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Volodin Vladislav Vladimirovich

Publications in Math-Net.Ru

  1. The interaction of exposed electrodes of symmetric plasma actuator in a subsonic flow for controlling the lift force of the wing

    Pisma v Zhurnal Tekhnicheskoi Fiziki, 51:20 (2025),  13–16
  2. Экспериментальное исследование фронта сферически расширяющегося пламени

    TVT, 63:6 (2025),  743–749
  3. Cellular structure of a hydrogen-air flame in a channel above a porous layer

    Pisma v Zhurnal Tekhnicheskoi Fiziki, 50:21 (2024),  11–14
  4. Исследование распространения водородно-воздушного пламени в плоском зазоре методом инфракрасной визуализации

    TVT, 62:3 (2024),  425–431
  5. Influence of acoustic oscillations on the speed of a cellular hydrogen-air flame in a horizontal channel

    Pisma v Zhurnal Tekhnicheskoi Fiziki, 48:9 (2022),  41–43
  6. Combustion of hydrogen–air mixtures in a tube with annular ignition

    TVT, 60:6 (2022),  957–960
  7. The effect of initial conditions on the laminar flame front velocity in gas mixtures

    Zhurnal Tekhnicheskoi Fiziki, 91:2 (2021),  247–254
  8. Resonance properties of a low-pressure dielectric barrier discharge

    Zhurnal Tekhnicheskoi Fiziki, 90:12 (2020),  2060–2065
  9. Efficiency of the application of disperse materials to attenuate reflected shock waves

    TVT, 57:1 (2019),  146–149
  10. Optimizing the efficiency of dielectric barrier discharge for creating synthetic jets

    Pisma v Zhurnal Tekhnicheskoi Fiziki, 42:7 (2016),  31–36
  11. The effect of reflected acoustic disturbances on flame front acceleration

    Pisma v Zhurnal Tekhnicheskoi Fiziki, 41:21 (2015),  60–65
  12. Experimental Study of the Development of a Helium Jet during Acoustic Action

    TVT, 52:3 (2014),  450–455
  13. The effect of acoustic oscillations on diffusion combustion of methane

    Pisma v Zhurnal Tekhnicheskoi Fiziki, 38:10 (2012),  57–63
  14. Influence of an acoustic field on flame development and transition to detonation

    TVT, 48:6 (2010),  901–907
  15. The impact made by acoustic waves on the ignition zone and the transition of combustion to detonation: Experiment and numerical simulation

    TVT, 47:2 (2009),  315–316
  16. The thermal correction of the inlet diffuser of a hypersonic scramjet engine

    TVT, 41:3 (2003),  472–474


© Steklov Math. Inst. of RAS, 2026