Numerical simulation of some problems of recovery capsule aerodynamics

O. M. Belotserkovskii; A. V. Babakov; A. V. Beloshitskiy; V. I. Gaydaenko; A. A. Dyadkin

doi:10.1134/S2070048216050057

Numerical simulation of some problems of recovery capsule aerodynamics

作者: Belotserkovskii O.M.¹, Babakov A.V.¹, Beloshitskiy A.V.², Gaydaenko V.I.¹, Dyadkin A.A.²
隶属关系:
1. Institute of Computer-Aided Design (ICAD)
2. Korolev Rocket and Space Public Corporation Energia (RSC Energia)
期: 卷 8, 编号 5 (2016)
页面: 568-576
栏目: Article
URL: https://journals.rcsi.science/2070-0482/article/view/201229
DOI: https://doi.org/10.1134/S2070048216050057
ID: 201229

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详细

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.