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Numerical Modeling of Subsonic Axisymmetric Reacting Gas Flows Научная публикация

Конференция 6th All-Russian Conference on Thermophysics and Physical Hydrodynamics
22-29 авг. 2021 , Севастополь
Журнал Journal of Physics: Conference Series
ISSN: 1742-6588 , E-ISSN: 1742-6596
Вых. Данные Год: 2021, Том: 2057, Номер: 1, Номер статьи : 012071, Страниц : 7 DOI: 10.1088/1742-6596/2057/1/012071
Ключевые слова Mach number; Navier Stokes equations; Pyrolysis
Авторы Peskova E.E. 1,2
Организации
1 Ogarev Mordovia State University, 68 Bolshevistskaya Street, Saransk, 430005, Russia
2 Boreskov Institute of Catalysis SB RAS, 5 Lavrentyev Avenue, Novosibirsk, 630090, Russia

Информация о финансировании (1)

1 Российский научный фонд 21-19-00429

Реферат: A numerical algorithm is developed and implemented for modelling axisymmetric subsonic reacting gas flows based on a previously created program for plane flows. The system of Navier-Stokes equations in the low Mach number limit is used as a mathematical model. Calculations of ethane pyrolysis for axisymmetric and plane flow of mixture at heat supply from the reactor's walls are carried out. Through the interplay of the developed code and the code for plane flows it becomes possible to identify the geometric factor role at the presence of a large number of nonlinear physicochemical processes. We found that diffusion of synthesized molecular hydrogen mainly influences heat supply from the reactor's walls to gas and pyrolysis products distribution along its length.
Библиографическая ссылка: Peskova E.E.
Numerical Modeling of Subsonic Axisymmetric Reacting Gas Flows
Journal of Physics: Conference Series. 2021. V.2057. N1. 012071 :1-7. DOI: 10.1088/1742-6596/2057/1/012071 Scopus РИНЦ OpenAlex
Даты:
Опубликована в печати: 8 нояб. 2021 г.
Опубликована online: 8 нояб. 2021 г.
Идентификаторы БД:
Scopus: 2-s2.0-85119623403
РИНЦ: 47533449
OpenAlex: W3212766611
Цитирование в БД:
БД Цитирований
Scopus 7
РИНЦ 12
OpenAlex 8
Альметрики: