Application of the DRGEP and Engagement Methods to Reduce the Reaction Mechanisms for Calculation of Chemically Non-Equilibrium Flows in Aircraft Engine Nozzles
- 作者: Krioukov V.1, Abdullin A.1, Nikandrova M.1, Safiullin I.1
-
隶属关系:
- Tupolev Kazan National Research Technical University
- 期: 卷 61, 编号 4 (2018)
- 页面: 682-686
- 栏目: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230782
- DOI: https://doi.org/10.3103/S1068799818040281
- ID: 230782
如何引用文章
详细
The procedure of the reaction mechanism reduction including the DRGEP and engagement methods is considered and applied to the problem of calculating the non-equilibrium flows of propellant combustion products (kerosene + oxygen) in nozzles.
作者简介
V. Krioukov
Tupolev Kazan National Research Technical University
Email: kazan711@yandex.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111
A. Abdullin
Tupolev Kazan National Research Technical University
Email: kazan711@yandex.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111
M. Nikandrova
Tupolev Kazan National Research Technical University
Email: kazan711@yandex.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111
I. Safiullin
Tupolev Kazan National Research Technical University
编辑信件的主要联系方式.
Email: kazan711@yandex.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111