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Impact of High-Temperature Effects on Shock Inclination Angle in Super- and Hypersonic Flow around Sharp Cone

  • AERO- AND GAS-DYNAMICS OF FLIGHT VEHICLES AND THEIR ENGINES
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Abstract

Numerical simulation of a super- and hypersonic flow of an inviscid gas around a sharp cone is performed taking into account high-temperature effects. The numerical implementation of a computational procedure designed to find stationary solutions of the gas dynamics equations describing flows around a cone with the real gas properties is carried out.

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ACKNOWLEDGEMENTS

The study was supported by the Russian Science Foundation (project 19-71-10019).

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Authors and Affiliations

  1. Kingston University, River House, 53–57 High Street, KT1 1LQ, Kingston upon Thames, Surrey, UK

    K. N. Volkov

  2. Baltic State Technical University “VOENMEH”, ul. 1ya Krasnoarmeiskaya 1, 190005, St. Petersburg, Russia

    V. N. Emel’yanov, A. G. Karpenko & S. S. Tolstoguzov

  3. Saint Petersburg State University, Universitetskaya naberezhnaya 7/9, 199034, St. Petersburg, Russia

    A. G. Karpenko & S. S. Tolstoguzov

Authors
  1. K. N. Volkov
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  2. V. N. Emel’yanov
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  3. A. G. Karpenko
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  4. S. S. Tolstoguzov
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Corresponding author

Correspondence to K. N. Volkov.

Additional information

Translated from Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2021, No. 3, pp. 99 - 107.

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Volkov, K.N., Emel’yanov, V.N., Karpenko, A.G. et al. Impact of High-Temperature Effects on Shock Inclination Angle in Super- and Hypersonic Flow around Sharp Cone. Russ. Aeronaut. 64, 466–475 (2021). https://doi.org/10.3103/S1068799821030132

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  • DOI: https://doi.org/10.3103/S1068799821030132

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