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Simulation of Characteristics of a System of Supersonic Jets in Carbon Dioxide Atmosphere

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Abstract

A simulation of the structure and processes of heat and mass transfer in the system of exhaust jets of brake engines of a spacecraft descending in the Martian atmosphere is carried out. It is taken into account that the system of jets is a chemically reacting gaseous medium consisting of the exhaust gases and the Martian atmosphere; it is under conditions of quite high temperatures and is characterized by a developed turbulence. For realistic conditions, the calculation fields of the entire set of parameters of the medium consisting of the system of interacting supersonic exhaust jets of brake engines of a descending spacecraft in the Martian atmosphere are obtained.

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Authors and Affiliations

  1. All-Russian Scientific Research Institute of Experimental Physics, Russian Federal Nuclear Center, Sarov, Nizhny Novgorod oblast, 607188, Russia

    Yu. N. Deryugin, D. K. Zelenskii, R. N. Zhuchkov & Ya. V. Emel’yanova

  2. Institute of Problems of Chemical Physics, Russian Academy of Sciences, Chernogolovka, Moscow oblast, 142432, Russia

    G. A. Pavlov & A. L. Smirnov

Authors
  1. Yu. N. Deryugin
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  2. D. K. Zelenskii
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  3. R. N. Zhuchkov
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  4. Ya. V. Emel’yanova
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  5. G. A. Pavlov
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  6. A. L. Smirnov
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Corresponding author

Correspondence to A. L. Smirnov.

Additional information

Original Russian Text © Yu.N. Deryugin, D.K. Zelenskii, R.N. Zhuchkov, Ya.V. Emel’yanova, G.A. Pavlov, A.L. Smirnov, 2018, published in Pis’ma v Zhurnal Tekhnicheskoi Fiziki, 2018, Vol. 44, No. 24, pp. 59–66.

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Deryugin, Y.N., Zelenskii, D.K., Zhuchkov, R.N. et al. Simulation of Characteristics of a System of Supersonic Jets in Carbon Dioxide Atmosphere. Tech. Phys. Lett. 44, 1145–1149 (2018). https://doi.org/10.1134/S1063785018120404

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  • DOI: https://doi.org/10.1134/S1063785018120404

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