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Publications in Math-Net.Ru
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Numerical simulation of heat flux around a ballistic model based on the hyperbolic quasi-gasdynamic system of equations
Mat. Model., 33:2 (2021), 41–54
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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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Algorithm for multilevel mesh adaptation with waveled-based criteria for gas dynamic problems
Keldysh Institute preprints, 2015, 097, 22 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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Parallel implicit scheme implementation LU-SGS method for 3D turbulent flows
Mat. Model., 26:10 (2014), 64–78
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Scalability of CFD-applications on hybrid computing systems
Informatsionnye Tekhnologii i Vychslitel'nye Sistemy, 2013, no. 2, 23–26
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The hybrid supercomputer K-100: what will come next?
Informatsionnye Tekhnologii i Vychslitel'nye Sistemy, 2012, no. 2, 29–35
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Simulation of a supersonic flowfield in the tip vortex core at Mach number of 6
Mat. Model., 24:6 (2012), 67–82
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The investigation of damping of the spacecraft’s angular rates in the off-optimum situation
Keldysh Institute preprints, 2011, 070, 20 pp.
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Numerical simulation of aero- and gasdynamic problems on the hybrid supercomputer “MVS-EXPRESS”
Mat. Model., 22:4 (2010), 90–98
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Simulating flows of incompressible and weakly compressible fluids on multicore hybrid computer systems
Zh. Vychisl. Mat. Mat. Fiz., 50:12 (2010), 2275–2284
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Reconstruction of attitude motion of the small spacecraft by measurements of the current from solar arrays
Keldysh Institute preprints, 2009, 032, 26 pp.
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Reconstruction of the spacecraft Monitor-E attitude motion by measurements of the current from solar arrays
Keldysh Institute preprints, 2008, 085, 27 pp.
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Use of jet engines for orbiral movement control of a spacecraft, simultaneously with dumping the momentum of electromechanical actuators
Keldysh Institute preprints, 2006, 082, 21 pp.
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The analysis of dynamic capabilities of the control systems by the spacecraft built on the basis of the reaction wheels
Keldysh Institute preprints, 2005, 047
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In memory of Arkady Viktorovich Kryazhimskiy (1949-2014)
Ural Math. J., 2:2 (2016), 3–15
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