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  1. No Access

    Article

    Continuous Multifront Detonation of Kerosene Mixtures with Air Heated in the Settling Chamber

    Regimes of continuous multifront detonation of two-phase mixtures of aviation kerosene and hot air are obtained for the first time and studied in a flow-type annular combustor 503 mm in diameter and 600 mm lon...

    F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov in Combustion, Explosion, and Shock Waves (2023)

  2. No Access

    Article

    Parameters of Continuous Multifront Detonation of a Methane Mixture with Heated Air in an Annular Cylindrical Combustor

    Regimes of continuous multifront detonation in a methane mixture with heated air in a flow-type annular combustor 503 mm in diameter are obtained and studied for the first time. Air is preheated by straight fi...

    F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov in Combustion, Explosion, and Shock Waves (2022)

  3. No Access

    Article

    Continuous Spin Detonation of the Kerosene–Air Mixture in a Flow-Type Radial Vortex Combustor 500 mm in Diameter

    Regimes of detonation burning of TS-1 aviation kerosene in an air flow in a flow-type radial vortex combustor 500 mm in diameter with exhaustion toward the center are obtained. The parameters varied in experim...

    F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov in Combustion, Explosion, and Shock Waves (2022)

  4. No Access

    Article

    Continuous multifront detonation of kerosene–air mixture in an annular combustor with variations of its geometry

    Regimes of continuous detonation of aviation kerosene and air mixtures are obtained for the first time and studied in a flow-type annular cylindrical chamber 503 mm in diameter with variations of its geometry....

    F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov in Shock Waves (2021)

  5. No Access

    Article

    Continuous Detonation of a Mixture of Gaseous Hydrogen and Liquid Oxygen in a Plane–Radial Combustor with Exhaustion Toward the Periphery

    Regimes of continuous spin detonation and continuous multifront detonation of a gas–droplet mixture of gaseous hydrogen and liquid oxygen in a plane–radial combustor (internal diameter of 100 mm and external d...

    F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov… in Combustion, Explosion, and Shock Waves (2020)

  6. No Access

    Article

    Continuous Detonation of CH4/H2–Air Mixtures in an Annular Combustor with Varied Geometry

    Regimes of continuous detonation of CH4/H2–air mixtures with mass fractions of H2 in the fuel equal to 0–1/5 are obtained in an annular combustor 503 mm in diameter with variation of the combustor geometry. The i...

    F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov in Combustion, Explosion, and Shock Waves (2020)

  7. No Access

    Article

    Continuous detonation of a hydrogen–oxygen gas mixture in a 100-mm plane-radial combustor with exhaustion toward the periphery

    Regimes of continuous spin detonation and continuous multifront detonation in a hydrogen–oxygen mixture are obtained in a plane-radial combustor with an inner diameter of 100 mm and exhaustion toward the perip...

    F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov, A. E. Tarnaikin… in Shock Waves (2020)

  8. No Access

    Article

    Parameters of Continuous Detonation of Methane/Hydrogen–Air Mixtures with Addition of Air to Combustion Products

    Results of experimental investigations in a flow-type annular cylindrical combustor with an outer diameter of 503 mm are reported. The influence of air addition to products of continuous spin detonation of CH4/ $...

    F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov in Combustion, Explosion, and Shock Waves (2020)

  9. No Access

    Article

    Continuous Detonation of the Liquid Kerosene—Air Mixture with Addition of Hydrogen or Syngas

    Regimes of continuous detonation of heterogeneous mixtures of aviation kerosene and air with addition of hydrogen or syngas are studied in a flow-type annular cylindrical combustor 503 mm in diameter. With var...

    F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov in Combustion, Explosion, and Shock Waves (2019)

  10. No Access

    Article

    MHD Effects in Continuous Spin Detonation

    Conversion possibility of the chemical energy of combustion products of a hydrogen–oxygen mixture into electrical energy with the use of continuous spin detonation has been demonstrated for the first time in a...

    E. L. Popov, A. N. Samsonov, F. A. Bykovskii, E. F. Vedernikov in Doklady Physics (2019)

  11. No Access

    Article

    Continuous Detonation of Methane/Hydrogen–Air Mixtures in an Annular Cylindrical Combustor

    Regimes of continuous detonation of methane/hydrogen–air mixtures in spin and opposing transverse detonation waves are obtained for the first time in a flow-type annular cylindrical combustor 503 mm in diamete...

    F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov in Combustion, Explosion, and Shock Waves (2018)

  12. No Access

    Article

    Detonation combustion of lignite with titanium dioxide and water additives in air

    The influence of mineral additives (6.2–70%) and water (15–54%) to lignite on the possibility of its burning in an air flow in a continuous detonation regime in a radial vortex combustor 500 mm in diameter is ...

    F. A. Bykovskii, E. F. Vedernikov… in Combustion, Explosion, and Shock Waves (2017)

  13. No Access

    Article

    Scaling factor in continuous spin detonation of syngas–air mixtures

    Multiwave regimes of continuous spin detonation in syngas–air mixtures in a flow-type annular cylindrical combustor 503 mm in diameter are obtained. Experiments are performed for mixtures of carbon oxide and h...

    F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov… in Combustion, Explosion, and Shock Waves (2017)

  14. No Access

    Article

    Pressure measurement by fast-response piezo-electric sensors during continuous spin detonation in the combustor

    Pressure profiles in a transverse detonation wave propagating in a plane-radial vortex chamber during continuous spin detonation of a mixture consisting of lignite, syngas, and air are measured by specially de...

    F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov… in Combustion, Explosion, and Shock Waves (2017)

  15. No Access

    Article

    Detonation burning of anthracite and lignite particles in a flow-type radial combustor

    Regimes of continuous spin detonation of anthracite and lignite particles in an air flow in a radial vortex combustor 500 mm in diameter with a constant (along the radius) cross-sectional area are studied. Gro...

    F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov… in Combustion, Explosion, and Shock Waves (2016)

  16. No Access

    Article

    Detonation combustion of a hydrogen–oxygen mixture in a plane–radial combustor with exhaustion toward the center

    Regimes of continuous spin detonation in a plane–radial combustor with an external diameter of 80 mm with peripheral injection of a hydrogen–oxygen mixture in the range of specific flow rates of the mixture 3....

    F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov… in Combustion, Explosion, and Shock Waves (2016)

  17. No Access

    Article

    Continuous spin detonation of a heterogeneous kerosene–air mixture with addition of hydrogen

    Regimes of continuous spin detonation of two-phase kerosene–air mixtures with small addition of hydrogen are obtained for the first time in a flow-type annular cylindrical combustor 503 mm in diameter.

    F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov in Combustion, Explosion, and Shock Waves (2016)

  18. No Access

    Article

    Effect of combustor geometry on continuous spin detonation in syngas–air mixtures

    Regimes of continuous detonation burning of syngas–air mixtures in transverse (spinning) detonation waves in a flow-type annular cylindrical combustor are considered. Mixtures of carbon oxide and hydrogen in p...

    F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov… in Combustion, Explosion, and Shock Waves (2015)

  19. No Access

    Article

    Current status of research of continuous detonation in fuel-air mixtures (Review)

    The current status of experimental research of continuous detonation of fuel-air mixtures in flow-type annular combustors is described. Experimental data for C2H2-air, H2-air, and CO/H2-air mixtures are analyzed,...

    F. A. Bykovskii, S. A. Zhdan in Combustion, Explosion, and Shock Waves (2015)

  20. No Access

    Article

    Initiation of detonation of fuel-air mixtures in a flow-type annular combustor

    Initiation of detonation in a fuel-air mixture flow formed in an annular cylindrical combustor 306 mm in diameter is studied. The source of detonation initiation is the detonation wave entering the annular cha...

    F. A. Bykovskii, S. A. Zhdan, E. F. Vedernikov in Combustion, Explosion, and Shock Waves (2014)

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