Search Results - "Guskov, O. V."

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  1. 1

    Computational and experimental study of the influence of the shape of nozzle supersonic part on the flow structure in the gas-dynamic flow path of a model high-altitude test facility by Zakharov, V. S., Guskov, O. V., Prokhorov, A. N., Berezhnoy, V. N.

    Published in Thermophysics and aeromechanics (01-03-2021)
    “…The influence due to the shape of the expanding part of supersonic nozzles on the gas-dynamic structures formed in the ducts of high-altitude rocket and…”
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    Journal Article
  2. 2

    Experimental Research of Gasdynamic Liquid Drops Breakup in the Supersonic Flow with an Oblique Shock Wave by Arefyev, K. Yu, Guskov, O. V., Prokhorov, A. N., Saveliev, A. S., Son, E. E., Gautham, K., Sam, D., Sonu, K. T., Muruganandam, T. M.

    Published in High temperature (01-11-2020)
    “…This paper is devoted to understanding gasdynamic liquid drops breakup in a supersonic flow with presence of an oblique shock wave. An experimental facility,…”
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    Journal Article
  3. 3

    The influence of combustion efficiency on the characteristics of ramjets by Aver’kov, I. S., Aleksandrov, V. Yu, Aref’ev, K. Yu, Voronetskii, A. V., Gus’kov, O. V., Prokhorov, A. N., Yanovskii, L. S.

    Published in High temperature (01-11-2016)
    “…Methods for determining the combustion efficiency, thermodynamics parameters of propellants, and characteristics of ramjets are analyzed. Energetic and…”
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    Journal Article
  4. 4

    Secondary structures in time-dependent rotating flows by Vatazhin, A. B., Gus’kov, O. V.

    Published in Fluid dynamics (01-02-2010)
    “…The problems related with the development of secondary structures in time-dependent rotating flows are considered. The experimental results on the generation…”
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    Journal Article
  5. 5

    Magnetogasdynamic generation of electrical energy in models of aircraft with a high-speed jet engine by Vatazhin, A. B., Gus’kov, O. V., Danilov, M. K., Kopchenov, V. I.

    Published in Fluid dynamics (01-08-2009)
    “…The possibility of generating electric power in a plane model of an integral high-speed hydrogen-burning jet engine by mounting a magnetogasdynamic (MHD)…”
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    Journal Article
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