Search Results - "Bykovskii, F. A."

Initiation of detonation of fuel-air mixtures in a flow-type annular combustor by Bykovskii, F. A., Zhdan, S. A., Vedernikov, E. F.

“…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…”
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Continuous Detonation of the Liquid Kerosene—Air Mixture with Addition of Hydrogen or Syngas by Bykovskii, F. A., Zhdan, S. A., Vedernikov, E. F.

“…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…”
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Heat fluxes to combustor walls during continuous spin detonation of fuel-air mixtures by Bykovskii, F. A., Vedernikov, E. F.

“…Pioneering measurements of heat fluxes to the walls of flow-type combustors of different geometries were performed in regimes of continuous spin detonation of…”
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Continuous Multifront Detonation of a Water-in-Fuel Emulsion with Hot Air in an Annular Combustor 503 mm in Diameter by Bykovskii, F. A., Zhdan, S. A., Vedernikov, E. F.

“…Regimes of continuous multifront detonation of a water-in-fuel emulsion (kerosene TS-1-in-water) mixed with hot air preheated by a firing method in the…”
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Continuous detonation in the regime of self-oscillatory ejection of the oxidizer. 2. Air as an oxidizer by Bykovskii, F. A., Zhdan, S. A., Vedernikov, E. F.

“…Results of an experimental study of continuous detonation of a hydrogen-air mixture in a flow-type annular combustor 306 mm in diameter in the regime of air…”
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Detonation Burning of a Kerosene–Air Mixture in a Radial Vortex Chamber with Geometry Variations at the Entrance and Exit by Bykovskii, F. A., Zhdan, S. A., Vedernikov, E. F.

“…Regimes of detonation burning of a two-phase mixture consisting of TS-1 aviation kerosene and air in a radial vortex chamber 500 mm in diameter with exhaustion…”
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Current status of research of continuous detonation in fuel-air mixtures (Review) by Bykovskii, F. A., Zhdan, S. A.

“…The current status of experimental research of continuous detonation of fuel-air mixtures in flow-type annular combustors is described. Experimental data for C…”
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Continuous Multifront Detonation of Kerosene Mixtures with Air Heated in the Settling Chamber by Bykovskii, F. A., Zhdan, S. A., Vedernikov, E. F.

“…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…”
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Continuous multifront detonation of kerosene–air mixture in an annular combustor with variations of its geometry by Bykovskii, F. A., Zhdan, S. A., Vedernikov, E. F.

“…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…”
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Continuous Spin Detonation of the Kerosene–Air Mixture in a Flow-Type Radial Vortex Combustor 500 mm in Diameter by Bykovskii, F. A., Zhdan, S. A., Vedernikov, E. F.

“…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…”
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Parameters of Continuous Multifront Detonation of a Methane Mixture with Heated Air in an Annular Cylindrical Combustor by Bykovskii, F. A., Zhdan, S. A., Vedernikov, E. F.

“…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…”
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Continuous Detonation of Methane/Hydrogen–Air Mixtures in an Annular Cylindrical Combustor by Bykovskii, F. A., Zhdan, S. A., Vedernikov, E. F.

“…Regimes of continuous detonation of methane/hydrogen–air mixtures in spin and opposing transverse detonation waves are obtained for the first time in a…”
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Parameters of Continuous Detonation of Methane/Hydrogen–Air Mixtures with Addition of Air to Combustion Products by Bykovskii, F. A., Zhdan, S. A., Vedernikov, E. F.

“…Results of experimental investigations in a flow-type annular cylindrical combustor with an outer diameter of 503 mm are reported. The influence of air…”
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Continuous Detonation of CH4/H2–Air Mixtures in an Annular Combustor with Varied Geometry by Bykovskii, F. A., Zhdan, S. A., Vedernikov, E. F.

“…Regimes of continuous detonation of CH 4 /H 2 –air mixtures with mass fractions of H 2 in the fuel equal to 0–1/5 are obtained in an annular combustor 503 mm…”
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Continuous detonation of a hydrogen–oxygen gas mixture in a 100-mm plane-radial combustor with exhaustion toward the periphery by Bykovskii, F. A., Zhdan, S. A., Vedernikov, E. F., Tarnaikin, A. E., Samsonov, A. N.

“…Regimes of continuous spin detonation and continuous multifront detonation in a hydrogen–oxygen mixture are obtained in a plane-radial combustor with an inner…”
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Detonation burning of anthracite and lignite particles in a flow-type radial combustor by Bykovskii, F. A., Zhdan, S. A., Vedernikov, E. F., Zholobov, Yu. A.

“…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…”
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Detonation combustion of lignite with titanium dioxide and water additives in air by Bykovskii, F. A., Vedernikov, E. F., Zholobov, Yu. A.

“…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…”
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Scaling factor in continuous spin detonation of syngas–air mixtures by Bykovskii, F. A., Zhdan, S. A., Vedernikov, E. F., Samsonov, A. N.

“…Multiwave regimes of continuous spin detonation in syngas–air mixtures in a flow-type annular cylindrical combustor 503 mm in diameter are obtained…”
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MHD Effects in Continuous Spin Detonation by Popov, E. L., Samsonov, A. N., Bykovskii, F. A., Vedernikov, E. F.

“…Conversion possibility of the chemical energy of combustion products of a hydrogen–oxygen mixture into electrical energy with the use of continuous spin…”
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Effect of combustor geometry on continuous spin detonation in syngas–air mixtures by Bykovskii, F. A., Zhdan, S. A., Vedernikov, E. F., Samsonov, A. N.

“…Regimes of continuous detonation burning of syngas–air mixtures in transverse (spinning) detonation waves in a flow-type annular cylindrical combustor are…”
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