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Fuel atomization and mixing in unsteady swirling flows behind the gas-dynamic stabilizer

  • Aircraft and Rocket Engine Theory
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Abstract

Features of fuel atomization and propagation in the flow behind a gas-dynamic stabilizer are considered. Estimations of the influence of transverse jets impulse magnitude on characteristics of mixing behind the stabilizer are obtained by numerical and experimental methods.

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Authors and Affiliations

  1. P.I. Baranov Central Institute of Aviation Motors Development (TsIAM), ul. Aviamotornaya 2, Moscow, 111116, Russia

    V. V. Tret’yakov, A. A. Sviridenkov & P. D. Toktaliev

Authors
  1. V. V. Tret’yakov
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  2. A. A. Sviridenkov
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  3. P. D. Toktaliev
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Corresponding author

Correspondence to P. D. Toktaliev.

Additional information

Original Russian Text© V.V. Tret’yakov, A.A. Sviridenkov, P.D. Toktaliev, 2017, published in Izvestiya Vysshikh Uchebnykh Zavedenii. Aviatsionnaya Tekhnika, 2017, No. 3, pp. 106–112.

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Tret’yakov, V.V., Sviridenkov, A.A. & Toktaliev, P.D. Fuel atomization and mixing in unsteady swirling flows behind the gas-dynamic stabilizer. Russ. Aeronaut. 60, 434–441 (2017). https://doi.org/10.3103/S1068799817030163

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  • DOI: https://doi.org/10.3103/S1068799817030163

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