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Publications in Math-Net.Ru
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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
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Coupled problem of modeling the internal ballistics of nozzleless solid rocket motors
Fizika Goreniya i Vzryva, 49:5 (2013), 77–85
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Bifurcations of the flow characteristics of an adjustable supersonic nozzle
Prikl. Mekh. Tekh. Fiz., 54:5 (2013), 48–57
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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
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Method of the model equation in the theory of unsteady combustion of a solid propellant
Fizika Goreniya i Vzryva, 48:1 (2012), 71–79
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Adjoint problem for modeling intraballistic characteristics of solid-propellant rocket motors
Fizika Goreniya i Vzryva, 48:1 (2012), 38–46
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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
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Two-zone model for combustion of a composite solid propellant with a coolant
Fizika Goreniya i Vzryva, 46:3 (2010), 84–94
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Effect of tension of a composite propellant on its burning rate
Fizika Goreniya i Vzryva, 45:6 (2009), 48–56
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Mechanism and laws of combustion of composite solid propellants with a coolant
Fizika Goreniya i Vzryva, 43:6 (2007), 51–60
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