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Miloekhin Yuri Mikhailovich

Publications in Math-Net.Ru

  1. Numerical simulation of gas-dynamic processes in model solid-fuel engines

    Mat. Model., 37:3 (2025),  3–17
  2. Numerical simulation of thermo-gasdynamic processes in model solid propellant rocket engines using a three-dimensional parallel code

    Keldysh Institute preprints, 2024, 007, 29 pp.
  3. Combustion model for a mixed solid fuel with evaporating coolant

    Fizika Goreniya i Vzryva, 58:3 (2022),  117–127
  4. Impact of a relativistic electron beam on aluminized cast energetic condensed systems

    Fizika Goreniya i Vzryva, 58:2 (2022),  88–99
  5. Comparative analysis of combustion of particles of boron, boron carbide, boron nitride and carbon in air

    Vestn. Tomsk. Gos. Univ. Mat. Mekh., 2022, no. 75,  122–137
  6. Experimental study of the formation of threaded structures and properties spheroplastics upon a shock-wave impact

    Fizika Goreniya i Vzryva, 57:2 (2021),  123–131
  7. Changes in dielectric and mechanical properties of spheroplastic containing metallized glass microspheres under compressive deformation

    Zhurnal Tekhnicheskoi Fiziki, 90:7 (2020),  1121–1127
  8. Dielectric relaxation in energy condensed systems on the basis of a polyesterrethane elastomer. II. Temperature dependence and ignition

    Fizika Goreniya i Vzryva, 55:2 (2019),  108–118
  9. Comparative analysis of boron powders obtained by various methods. I. Microstructure and oxidation parameters during heating

    Fizika Goreniya i Vzryva, 54:4 (2018),  73–83
  10. Effect of distributed injection of air into the afterburning chamber of a ram-rocket engine on the efficiency of combustion of boron particles

    Fizika Goreniya i Vzryva, 53:6 (2017),  38–52
  11. Dielectric relaxation in energy condensed systems on the basis of polyefirretane elastomer. I. Frequency dependence

    Fizika Goreniya i Vzryva, 53:5 (2017),  132–140
  12. Some features of the dielectric relaxation of glyceryl trinitrate

    Fizika Goreniya i Vzryva, 53:1 (2017),  57–63
  13. Correlation of parameters in the burning rate law and its influence on intraballistic characteristics of a rocket motor

    Fizika Goreniya i Vzryva, 52:4 (2016),  61–73
  14. Calculation of the unsteady internal ballistic parameters of the transition of a solid rocket motor to steady-state operation using the method of characteristics

    Fizika Goreniya i Vzryva, 50:6 (2014),  61–74
  15. Coupled problem of modeling the internal ballistics of nozzleless solid rocket motors

    Fizika Goreniya i Vzryva, 49:5 (2013),  77–85
  16. Bifurcations of the flow characteristics of an adjustable supersonic nozzle

    Prikl. Mekh. Tekh. Fiz., 54:5 (2013),  48–57
  17. Combustion mechanism of mixtures of binders capable of self-sustained combustion with inert and active fillers

    Fizika Goreniya i Vzryva, 48:2 (2012),  60–75
  18. Specific features of propagation of an electromagnetic pulse in a solid-propellant energetic system

    Fizika Goreniya i Vzryva, 48:1 (2012),  110–116
  19. Method of the model equation in the theory of unsteady combustion of a solid propellant

    Fizika Goreniya i Vzryva, 48:1 (2012),  71–79
  20. Adjoint problem for modeling intraballistic characteristics of solid-propellant rocket motors

    Fizika Goreniya i Vzryva, 48:1 (2012),  38–46
  21. Diffraction of an electromagnetic pulse at a finite-length dielectric gradient cylinder

    Zhurnal Tekhnicheskoi Fiziki, 82:9 (2012),  55–62
  22. Calculation of heat balance in burning HMX

    Fizika Goreniya i Vzryva, 47:3 (2011),  60–73
  23. Technical approach to evaluating the loss in rocket motor specific impulse due to discontinuity of the nozzle block contour

    Fizika Goreniya i Vzryva, 46:5 (2010),  112–118
  24. Pulsed electrical breakdown of energetic composite condensed systems

    Fizika Goreniya i Vzryva, 46:4 (2010),  107–115
  25. Two-zone model for combustion of a composite solid propellant with a coolant

    Fizika Goreniya i Vzryva, 46:3 (2010),  84–94
  26. Mathematical Modelling the Electromagnetic Pulse’s Propagation in the Solid Propellant Propulsion Device

    Keldysh Institute preprints, 2010, 080, 16 pp.
  27. Effect of tension of a composite propellant on its burning rate

    Fizika Goreniya i Vzryva, 45:6 (2009),  48–56
  28. Gas release in energetic compositions with an active fuel binder on exposure to ionizing radiation

    Fizika Goreniya i Vzryva, 44:4 (2008),  66–71
  29. Special features characteristic of the use of differential scanning calorimetry for the investigation of the kinetics of thermal decomposition of energetic materials

    TVT, 46:2 (2008),  290–304
  30. Specific features of thermal decomposition of ammonium perchlorate subjected to $\gamma$ radiation

    Fizika Goreniya i Vzryva, 43:6 (2007),  69–74
  31. Mechanism and laws of combustion of composite solid propellants with a coolant

    Fizika Goreniya i Vzryva, 43:6 (2007),  51–60
  32. Electrical effects in propellant compositions radiated by electrons

    Fizika Goreniya i Vzryva, 43:5 (2007),  52–63
  33. Thermal decomposition of polyester polyurethane and its elastomers exposed to $\gamma$-radiation

    Fizika Goreniya i Vzryva, 42:2 (2006),  133–138


© Steklov Math. Inst. of RAS, 2026