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Publications in Math-Net.Ru
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Numerical investigation of vortices generator influence on the supersonic flow around wing
Matem. Mod., 36:4 (2024), 3–23
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Numerical simulation of 3D flow past an inlet model
Matem. Mod., 36:3 (2024), 51–66
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The influence of the tip vortex from generator wing on the flow around the main wing at an attack angle
Keldysh Institute preprints, 2023, 032, 20 pp.
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Comparison of turbulence models for a supersonic tip vortex simulation
Keldysh Institute preprints, 2022, 071, 24 pp.
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Influence of porous wingtips on the formation of tip vortices
Keldysh Institute preprints, 2022, 035, 16 pp.
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Investigation of vortex structures in supersonic flow around tandem wings
Matem. Mod., 34:6 (2022), 92–110
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High-speed channel flow control with porous inserts
Matem. Mod., 34:4 (2022), 100–112
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Calculation of high-speed flows based on a hyperbolic quasi-gas dynamic system
Matem. Mod., 34:2 (2022), 17–31
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Numerical simulation of heat flux around a ballistic model based on the hyperbolic quasi-gasdynamic system of equations
Matem. Mod., 33:2 (2021), 41–54
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Limits for detailed description of problems in continuous media mechanics and numerical algorithm for viscous gas flow simulation
Dokl. RAN. Math. Inf. Proc. Upr., 493 (2020), 57–61
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Numerical simulation of interaction and evolution of discontinuities in a channel based on a compact form of quasi-gasdynamic equations
Matem. Mod., 32:5 (2020), 44–58
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The influence of the acoustic type perturbations on three-dimensional transonic flow
Keldysh Institute preprints, 2019, 135, 16 pp.
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Conservation laws and a compact quasi-gasdynamic system
Matem. Mod., 31:12 (2019), 21–32
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Numerical simulation of recirculation flow during supersonic separation of moving bodies
Matem. Mod., 31:9 (2019), 21–38
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Numerical investigation of the transonic flow around the above-caliber head part model of the carrier rocket taking into account acoustic disturbances in the flow
Keldysh Institute preprints, 2018, 264, 16 pp.
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Simulation of supersonic flow in the wake behind a wing at $M=2$–$4$
Keldysh Institute preprints, 2018, 050, 19 pp.
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Numerical study of the flow around spacecraft model
Keldysh Institute preprints, 2017, 130, 19 pp.
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Numerical simulation of a vortex wake behind a wing at a wide distance from the wing in supersonic flow
Keldysh Institute preprints, 2017, 095, 15 pp.
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Quadrature-free WENO reconstruction on unstructured meshes
Keldysh Institute preprints, 2017, 039, 26 pp.
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Active impact on the flow around hypersonic flying vehicles
Keldysh Institute preprints, 2016, 137, 14 pp.
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Numerical simulation of shock waves interaction with boundary layers on adaptive grids
Keldysh Institute preprints, 2016, 136, 15 pp.
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Numerical study of flow X-43 hypersonic aircraft using adaptive grids
Keldysh Institute preprints, 2016, 102, 24 pp.
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Simulation of transition between regular and Mach shock waves reflections by an implicit scheme based on the LU-SGS and BiCGStab methods
Keldysh Institute preprints, 2016, 068, 36 pp.
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Numerical simulation of the pseudo-shock region formation in the channel
Keldysh Institute preprints, 2016, 002, 24 pp.
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Numerical simulation of the wake influence on the flow around truncated cone
Matem. Mod., 28:7 (2016), 45–55
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Algorithm of local mesh adaptation based on wavelet analysis with the use of free boundary method
Keldysh Institute preprints, 2015, 094, 20 pp.
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Estimation of typical frequencies of pressure pulsations in a flow over a rectangular cavity
Keldysh Institute preprints, 2015, 080, 24 pp.
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Numerical investigation of flow reconstruction features on a hammerhead cylinder-conic model
Matem. Mod., 27:10 (2015), 65–80
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Numerical simulation of the energy deposition influence on the base flow
Matem. Mod., 27:9 (2015), 33–48
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3d problem of the flow around aircraft model with active influence on the flow
Yakutian Mathematical Journal, 22:2 (2015), 83–91
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On technology of adaptive numerical simulations of gas dynamic flows based on wavelet analysis
Keldysh Institute preprints, 2014, 110, 30 pp.
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Numerical simulation of supersonic flows in the wing wake and its interaction with crossing shock waves
Keldysh Institute preprints, 2014, 098, 16 pp.
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The use of free boundary method for solving the problem of the flow past moving bodies
Keldysh Institute preprints, 2014, 093, 16 pp.
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GridMan3D — a subroutine library for parallel computing on unstructured grids
Keldysh Institute preprints, 2014, 078, 22 pp.
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Parallel implicit scheme implementation LU-SGS method for 3D turbulent flows
Matem. Mod., 26:10 (2014), 64–78
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Numerical modeling of flow turbulization and relaminarization due to external active influence
Matem. Mod., 26:3 (2014), 3–13
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The minimal realization of the wall functions method
Keldysh Institute preprints, 2013, 038, 22 pp.
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Wavelet analysis application for the localization of structures in the calculations for ideal and viscous models and for the grids adaptation
Keldysh Institute preprints, 2012, 045, 24 pp.
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Localization of gas-dynamic fields singularities and adaptation of grid to the singularities position
Matem. Mod., 24:12 (2012), 49–54
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Adapting of the code, simulating viscous fluids flows, to a hybrid computing systems based on CUDA-MPI
Matem. Mod., 24:7 (2012), 33–44
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Simulation of a supersonic flowfield in the tip vortex core at Mach number of 6
Matem. Mod., 24:6 (2012), 67–82
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Mathematical simulation of turbulent separated transonic flows about the bodies of revolution
Matem. Mod., 23:5 (2011), 71–80
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Wavelet study of localised structures in the ideal and viscous models
Matem. Mod., 23:1 (2011), 41–50
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Numerical simulation of separated transonic flow about the boat-tailed objects
Keldysh Institute preprints, 2010, 007, 12 pp.
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Aerodynamic characteristics of a body of revolution with gas-permeable surface areas
Prikl. Mekh. Tekh. Fiz., 51:1 (2010), 79–88
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Localised structures in the ideal and viscous models. Wavelet study
Keldysh Institute preprints, 2009, 078, 10 pp.
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Multi-scale analysis of gas-dynamic fields singularities
Keldysh Institute preprints, 2008, 098, 17 pp.
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Localization of singularities in gas-dynamic fields with the aid of wavelet analyses
Matem. Mod., 20:7 (2008), 65–84
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Numerical studies of flow around aircraft using the multiprocessor computer systems
Avtomat. i Telemekh., 2007, no. 5, 141–156
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An investigation of surface energy input to gas during initiation of a nanosecond distributed surface discharge
TVT, 45:4 (2007), 580–587
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The evolution and interaction of channel flow discontinuities under the instant volume energy release influence
Keldysh Institute preprints, 2005, 088
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The numerical analysis of viscous flows on the multiprocessor computers
Keldysh Institute preprints, 2005, 035, 22 pp.
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The influence of viscosity to the parameters of supersonic flow over the wing section
Keldysh Institute preprints, 2004, 026, 27 pp.
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Параллельные вычисления при решении современных задач науки и технологий
Informatsionnye Tekhnologii i Vychslitel'nye Sistemy, 2003, no. 4, 14–22
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The Numerical Simulation Supersonic Flows over Complex Shaped Bodies
Keldysh Institute preprints, 1999, 012
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The Numerical Simulation of Subsonic Flows over Shaped Bodies
Keldysh Institute preprints, 1998, 022
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Numerical and Experimental Investigation of Supersonic Flow around Blunt Body at the Existence of the Longitudinal Discharge
Keldysh Institute preprints, 1997, 027
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A Numerical Algorithm for Calculation of Compressible Inviscid Subsonic Flows about Flying Vehicles
Keldysh Institute preprints, 1996, 105
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Numerical and Experimental Investigation of Supersonic Flow Around Blunt Body with the Needle-Eletrode in Front of It and in the Presence of Electric Discharge
Keldysh Institute preprints, 1995, 019
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Aleksei Valerievich Zabrodin (1933–2008)
Zh. Vychisl. Mat. Mat. Fiz., 49:7 (2009), 1340–1344
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