Numerical simulation of some problems of recovery capsule aerodynamics

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 eng...

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Veröffentlicht in:Mathematical models and computer simulations 2016-09, Vol.8 (5), p.568-576
Hauptverfasser: Belotserkovskii, O. M., Babakov, A. V., Beloshitskiy, A. V., Gaydaenko, V. I., Dyadkin, A. A.
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Sprache:eng
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Zusammenfassung: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.
ISSN:2070-0482
2070-0490
DOI:10.1134/S2070048216050057