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Numerical modelling of detonation combustion of hydrogen-air mixture in a supersonic annular chamber Научная публикация

Конференция 3RD ALL-RUSSIAN SCIENTIFIC CONFERENCE THERMOPHYSICS AND PHYSICAL HYDRODYNAMICS WITH THE SCHOOL FOR YOUNG SCIENTISTS, TPH 2018 3RD ALL-RUSSIAN SCIENTIFIC CONFERENCE THERMOPHYSICS AND PHYSICAL HYDRODYNAMICS WITH THE SCHOOL FOR YOUNG SCIENTISTS
10-16 сент. 2018 , Ялта, Крым
Журнал Journal of Physics: Conference Series
ISSN: 1742-6588
Вых. Данные Год: 2018, Том: 1128, Номер статьи : 012078, Страниц : 6 DOI: 10.1088/1742-6596/1128/1/012078
Авторы Trotsyuk A V 1
Организации
1 Lavrentyev Institute of Hydrodynamics, Siberian Branch of the Russian Academy of Science

Информация о финансировании (1)

1 Министерство науки и высшего образования Российской Федерации FWGG-2021-0003

Реферат: The flow structure for various detonation regimes is numerically studied in a new flow-type supersonic annular detonation combustor. In the combustor with a new design, detonation burning of the reacting mixture is organized by using a compression body, shaped as a continuous monofilar helix with a constant pitch angle. Numerical simulations are performed for a supersonic flow of a stoichiometric hydrogen-air mixture with Mach number M0=3 at the combustor entrance. A mathematical model of the reacting flow in the combustor is developed in a two-dimensional unsteady formulation. The flow dynamics at the beginning of combustor operation and the structure of the steady flow in the combustor are numerically studied. Simulations are performed for various helix angles and combustor sizes. A bifurcation of the steady flow structures with respect to the initial conditions of combustor operations is detected for some combinations of the geometric parameters of the combustor.
Библиографическая ссылка: Trotsyuk A.V.
Numerical modelling of detonation combustion of hydrogen-air mixture in a supersonic annular chamber
Journal of Physics: Conference Series. 2018. V.1128. 012078 :1-6. DOI: 10.1088/1742-6596/1128/1/012078 Scopus РИНЦ OpenAlex
Идентификаторы БД:
Scopus: 2-s2.0-85058617950
РИНЦ: 38637133
OpenAlex: W2904571640
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OpenAlex 1
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