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Pressure and Heat Flux Oscillations Induced by Gas-Dynamic Interaction between a High Inertia Particle and a Shock Layer

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

Oscillatory flow and heat transfer regimes arising from the gas-dynamic interaction between a high-inertial particle and a shock layer in a supersonic flow around bodies are under numerical research. Detailed space-time flow patterns were obtained using high-resolution adaptive grids and parallelization of computations using the graphic processing units.

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ACKNOWLEDGEMENTS

The research was carried out within the framework of the state task of the Ministry of Science and Higher Education of the Russian Federation, project number FSFF-2020-0013.

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Authors and Affiliations

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

    A. V. Sposobin, D. L. Reviznikov, I. E. Ivanov & I. A. Kryukov

  2. Lomonosov Moscow State University, Leninskie gory 1, 119991, Moscow, Russia

    I. E. Ivanov

  3. Ishlinsky Institute for Problems in Mechanics of the Russian Academy of Sciences (IPMekh RAN), pr. Vernadskogo 101-1, 119526, Moscow, Russia

    I. A. Kryukov

Authors
  1. A. V. Sposobin
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  2. D. L. Reviznikov
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  3. I. E. Ivanov
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  4. I. A. Kryukov
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Corresponding author

Correspondence to D. L. Reviznikov.

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Translated from Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2020, No. 4, pp. 108 - 115.

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Sposobin, A.V., Reviznikov, D.L., Ivanov, I.E. et al. Pressure and Heat Flux Oscillations Induced by Gas-Dynamic Interaction between a High Inertia Particle and a Shock Layer. Russ. Aeronaut. 63, 677–685 (2020). https://doi.org/10.3103/S1068799820040157

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  • DOI: https://doi.org/10.3103/S1068799820040157

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