Controlling transonic region formation in the supersonic flow by jet and near-wall energy supply

V. P. Zamuraev; A. P. Kalinina

doi:10.1063/1.5065298

Controlling transonic region formation in the supersonic flow by jet and near-wall energy supply

Результат исследования: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › научная › рецензирование

Аннотация

Numerical modeling based on the Reynolds-averaged Navier - Stokes equations has shown qualitatively the possibility to realize controlled energy release and to obtain a transonic mode with the help of a transverse control air jet, as in modeling based on the Euler equations. The determining role in ignition in the vortex and detachment regions formed near the jets of hydrogen or ethylene and air are played by shock waves.

Язык оригинала	английский
Название основной публикации	19th International Conference on the Methods of Aerophysical Research, ICMAR 2018
Редакторы	Fomin
Издатель	American Institute of Physics Inc.
Число страниц	6
Том	2027
ISBN (электронное издание)	9780735417472
DOI	https://doi.org/10.1063/1.5065298
Состояние	Опубликовано - 2 ноя 2018
Событие	19th International Conference on the Methods of Aerophysical Research, ICMAR 2018 - Akademgorodok, Novosibirsk, Российская Федерация Продолжительность: 13 авг 2018 → 19 авг 2018

Серия публикаций

Название	AIP Conference Proceedings
Издатель	AMER INST PHYSICS
Том	2027
ISSN (печатное издание)	0094-243X

Конференция

Конференция	19th International Conference on the Methods of Aerophysical Research, ICMAR 2018
Страна	Российская Федерация
Город	Akademgorodok, Novosibirsk
Период	13.08.2018 → 19.08.2018

Доступ к документу

10.1063/1.5065298

Link to publication in Scopus

Fingerprint Подробные сведения о темах исследования «Controlling transonic region formation in the supersonic flow by jet and near-wall energy supply». Вместе они формируют уникальный семантический отпечаток (fingerprint).

Цитировать

Zamuraev, V. P., & Kalinina, A. P. (2018). Controlling transonic region formation in the supersonic flow by jet and near-wall energy supply. В Fomin (Ред.), 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018 (Том 2027). [040024] (AIP Conference Proceedings; Том 2027). American Institute of Physics Inc.. https://doi.org/10.1063/1.5065298

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abstract = "Numerical modeling based on the Reynolds-averaged Navier - Stokes equations has shown qualitatively the possibility to realize controlled energy release and to obtain a transonic mode with the help of a transverse control air jet, as in modeling based on the Euler equations. The determining role in ignition in the vortex and detachment regions formed near the jets of hydrogen or ethylene and air are played by shock waves.",

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Zamuraev, VP & Kalinina, AP 2018, Controlling transonic region formation in the supersonic flow by jet and near-wall energy supply. в Fomin (ред.), 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. том. 2027, 040024, AIP Conference Proceedings, том. 2027, American Institute of Physics Inc., 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018, Akademgorodok, Novosibirsk, Российская Федерация, 13.08.2018. https://doi.org/10.1063/1.5065298

Controlling transonic region formation in the supersonic flow by jet and near-wall energy supply. / Zamuraev, V. P.; Kalinina, A. P.

19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. ред. / Fomin. Том 2027 American Institute of Physics Inc., 2018. 040024 (AIP Conference Proceedings; Том 2027).

Результат исследования: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › научная › рецензирование

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AU - Kalinina, A. P.

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N2 - Numerical modeling based on the Reynolds-averaged Navier - Stokes equations has shown qualitatively the possibility to realize controlled energy release and to obtain a transonic mode with the help of a transverse control air jet, as in modeling based on the Euler equations. The determining role in ignition in the vortex and detachment regions formed near the jets of hydrogen or ethylene and air are played by shock waves.

AB - Numerical modeling based on the Reynolds-averaged Navier - Stokes equations has shown qualitatively the possibility to realize controlled energy release and to obtain a transonic mode with the help of a transverse control air jet, as in modeling based on the Euler equations. The determining role in ignition in the vortex and detachment regions formed near the jets of hydrogen or ethylene and air are played by shock waves.

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