Мақаланы E-mail арқылы жіберу Numerical simulation of some problems of recovery capsule aerodynamics
- Авторлар: Belotserkovskii O.M.1, Babakov A.V.1, Beloshitskiy A.V.2, Gaydaenko V.I.1, Dyadkin A.A.2
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Мекемелер:
- Institute of Computer-Aided Design (ICAD)
- Korolev Rocket and Space Public Corporation Energia (RSC Energia)
- Шығарылым: Том 8, № 5 (2016)
- Беттер: 568-576
- Бөлім: Article
- URL: https://journals.rcsi.science/2070-0482/article/view/201229
- DOI: https://doi.org/10.1134/S2070048216050057
- ID: 201229
Дәйексөз келтіру
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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.
Авторлар туралы
O. Belotserkovskii
Institute of Computer-Aided Design (ICAD)
Email: icad@icad.org.ru
Ресей, Moscow
A. Babakov
Institute of Computer-Aided Design (ICAD)
Хат алмасуға жауапты Автор.
Email: icad@icad.org.ru
Ресей, Moscow
A. Beloshitskiy
Korolev Rocket and Space Public Corporation Energia (RSC Energia)
Email: icad@icad.org.ru
Ресей, Moscow
V. Gaydaenko
Institute of Computer-Aided Design (ICAD)
Email: icad@icad.org.ru
Ресей, Moscow
A. Dyadkin
Korolev Rocket and Space Public Corporation Energia (RSC Energia)
Email: icad@icad.org.ru
Ресей, Moscow
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