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Publications in Math-Net.Ru
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Optimal aerodynamic design of a wing-body configuration for a wide-body long-range aircraft
Vestn. Tomsk. Gos. Univ. Mat. Mekh., 2020, no. 63, 115–124
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Investigation of the stability of optimal aerodynamic designing of the three-dimensional wing-fuselage layout for a wide-body long-range aircraft with regard to its initial shape
Vestn. Tomsk. Gos. Univ. Mat. Mekh., 2019, no. 62, 79–90
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The stability of the optimal aerodynamic design of an isolated three-dimensional wing to its initial form
Zhurnal Tekhnicheskoi Fiziki, 88:12 (2018), 1793–1800
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An optimal aerodynamic design for the wing of a wide-body long-range aircraft
Vestn. Tomsk. Gos. Univ. Mat. Mekh., 2018, no. 51, 117–129
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An optimal design technology for aerodynamic configurations based on the numerical solutions of the full Navier–Stokes equations
Vestn. Tomsk. Gos. Univ. Mat. Mekh., 2017, no. 50, 90–98
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Computational technology for optimal automatic design of aerodynamic shapes
Matem. Mod., 27:2 (2015), 96–114
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Effective implementation of nonlinear constraints in optimization of three-dimensional transonic wings
Vestn. Tomsk. Gos. Univ. Mat. Mekh., 2015, no. 1(33), 72–81
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Nonequilibrium air flow at 3d parabolic viscous shock layer with vibrational relaxation
Matem. Mod., 12:10 (2000), 61–76
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Optimization of the Earth reentry trajectory of a blunted body by the integral heat flux
Prikl. Mekh. Tekh. Fiz., 41:4 (2000), 112–123
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Numerical investigation of supersonic flow past blunt bodies of intricate shape at an angle of attack and slip angle
TVT, 38:3 (2000), 468–476
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Heat transfer in a three-dimensional parabolized viscous shock layer in the vicinity of blunt bodies subjected to flow at angles of incidence and slip
TVT, 37:5 (1999), 765–771
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Optimization of the shape of bluntness of a body for convective heat flow within the framework of laminar boundary layer equations
TVT, 37:1 (1999), 92–97
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Numerical solution of the equations of three-dimensional viscous shock layer in the vicinity of blunt bodies placed in a stream at the angle of attack
Zh. Vychisl. Mat. Mat. Fiz., 39:7 (1999), 1226–1235
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Calculations for 3D boundary layer by high accuracy finite-difference method
Matem. Mod., 10:10 (1998), 79–86
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Application of genetic algorithms for heat flux optimization problem
Matem. Mod., 10:9 (1998), 111–122
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High accuracy finite-difference method for boundary layer equations
Matem. Mod., 10:4 (1998), 70–82
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Determination of the catalytic activity of materials by solving the equations of a nonequilibrium multicomponent boundary layer on a flat plate
Prikl. Mekh. Tekh. Fiz., 39:4 (1998), 110–117
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Numerical simulation of two-dimensional nonequilibrium supersonic flows within the model of viscous shock layer
TVT, 36:5 (1998), 776–784
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Solution of the equations of a nonequilibrium viscous shock layer for blunt bodies with catalytic surfaces
Zh. Vychisl. Mat. Mat. Fiz., 38:5 (1998), 860–869
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Calculation of three-dimensional turbulent boundary-layer flows on a network of different-power computers
Zh. Vychisl. Mat. Mat. Fiz., 38:3 (1998), 510–519
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Simulation of multi-component flows with chemical reactions in the model of parabolized viscous shock layer
Matem. Mod., 8:10 (1996), 3–14
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Numerical simulation of 3D nonequilibrium flows at viscous shock layer
Matem. Mod., 8:5 (1996), 63–75
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A study in three-dimensional flow of a viscous gas within the framework of parabolic flow models
TVT, 34:3 (1996), 429–435
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Numerical investigation of supersonic flow around blunt bodies in the model of a viscous shock layer
Zh. Vychisl. Mat. Mat. Fiz., 36:8 (1996), 158–168
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Simulation of flow in threedimensional viscous shock layer on distributed memory multiprocessor system
Matem. Mod., 5:7 (1993), 41–48
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Threedimensional gas flow past blunt bodies in the framework of the parabolic viscous shock layer theory
Matem. Mod., 5:1 (1993), 16–25
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Model of a parabolized, viscous shock layer for the investigation of a three-dimensional, hypersonic flow of viscous gas past a body
TVT, 31:6 (1993), 925–933
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Investigation of three-dimensional hypersonic flow of chemically nonequilibrium viscous gas past a sharp cone
TVT, 31:5 (1993), 780–786
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Method of global iterations for solving the three-dimensional equations of a viscous shock layer
TVT, 30:6 (1992), 1124–1129
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Three-dimensional, nonuniform, hypersonic viscous gas flow around blunt bodies
TVT, 30:1 (1992), 116–121
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Hypersonic flow of a viscous gas past pointed elliptical cones at angles of attack and yaw
TVT, 29:6 (1991), 1157–1163
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Spatial thin viscous shock layer in non-homogeneous gas flow in the absence of symmetry planes
Matem. Mod., 1:11 (1989), 51–57
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Numerical modelling of chemically non-equilibrium flows in spatial viscous shock layer around bodies with catalytic surface
Matem. Mod., 1:8 (1989), 12–21
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Supersonic nonuniform gas flow around elongated axisymmetric bodies
Prikl. Mekh. Tekh. Fiz., 30:5 (1989), 60–65
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Investigation of swirling flow of a viscous gas near the stagnation line of a blunt body
Prikl. Mekh. Tekh. Fiz., 29:5 (1988), 52–58
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$3$-dimensional multicomponent viscous shock layer on a catalytic surface near a critical-point
TVT, 26:5 (1988), 901–908
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Hypersonic $3$-dimensional viscous shock layer on blunt bodies at angles of pitch and yaw
TVT, 26:4 (1988), 751–758
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Unsteady three-dimensional laminar boundary layer on blunt bodies with strong blowing
Prikl. Mekh. Tekh. Fiz., 28:6 (1987), 50–56
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$3$-dimensional boundary-layer on blunt bodies with a permeable surface at angles of attack and yaw to a stream
TVT, 25:3 (1987), 509–516
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Higher order numerical approximation method for the solution of two-dimensional boundary layer problems
Zh. Vychisl. Mat. Mat. Fiz., 27:6 (1987), 952–953
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$3$-dimensional multicomponent boundary-layer on a catalytic surface near the critical-point
TVT, 23:3 (1985), 513–521
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Numerical solution of the equations of a three-dimensional mixing
layer
Zh. Vychisl. Mat. Mat. Fiz., 24:1 (1984), 132–139
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$3$-dimensional laminar boundary-layer in the symmetry planes of blunt bodies with large injection
TVT, 19:3 (1981), 566–576
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Space viscous schock layer in flows with angles of attack past sharp cones
Matem. Mod., 3:1 (1991), 3–10
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