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A hybrid model of hypersonic flow

  • Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
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Abstract

In this paper, a nonequilibrium flow model containing elements of 24-moment and two-temperature models is considered. The model is intended for analyzing the hypersonic flows of polyatomic gases.

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References

  1. Nikitchenko, Yu.A., Modeli neravnovesnykh techenii (Models of Nonequilibrium Flows), Moscow: Izd. MAI, 2013.

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  2. Nikitchenko, Yu.A., The Models of First and Second Approximations for Polyatomic Gas Flows, Vestnik MAI, 2012, vol. 19, no. 2, pp. 11–17.

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Authors and Affiliations

  1. Moscow Aviation Institute (National Research University), Volokolamskoe shosse 4, Moscow, 125993, Russia

    Yu. A. Ryzhov, Yu. A. Nikitchenko & S. A. Popov

Authors
  1. Yu. A. Ryzhov
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  2. Yu. A. Nikitchenko
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  3. S. A. Popov
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Corresponding author

Correspondence to Yu. A. Nikitchenko.

Additional information

Original Russian Text © Yu.A. Ryzhov, Yu.A. Nikitchenko, S.A. Popov, 2015, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2015, No. 1, pp. 26–30.

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Ryzhov, Y.A., Nikitchenko, Y.A. & Popov, S.A. A hybrid model of hypersonic flow. Russ. Aeronaut. 58, 30–36 (2015). https://doi.org/10.3103/S1068799815010055

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  • DOI: https://doi.org/10.3103/S1068799815010055

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