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Publications in Math-Net.Ru
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Modeling of synthesis of composite nanoparticles with a TiO$_2$ core and SiO$_2$ shell in a plasmochemical reactor with agglomeration of both species
Prikl. Mekh. Tekh. Fiz., 64:1 (2023), 27–35
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Control of gas-phase high-temperature synthesis of titanium dioxide nanoparticles in a plasma-chemical reactor with the use of a quenching jet
Prikl. Mekh. Tekh. Fiz., 62:3 (2021), 80–90
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Modeling of synthesis of composite particles consisting of a core and a shell on the basis of simultaneous oxidation of titanium and silicon tetrachlorides in a plasma-chemical reactor
Prikl. Mekh. Tekh. Fiz., 61:4 (2020), 77–83
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Analysis of flight trajectories of a ramjet-powered vehicle
Prikl. Mekh. Tekh. Fiz., 55:6 (2014), 35–42
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Criterial analysis of the effect of vibrations of an airfoil surface element on the transonic flow structure
Prikl. Mekh. Tekh. Fiz., 55:4 (2014), 43–49
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Criterion analysis of nonlinear transonic profile flows under local energy impact
Zhurnal Tekhnicheskoi Fiziki, 83:4 (2013), 21–28
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Control of the flow over wing airfoils in transonic regimes by means of force action of surface elements on the flow
Pisma v Zhurnal Tekhnicheskoi Fiziki, 38:17 (2012), 39–44
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Comparative analysis of the influence of various models of energy supply on the wave drag of an airfoil
Pisma v Zhurnal Tekhnicheskoi Fiziki, 38:12 (2012), 30–36
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Transonic flow control by means of local energy deposition
Zhurnal Tekhnicheskoi Fiziki, 81:11 (2011), 13–22
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Numerical simulation of formation of the titan dioxide in the plasma-chemical reactor of flowing-type
Nanosystems: Physics, Chemistry, Mathematics, 2:4 (2011), 113–119
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Resonant phenomena in a transonic flow around an airfoil with pulsed periodic energy supply
Prikl. Mekh. Tekh. Fiz., 52:5 (2011), 85–93
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Resonant interaction of periodic pulsed energy source with shock-wave structure in transonic flow past airfoil
Pisma v Zhurnal Tekhnicheskoi Fiziki, 36:12 (2010), 8–15
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Skip trajectory flight of a ramjet-powered hypersonic vehicle
Prikl. Mekh. Tekh. Fiz., 51:4 (2010), 85–94
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Controlling a transonic flow around airfoils by means of energy supply with allowance for real properties of air
Prikl. Mekh. Tekh. Fiz., 51:3 (2010), 41–48
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Numerical design of multimodal axisymmetric hypersonic nozzles for wind tunnels
Prikl. Mekh. Tekh. Fiz., 51:2 (2010), 90–97
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Study of shells forced oscillations under effect of circumfluent flow
Mat. Model., 21:9 (2009), 121–128
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Aerodynamic characteristics of airfoils with energy supply
Prikl. Mekh. Tekh. Fiz., 50:5 (2009), 36–45
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Effect of one-sided unsteady energy supply on aerodynamic characteristics of airfoils in a transonic flow
Prikl. Mekh. Tekh. Fiz., 49:6 (2008), 82–87
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Effect of asymmetric pulsed periodic energy supply on aerodynamic characteristics of airfoils
Prikl. Mekh. Tekh. Fiz., 48:6 (2007), 70–76
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Nonlinear effects caused by pulsed periodic supply of energy in the vicinity of a symmetric airfoil in a transonic flow
Prikl. Mekh. Tekh. Fiz., 47:3 (2006), 64–71
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Controlling transonic flow around airfoils by means of local pulsed addition of energy
Prikl. Mekh. Tekh. Fiz., 45:5 (2004), 62–67
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Mathematical simulation of unsteady three-dimensional processes in the space gas dynamics
Num. Meth. Prog., 4:1 (2003), 294–322
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Experience of optimization of aerodynamic characteristics of airfoils
Prikl. Mekh. Tekh. Fiz., 43:1 (2002), 60–64
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Construction of surfaces by means of parametric polynomials
Zh. Vychisl. Mat. Mat. Fiz., 40:3 (2000), 356–364
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Construction of curves by means of parametric polynomials
Zh. Vychisl. Mat. Mat. Fiz., 38:12 (1998), 1967–1972
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A method of numerical integration for a system of ordinary differential equations with the use of the Hermitian interpolating polynomials
Zh. Vychisl. Mat. Mat. Fiz., 38:10 (1998), 1665–1670
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Application of the method of boundary elements and parametric polynomials in airfoil optimization problems
Prikl. Mekh. Tekh. Fiz., 38:2 (1997), 73–79
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Construction of plane curves by means of fourth-order parametric polynomials
Zh. Vychisl. Mat. Mat. Fiz., 35:7 (1995), 1139–1142
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Application of the boundary-element method to calculate subsonic flow around a profile
Prikl. Mekh. Tekh. Fiz., 34:5 (1993), 94–97
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Variational method of constructing subsonic airfoil profiles
Prikl. Mekh. Tekh. Fiz., 33:4 (1992), 90–93
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