Отправить статью по E-mail The Structure of a Hypersonic Air Flow near a Plane Surface at Various Intensities of Magnetogasdynamic Interaction
- Авторы: Fomichev V.1, Yadrenkin M.1
-
Учреждения:
- Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch
- Выпуск: Том 43, № 12 (2017)
- Страницы: 1063-1066
- Раздел: Article
- URL: https://journals.rcsi.science/1063-7850/article/view/206713
- DOI: https://doi.org/10.1134/S1063785017120057
- ID: 206713
Цитировать
Открытый доступ
Доступ предоставлен
Только для подписчиков
Аннотация
This Letter presents a systematization of the effects observed in experiments on the magnetogasdynamic interaction near the surface of a plate in a high-speed gas flow. Ranges of the hydromagnetic-interaction parameter determining various levels of influence on the shock-wave structure of the flow are established.
Об авторах
V. Fomichev
Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch
Email: yadrenkin@itam.nsc.ru
Россия, Novosibirsk, 630090
M. Yadrenkin
Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch
Автор, ответственный за переписку.
Email: yadrenkin@itam.nsc.ru
Россия, Novosibirsk, 630090
