, A. A. Yurtaev, М. A. Benedyuk, Yu. V. Komisar

Publikováno v: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 23, Iss 4, Pp 167-179 (2024)

The paper presents the results of simulation of spray and combustion processes in the liquid-propellant rocket engine chamber using the z77 reduced kinetic mechanism of chemical reactions and a hybrid method for determining spray parameters of a swir

Externí odkaz: https://doaj.org/article/760f5740eca24716a40630e1c0286377