Analysis of Gas Dynamics and Combustion in a Small Reverse-Flow Combustion Chamber
- Авторы: Yousef W.M.1, Sychenkov V.A.1, Davydov N.V.1, Aleksandrov Y.B.1
-
Учреждения:
- Tupolev Kazan National Research Technical University
- Выпуск: Том 61, № 3 (2018)
- Страницы: 460-466
- Раздел: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230646
- DOI: https://doi.org/10.3103/S1068799818030212
- ID: 230646
Цитировать
Аннотация
This paper presents the calculation results by a reactor model, numerical simulation in ANSYS Fluent CFD software, and the results of studying the flow structure and the burn-up fuel in the reverse-flow combustion chamber. These results are intended to create a methodology for further refinement of a combustion process in a combustion chamber.
Об авторах
W. Yousef
Tupolev Kazan National Research Technical University
Автор, ответственный за переписку.
Email: wyasen@mail.ru
Россия, ul. Karla Marksa 10, Kazan, 420111
V. Sychenkov
Tupolev Kazan National Research Technical University
Email: wyasen@mail.ru
Россия, ul. Karla Marksa 10, Kazan, 420111
N. Davydov
Tupolev Kazan National Research Technical University
Email: wyasen@mail.ru
Россия, ul. Karla Marksa 10, Kazan, 420111
Yu. Aleksandrov
Tupolev Kazan National Research Technical University
Email: wyasen@mail.ru
Россия, ul. Karla Marksa 10, Kazan, 420111
Дополнительные файлы
