S M Frolov


Ontology type: schema:Person     


Person Info

NAME

S M

SURNAME

Frolov

Publications in SciGraph latest 50 shown

  • 2018-03 Well-posed Euler model of shock-induced two-phase flow in bubbly liquid in SHOCK WAVES
  • 2018 Pulse-Detonation Hydrojet in PROCEEDINGS OF THE SCIENTIFIC-PRACTICAL CONFERENCE "RESEARCH AND DEVELOPMENT - 2016"
  • 2017-09 Deflagration-to-detonation transition in crossed-flow fast jets of propellant components in DOKLADY PHYSICAL CHEMISTRY
  • 2017-07 Hydrojet engine with pulse detonation combustion of liquid-fuel in DOKLADY PHYSICAL CHEMISTRY
  • 2017-06 Deflagration-to-detonation transition in the gas–liquid-fuel film system in DOKLADY PHYSICAL CHEMISTRY
  • 2017-05 Demonstrator of continuous-detonation air-breathing ramjet: Wind tunnel data in DOKLADY PHYSICAL CHEMISTRY
  • 2017-03 Calculation of shock wave propagation in water containing reactive gas bubbles in RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B
  • 2016-05 Three-dimensional numerical simulation of the characteristics of a ramjet power plant with a continuous-detonation combustor in supersonic flight in RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B
  • 2016-05 Promotion of the self-ignition of fuel–air mixtures with mechanoactivated Al (Mg)–MoO3 particles in RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B
  • 2016-05 Erratum to: “Three-dimensional numerical simulation of the operation process in a continuous detonation combustor with separate feeding of hydrogen and air” in RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B
  • 2016-03 Thrust characteristics of a pulse detonation engine operating on a liquid hydrocarbon fuel in RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B
  • 2016-03 Thrust characteristics of an airbreathing pulse detonation engine in flight at mach numbers of 0.4 to 5.0 in RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B
  • 2015-11 Chemiionization and acoustic diagnostics of the process in continuous- and pulse-detonation combustors in DOKLADY PHYSICAL CHEMISTRY
  • 2015-11 Momentum transfer from a shock wave to a bubbly liquid in RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B
  • 2015-07 Magnetohydrodynamic effects of heterogeneous spray detonation in RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B
  • 2015-05 Numerical simulation of momentum transfer from a shock wave to a bubbly medium in RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B
  • 2015-03 Energy efficiency of a continuous-detonation combustion chamber in COMBUSTION, EXPLOSION, AND SHOCK WAVES
  • 2015-01 Three-dimensional numerical simulation of the operation process in a continuous detonation combustor with separate feeding of hydrogen and air in RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B
  • 2014-12 Experimental proof of the energy efficiency of the Zel’dovich thermodynamic cycle in DOKLADY PHYSICAL CHEMISTRY
  • 2014-11 3D versus 2D calculation of thrust characteristics of the air-breathing pulse detonation engine under supersonic flight conditions in RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B
  • 2014-03 Transient modes of propagation of the shock wave-reaction zone complex in methane-air mixtures in RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B
  • 2013-05 Thrust characteristics of an airbreathing pulse detonation engine in supersonic flight at various altitudes in RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B
  • 2013-04 Deflagration-to-detonation transition in a high-velocity flow with separate delivery of fuel and oxidizer in DOKLADY PHYSICAL CHEMISTRY
  • 2013-03 Cyclic deflagration-to-detonation transition in the flow-type combustion chamber of a pulse-detonation burner in RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B
  • 2013-02 Three-dimensional numerical simulation of the operation of a rotating-detonation chamber with separate supply of fuel and oxidizer in RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B
  • 2012-03 Three-dimensional numerical simulation of the operation of the rotating-detonation chamber in RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B
  • 2011-08 Pulse-detonation burner unit operating on natural gas in RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B
  • 2011-08 Numerical simulation of the operation process and thrust performance of an air-breathing pulse detonation engine in supersonic flight conditions in RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B
  • 2011-08 Formation of nitrogen oxides in detonation waves in RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B
  • 2011-08 Experimental demonstration of the operation process of a pulse-detonation liquid rocket engine in RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B
  • 2009-12 Real-gas properties of n-alkanes, O2, N2, H2O, CO, CO2, and H2 for diesel engine operation conditions in RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B
  • 2009-06 Correlation between drop vaporization and self-ignition in RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B
  • 2009 Shock-to-detonation transition due to shock interaction with prechamber-jet cloud in SHOCK WAVES
  • 2008-06 A modified model of the ignition of a magnesium particle in RUSSIAN JOURNAL OF PHYSICAL CHEMISTRY B
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