Мақаланы E-mail арқылы жіберу Application of the DRGEP and Engagement Methods to Reduce the Reaction Mechanisms for Calculation of Chemically Non-Equilibrium Flows in Aircraft Engine Nozzles
- Авторлар: Krioukov V.1, Abdullin A.1, Nikandrova M.1, Safiullin I.1
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Мекемелер:
- Tupolev Kazan National Research Technical University
- Шығарылым: Том 61, № 4 (2018)
- Беттер: 682-686
- Бөлім: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230782
- DOI: https://doi.org/10.3103/S1068799818040281
- ID: 230782
Дәйексөз келтіру
Ашық рұқсат
Рұқсат берілді
Тек жазылушылар үшін
Аннотация
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.
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Авторлар туралы
V. Krioukov
Tupolev Kazan National Research Technical University
Email: kazan711@yandex.ru
Ресей, ul. Karla Marksa 10, Kazan, 420111
A. Abdullin
Tupolev Kazan National Research Technical University
Email: kazan711@yandex.ru
Ресей, ul. Karla Marksa 10, Kazan, 420111
M. Nikandrova
Tupolev Kazan National Research Technical University
Email: kazan711@yandex.ru
Ресей, ul. Karla Marksa 10, Kazan, 420111
I. Safiullin
Tupolev Kazan National Research Technical University
Хат алмасуға жауапты Автор.
Email: kazan711@yandex.ru
Ресей, ul. Karla Marksa 10, Kazan, 420111
