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Numerical simulation of some problems of recovery capsule aerodynamics

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Abstract

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.

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References

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Authors and Affiliations

  1. Institute of Computer-Aided Design (ICAD), Russian Academy of Sciences, Moscow, Russia

    O. M. Belotserkovskii, A. V. Babakov & V. I. Gaydaenko

  2. Korolev Rocket and Space Public Corporation Energia (RSC Energia), Moscow, Russia

    A. V. Beloshitskiy & A. A. Dyadkin

Authors
  1. O. M. Belotserkovskii
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  2. A. V. Babakov
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  3. A. V. Beloshitskiy
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  4. V. I. Gaydaenko
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  5. A. A. Dyadkin
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Corresponding author

Correspondence to A. V. Babakov.

Additional information

Original Russian Text © O.M. Belotserkovskii, A.V. Babakov, A.V. Beloshitskiy, V.I. Gaydaenko, A.A. Dyadkin, 2016, published in Matematicheskoe Modelirovanie, 2016, Vol. 28, No. 2, pp. 111–122.

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Belotserkovskii, O.M., Babakov, A.V., Beloshitskiy, A.V. et al. Numerical simulation of some problems of recovery capsule aerodynamics. Math Models Comput Simul 8, 568–576 (2016). https://doi.org/10.1134/S2070048216050057

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  • DOI: https://doi.org/10.1134/S2070048216050057

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