Отправить статью по E-mail Numerical simulation of some problems of recovery capsule aerodynamics
- Авторы: Belotserkovskii O.M.1, Babakov A.V.1, Beloshitskiy A.V.2, Gaydaenko V.I.1, Dyadkin A.A.2
-
Учреждения:
- Institute of Computer-Aided Design (ICAD)
- Korolev Rocket and Space Public Corporation Energia (RSC Energia)
- Выпуск: Том 8, № 5 (2016)
- Страницы: 568-576
- Раздел: Article
- URL: https://journals.rcsi.science/2070-0482/article/view/201229
- DOI: https://doi.org/10.1134/S2070048216050057
- ID: 201229
Цитировать
Открытый доступ
Доступ предоставлен
Только для подписчиков
Аннотация
This paper presents the numerical simulation of the circumfluence of a recovery apparatus with brake engines and a detachable heat protection shield carried out by the use of the conservative numerical method of cluster architecture. The simulation results of the action of reactive jets of brake engines on the landing surface and the recovery apparatus, as well as the basic aerodynamic characteristics, are considered.
Об авторах
O. Belotserkovskii
Institute of Computer-Aided Design (ICAD)
Email: icad@icad.org.ru
Россия, Moscow
A. Babakov
Institute of Computer-Aided Design (ICAD)
Автор, ответственный за переписку.
Email: icad@icad.org.ru
Россия, Moscow
A. Beloshitskiy
Korolev Rocket and Space Public Corporation Energia (RSC Energia)
Email: icad@icad.org.ru
Россия, Moscow
V. Gaydaenko
Institute of Computer-Aided Design (ICAD)
Email: icad@icad.org.ru
Россия, Moscow
A. Dyadkin
Korolev Rocket and Space Public Corporation Energia (RSC Energia)
Email: icad@icad.org.ru
Россия, Moscow
Дополнительные файлы
