Calculation of continuous spin detonation in a hydrogen-air mixture in an annular combustor Научная публикация
| Конференция |
19th International Conference on the Methods of Aerophysical Research 13-19 авг. 2018 , Новосибирск |
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| Журнал |
AIP Conference Proceedings
ISSN: 0094-243X |
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| Вых. Данные | Год: 2018, Том: 2027, Номер статьи : 030007, Страниц : 8 DOI: 10.1063/1.5065101 | ||
| Авторы |
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| Организации |
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Реферат:
A closed mathematical model of continuous spin detonation of a hydrogen-air mixture in a quasi-three-dimensional unsteady gas-dynamic formulation is developed. The model takes into account the reverse effect of oscillatory processes in the combustor on the injection system. Numerical simulations are performed for the geometric parameters of the flow-type annular combustor 306 mm in diameter used in experiments. The one-wave, two-wave, and three-wave regimes of continuous spin detonation for varied flow rates of the mixture are calculated, and the flow structure is analyzed.
Библиографическая ссылка:
Zhdan S.A.
, Rybnikov A.I.
, Simonov E.V.
Calculation of continuous spin detonation in a hydrogen-air mixture in an annular combustor
AIP Conference Proceedings. 2018. V.2027. 030007 :1-8. DOI: 10.1063/1.5065101 Scopus РИНЦ OpenAlex
Calculation of continuous spin detonation in a hydrogen-air mixture in an annular combustor
AIP Conference Proceedings. 2018. V.2027. 030007 :1-8. DOI: 10.1063/1.5065101 Scopus РИНЦ OpenAlex
Идентификаторы БД:
| Scopus: | 2-s2.0-85056324768 |
| РИНЦ: | 38622690 |
| OpenAlex: | W2898718531 |