3. Теория вероятностей

Joint Meeting of the Russian and Japanese Sections of the Combustion Institute. Chernogolovka, Moscow 3. Теория вероятностей, 1993, 245 p. Moscow, ENAS Publishers, 1995, 476 p. Advanced Computation and Analysis of Combustion.

Moscow, ENAS Publishers, 1997, 592 p. Advances in Experimentation and Computation of Detonations. Moscow, ENAS Publishers, 1998, 144 p. Gaseous and Heterogeneous Detonations: Science to Applications, ENAS Publishers, Moscow, 1999. Control of Detonation Processes, ELEX-KM Publishers, Moscow, 2000, 240 p.

Detonation and High-Speed Deflagration: Fundamentals and Control, ELEX-KM Publishers, Moscow, 2001, 384 p. Confined Detonations and Pulse Detonation Engines. Moscow, Torus Press, 2003, 384 p. Moscow, Torus Press, 2003, 680 p. Moscow, Torus Press, 2004, 432 p. Moscow, Torus Press, 2004, 168 p.

Moscow, Torus Press, 2004, 328 p. Moscow, Torus Press, 2005, 312 p. Moscow, Torus Press, 2005, 440 p. Volume 2: Plasma, Aerosols, and Atmospheric Phenomena. Moscow, Torus Press, 2005, 392 p. Moscow, Torus Press, 2006, 286 p.

Moscow: Torus Press, 2006, 376 p. Turbomachines: Aeroelasticity, Aeroacoustics, and Unsteady Aerodynamics. Moscow: Torus Press, 2006, 472 p. Nonequilibrium Processes: Plasma, Combustion, Atmospheric Phenomena. Moscow, Torus Press, 2007, 120 p.

EUCASS Advances in Aerospace Sciences Book Ser. EDP Sciences, TORUS PRESS, 2009, Vol. Aerospace Research: ISTC Funded Projects 1994-2009. Moscow: Torus Press, 2010, 520 p. Moscow, Torus Press, 2010, 488 p. EDP Sciences, TORUS PRESS, 2011, Vol.

Nonequilibrium Processes in Plasma, Combustion, and Atmosphere. Moscow, Torus Press, 2012, 482 p. EDP Sciences, TORUS PRESS, 2013, Vol. Advances in Nonequilibrium Processes: Plasma, Combustion, and Atmosphere. Moscow, Torus Press, 2014, 344 p. Zel’dovich Memorial: Accomplishments in the combustion science in the last decade. Transient Combustion and Detonation Phenomena: Fundamentals and Applications.

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Moscow, Torus Press, 2014, 696 p. EUCASS advances in aerospace sciences book series. Moscow: TORUS PRESS, 2016, 496 p. Moscow, TORUS PRESS, 2016, 368 p. Nonequilibrium Processes in Physics and Chemistry, Vol.

Moscow, Torus Press, 2016, 334 p. Moscow, Torus Press, 2016, 380 p. Flow structure in rotating detonation engine with separate supply of fuel and oxidizer: experiment and CFD. In: Detonation Control for Propulsion: Pulse Detonation and Rotating Detonation Engines. Springer International Publishing AG 2018, 2018, pp. Well-posed Euler model of shock-induced two-phase flow in bubbly liquid.

Hydrogen-fueled detonation ramjet model: Wind tunnel tests at approach air stream Mach number 5. 7 and stagnation temperature 1500 K, International Journal of Hydrogen Energy, 2018, Vol. Low-temperature flameless combustion of a large drop of n-dodecane under microgravity conditions. A detailed kinetic mechanism of multistage oxidation and combustion of octanes. Experimental and computational studies of shock wave-to-bubbly water momentum transfer.

International Journal of Multiphase Flow, 2017, No. Novel approach for predicting knocking combustion in gasoline engines. In: Automotive Engineering for Improved Safety. 19-20 April 2017, Belgrade, Serbia, JUMV Publ. Deflagration-to-Detonation Transition in Crossed-Flow Fast Jets of Propellant Components.

Hydrojet engine with pulse detonation combustion of liquid fuel. Wind tunnel tests of a hydrogen-fueled detonation ramjet model at approach air stream Mach numbers from 4 to 8. 9th International Seminar of Flame Structure, Book of Abstracts, Novosibirsk, Russia, 10-14 July 2017. International Journal of Hydrogen Energy, 2017, Vol. D in detonation engines and droplet combustion in microgravity experiment.

Wind tunnel tests of a hydrogen-fueled detonation ramjet model at Mach 4 to 8. IWDP 2017 Program and Abstracts, International Workshop on Detonation for Propulsion, December 6 to 8, 2017, Poitiers, France, 2017, p. 31st Annual Symposium of the Israeli Section of the Combustion Institute, December 14, 2017, Tel Aviv, The Open University of Israel, 2017, pp. Thrust characteristics of an air-breathing pulse detonation engine in flight at Mach numbers of 0. Russian Journal of Physical Chemistry B, 2016, Vol.

Thrust characteristics of a pulse detonation engine operating on a liquid hydrocarbon fuel. The effect of turbulence on flow development in high-speed combustor. Well-posed Euler model of shock and detonation induced two-phase flow in bubbly liquid. Operation and performance of rotating detonation rocket engine fueled by natural gas: Experimental studies.

Operation of air-breathing hydrogen-fueled rotating detonation engine in supersonic flight conditions: numerical simulation. Flight performance of a propulsion unit equipped with pulse detonation engine and bypass duct. Subgrid model for simulating turbulent combustion, preflame autoignition and pollutant formation. Modeling of n-heptane drop self-ignition and combustion using detailed reaction mechanism. Pressure-enthalpy coupling for subsonic flows with density variation. In: Advances in Fluid Mechanics VIII, Ed.

Initiation of gas detonation in a tube with a shaped contraction. Nonreflecting boundary conditions at open boundaries for compressible and incompressible multidimensional flows. Equations of state of gas-phase n-alkanes for modeling the operation process in piston engines. Conjugate model of ignition and combustion of a particle of condensed energetic material with regard for reactions in gas and condensed phase. Advances in Aerospace Sciences EUCASS Book Ser.

TORUS PRESS, EDP, Moscow-Paris, 2009, pp. Detonation initiation techniques for pulse detonation propulsion. Tracking of propagating turbulent flames and autoignition in enclosure. Correlation between drop vaporization and self-ignition. Russian Journal of Physical Chemistry B, 2009, Vol.

(Horizontal)

Initiation of gas detonation in a tube with a shaped obstacle. Detonations of liquid sprays and drop suspensions: Theory. Detonations of liquid sprays and drop suspensions: Experiment. Improving cost-effectivemess of LES by using non-reflecting boundary conditions: The flow around simplified ICE2 train.

Numerical and experimental investigation of detonation initiation in profiled tubes. In: Nonequilibrium Phenomena: Plasma, Combustion, Atmosphere. Ignition of hydrogen-air mixture in the flow over hot catalytic surface. Spray penetration and vaporization in Diesel engines: Numerical simulation and experiments. Numerical simulation of propane-air turbulent flame acceleration in straight tubes of different length. European-Russian Workshop on Rotating Detonation Wave Engine for Space Propulsion.

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LCD, UPR9029 CNRS, ENSMA-Futuroscope-France, 2009, p. Real-gas properties of n-alkanes, O2, N2, H2O, CO, CO2, and H2 for Diesel engine operation conditions. Journal of Physical Chemistry B, 2009, Vol. Shock-to-detonation transition due to shock interaction with prechamber-jet cloud. Seiler, Springer Berlin Heidelberg, 2009, pp. In: Shock Wave Science and Technology Reference Library, Vol.

Zhang, Springer Berlin Heidelberg, 2009, pp. Turbulent combustion and localized preflame autoignition of hydrogen-air mixture in an enclosure. ISSN 1990-7931, Russian Journal of Physical Chemistry B, 2008, Vol. A modified model of the ignition of a magnesium particle. Russian Journal of Physical Chemistry B, 2008, Vol.

Structure and limits of heterogeneous detonation. Modeling of soot formation in internal combustion engines. Propagation of shock and detonation waves in channels with U-shaped bends of limiting curvature. Correlation between drop vaporization and autoignition phenomena.

Influence of melting on magnesium particle ignition. Simulation of chemical processes in turbulent flow reactors by Monte Carlo method. Transient numerical code with grid adaptation for gas combustion and detonation studies. Modified model of aluminum particle ignition. The calculation of liquid-vapor phase equilibrium in H2O-H2O2 two-component system. Pulse-detonation combustion: new generation of power plants. Modeling of evaporation, self-ignition and combustion of diesel oil sprays.

Transactions of Vladimir State University, 2008, No. Combustion science and problems of contemporary power engineering. Russian Journal of General Chemistry, 2009, Vol. Modeling of drop ignition and combustion in dense suspensions.

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Poipu Bay, Kauai, 10-12 December 2008, pp. ISSN 0012-5016, Doklady Physical Chemistry, 2007, Vol. Shock wave and detonation propagation through U-bend tubes. Proceedings of the Combustion Institute, 2007, Vol. Modeling of n-butane ignition, combustion, and preflame oxidation in the 20-liter vessel.

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Effect of transient heat transfer on ignition of solid particles. Shamshin Reactive shock and detonation propagation in U-bend tubes. Shock-induced dust ignition in curved pipeline with steady flow. Joint Meeting of the Russian and Japanese Sections of the Combustion Institute.

Chernogolovka, Moscow Region, 1993, 245 p. Moscow, ENAS Publishers, 1995, 476 p. Advanced Computation and Analysis of Combustion. Moscow, ENAS Publishers, 1997, 592 p. Advances in Experimentation and Computation of Detonations. Moscow, ENAS Publishers, 1998, 144 p.

Gaseous and Heterogeneous Detonations: Science to Applications, ENAS Publishers, Moscow, 1999. Control of Detonation Processes, ELEX-KM Publishers, Moscow, 2000, 240 p. Detonation and High-Speed Deflagration: Fundamentals and Control, ELEX-KM Publishers, Moscow, 2001, 384 p. Confined Detonations and Pulse Detonation Engines. Moscow, Torus Press, 2003, 384 p. Moscow, Torus Press, 2003, 680 p. Moscow, Torus Press, 2004, 432 p.

Moscow, Torus Press, 2004, 168 p. Moscow, Torus Press, 2004, 328 p. Moscow, Torus Press, 2005, 312 p. Moscow, Torus Press, 2005, 440 p. Volume 2: Plasma, Aerosols, and Atmospheric Phenomena. Moscow, Torus Press, 2005, 392 p.

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Moscow, Torus Press, 2006, 286 p. Moscow: Torus Press, 2006, 376 p. Turbomachines: Aeroelasticity, Aeroacoustics, and Unsteady Aerodynamics. Moscow: Torus Press, 2006, 472 p. Nonequilibrium Processes: Plasma, Combustion, Atmospheric Phenomena. Moscow, Torus Press, 2007, 120 p.

EUCASS Advances in Aerospace Sciences Book Ser. EDP Sciences, TORUS PRESS, 2009, Vol. Aerospace Research: ISTC Funded Projects 1994-2009. Moscow: Torus Press, 2010, 520 p.

Moscow, Torus Press, 2010, 488 p. EDP Sciences, TORUS PRESS, 2011, Vol. Nonequilibrium Processes in Plasma, Combustion, and Atmosphere. Moscow, Torus Press, 2012, 482 p. EDP Sciences, TORUS PRESS, 2013, Vol.

Advances in Nonequilibrium Processes: Plasma, Combustion, and Atmosphere. Moscow, Torus Press, 2014, 344 p. Zel’dovich Memorial: Accomplishments in the combustion science in the last decade. Transient Combustion and Detonation Phenomena: Fundamentals and Applications. Moscow, Torus Press, 2014, 696 p. EUCASS advances in aerospace sciences book series. Moscow: TORUS PRESS, 2016, 496 p.

Moscow, TORUS PRESS, 2016, 368 p. Nonequilibrium Processes in Physics and Chemistry, Vol. Moscow, Torus Press, 2016, 334 p. Moscow, Torus Press, 2016, 380 p. Flow structure in rotating detonation engine with separate supply of fuel and oxidizer: experiment and CFD. In: Detonation Control for Propulsion: Pulse Detonation and Rotating Detonation Engines. Springer International Publishing AG 2018, 2018, pp.

Well-posed Euler model of shock-induced two-phase flow in bubbly liquid. Hydrogen-fueled detonation ramjet model: Wind tunnel tests at approach air stream Mach number 5. 7 and stagnation temperature 1500 K, International Journal of Hydrogen Energy, 2018, Vol. Low-temperature flameless combustion of a large drop of n-dodecane under microgravity conditions. A detailed kinetic mechanism of multistage oxidation and combustion of octanes. Experimental and computational studies of shock wave-to-bubbly water momentum transfer.

International Journal of Multiphase Flow, 2017, No. Novel approach for predicting knocking combustion in gasoline engines. In: Automotive Engineering for Improved Safety. 19-20 April 2017, Belgrade, Serbia, JUMV Publ. Deflagration-to-Detonation Transition in Crossed-Flow Fast Jets of Propellant Components. Hydrojet engine with pulse detonation combustion of liquid fuel.

Wind tunnel tests of a hydrogen-fueled detonation ramjet model at approach air stream Mach numbers from 4 to 8. 9th International Seminar of Flame Structure, Book of Abstracts, Novosibirsk, Russia, 10-14 July 2017. International Journal of Hydrogen Energy, 2017, Vol. D in detonation engines and droplet combustion in microgravity experiment. Wind tunnel tests of a hydrogen-fueled detonation ramjet model at Mach 4 to 8. IWDP 2017 Program and Abstracts, International Workshop on Detonation for Propulsion, December 6 to 8, 2017, Poitiers, France, 2017, p. 31st Annual Symposium of the Israeli Section of the Combustion Institute, December 14, 2017, Tel Aviv, The Open University of Israel, 2017, pp.

Thrust characteristics of an air-breathing pulse detonation engine in flight at Mach numbers of 0. Russian Journal of Physical Chemistry B, 2016, Vol. Thrust characteristics of a pulse detonation engine operating on a liquid hydrocarbon fuel. The effect of turbulence on flow development in high-speed combustor.