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Control of the Formation of a Transonic Region in a Supersonic Flow by Using a Throttling Jet and Near-Wall Heat Release

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Abstract

Starting of an air-breathing engine with fuel injection distributed along the combustion chamber is numerically simulated. Issues of principal importance are the presence of a compressed ar jet generating a throttling effect and preliminary deceleration of the flow to transonic velocities. Averaged Navier-Stokes equations closed by the SST, SST k-ω, or k-ε turbulence model are solved. Hydrogen and ethylene combustion is simulated by one reaction. The computations are performed for various values of the turbulent kinetic energy in the flow. A pulsed transonic regime of hydrogen and ethylene combustion is discovered.

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Authors and Affiliations

  1. Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch, Russian Academy of Sciences, Novosibirsk, 630090, Russia

    V. P. Zamuraev & A. P. Kalinina

  2. Novosibirsk State University, Novosibirsk, 630090, Russia

    V. P. Zamuraev & A. P. Kalinina

Authors
  1. V. P. Zamuraev
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  2. A. P. Kalinina
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Correspondence to V. P. Zamuraev.

Additional information

Original Russian Text © V.P. Zamuraev, A.P. Kalinina.

Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, Vol. 60, No. 4, pp. 47–55, July–August, 2019.

This study was performed within the framework of the Program of Fundamental Scientific Research of the State Academies of Sciences in 2013–2020 (Project No. AAAA-A17-117030610135-6) and was also supported by the Russian Foundation for Basic Research (Grant No. 17-08-00183).

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Zamuraev, V.P., Kalinina, A.P. Control of the Formation of a Transonic Region in a Supersonic Flow by Using a Throttling Jet and Near-Wall Heat Release. J Appl Mech Tech Phy 60, 631–638 (2019). https://doi.org/10.1134/S0021894419040059

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  • DOI: https://doi.org/10.1134/S0021894419040059

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