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Lutsky Alexander Evgenjevich

Publications in Math-Net.Ru

  1. Numerical investigation of vortices generator influence on the supersonic flow around wing

    Matem. Mod., 36:4 (2024),  3–23
  2. Numerical simulation of 3D flow past an inlet model

    Matem. Mod., 36:3 (2024),  51–66
  3. 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.
  4. Comparison of turbulence models for a supersonic tip vortex simulation

    Keldysh Institute preprints, 2022, 071, 24 pp.
  5. Influence of porous wingtips on the formation of tip vortices

    Keldysh Institute preprints, 2022, 035, 16 pp.
  6. Investigation of vortex structures in supersonic flow around tandem wings

    Matem. Mod., 34:6 (2022),  92–110
  7. High-speed channel flow control with porous inserts

    Matem. Mod., 34:4 (2022),  100–112
  8. Calculation of high-speed flows based on a hyperbolic quasi-gas dynamic system

    Matem. Mod., 34:2 (2022),  17–31
  9. 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
  10. 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
  11. 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
  12. The influence of the acoustic type perturbations on three-dimensional transonic flow

    Keldysh Institute preprints, 2019, 135, 16 pp.
  13. Conservation laws and a compact quasi-gasdynamic system

    Matem. Mod., 31:12 (2019),  21–32
  14. Numerical simulation of recirculation flow during supersonic separation of moving bodies

    Matem. Mod., 31:9 (2019),  21–38
  15. 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.
  16. Simulation of supersonic flow in the wake behind a wing at $M=2$$4$

    Keldysh Institute preprints, 2018, 050, 19 pp.
  17. Numerical study of the flow around spacecraft model

    Keldysh Institute preprints, 2017, 130, 19 pp.
  18. 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.
  19. Quadrature-free WENO reconstruction on unstructured meshes

    Keldysh Institute preprints, 2017, 039, 26 pp.
  20. Active impact on the flow around hypersonic flying vehicles

    Keldysh Institute preprints, 2016, 137, 14 pp.
  21. Numerical simulation of shock waves interaction with boundary layers on adaptive grids

    Keldysh Institute preprints, 2016, 136, 15 pp.
  22. Numerical study of flow X-43 hypersonic aircraft using adaptive grids

    Keldysh Institute preprints, 2016, 102, 24 pp.
  23. 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.
  24. Numerical simulation of the pseudo-shock region formation in the channel

    Keldysh Institute preprints, 2016, 002, 24 pp.
  25. Numerical simulation of the wake influence on the flow around truncated cone

    Matem. Mod., 28:7 (2016),  45–55
  26. Algorithm of local mesh adaptation based on wavelet analysis with the use of free boundary method

    Keldysh Institute preprints, 2015, 094, 20 pp.
  27. Estimation of typical frequencies of pressure pulsations in a flow over a rectangular cavity

    Keldysh Institute preprints, 2015, 080, 24 pp.
  28. Numerical investigation of flow reconstruction features on a hammerhead cylinder-conic model

    Matem. Mod., 27:10 (2015),  65–80
  29. Numerical simulation of the energy deposition influence on the base flow

    Matem. Mod., 27:9 (2015),  33–48
  30. 3d problem of the flow around aircraft model with active influence on the flow

    Yakutian Mathematical Journal, 22:2 (2015),  83–91
  31. On technology of adaptive numerical simulations of gas dynamic flows based on wavelet analysis

    Keldysh Institute preprints, 2014, 110, 30 pp.
  32. Numerical simulation of supersonic flows in the wing wake and its interaction with crossing shock waves

    Keldysh Institute preprints, 2014, 098, 16 pp.
  33. The use of free boundary method for solving the problem of the flow past moving bodies

    Keldysh Institute preprints, 2014, 093, 16 pp.
  34. GridMan3D — a subroutine library for parallel computing on unstructured grids

    Keldysh Institute preprints, 2014, 078, 22 pp.
  35. Parallel implicit scheme implementation LU-SGS method for 3D turbulent flows

    Matem. Mod., 26:10 (2014),  64–78
  36. Numerical modeling of flow turbulization and relaminarization due to external active influence

    Matem. Mod., 26:3 (2014),  3–13
  37. The minimal realization of the wall functions method

    Keldysh Institute preprints, 2013, 038, 22 pp.
  38. 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.
  39. Localization of gas-dynamic fields singularities and adaptation of grid to the singularities position

    Matem. Mod., 24:12 (2012),  49–54
  40. Adapting of the code, simulating viscous fluids flows, to a hybrid computing systems based on CUDA-MPI

    Matem. Mod., 24:7 (2012),  33–44
  41. Simulation of a supersonic flowfield in the tip vortex core at Mach number of 6

    Matem. Mod., 24:6 (2012),  67–82
  42. Mathematical simulation of turbulent separated transonic flows about the bodies of revolution

    Matem. Mod., 23:5 (2011),  71–80
  43. Wavelet study of localised structures in the ideal and viscous models

    Matem. Mod., 23:1 (2011),  41–50
  44. Numerical simulation of separated transonic flow about the boat-tailed objects

    Keldysh Institute preprints, 2010, 007, 12 pp.
  45. Aerodynamic characteristics of a body of revolution with gas-permeable surface areas

    Prikl. Mekh. Tekh. Fiz., 51:1 (2010),  79–88
  46. Localised structures in the ideal and viscous models. Wavelet study

    Keldysh Institute preprints, 2009, 078, 10 pp.
  47. Multi-scale analysis of gas-dynamic fields singularities

    Keldysh Institute preprints, 2008, 098, 17 pp.
  48. Localization of singularities in gas-dynamic fields with the aid of wavelet analyses

    Matem. Mod., 20:7 (2008),  65–84
  49. Numerical studies of flow around aircraft using the multiprocessor computer systems

    Avtomat. i Telemekh., 2007, no. 5,  141–156
  50. An investigation of surface energy input to gas during initiation of a nanosecond distributed surface discharge

    TVT, 45:4 (2007),  580–587
  51. The evolution and interaction of channel flow discontinuities under the instant volume energy release influence

    Keldysh Institute preprints, 2005, 088
  52. The numerical analysis of viscous flows on the multiprocessor computers

    Keldysh Institute preprints, 2005, 035, 22 pp.
  53. The influence of viscosity to the parameters of supersonic flow over the wing section

    Keldysh Institute preprints, 2004, 026, 27 pp.
  54. Параллельные вычисления при решении современных задач науки и технологий

    Informatsionnye Tekhnologii i Vychslitel'nye Sistemy, 2003, no. 4,  14–22
  55. The Numerical Simulation Supersonic Flows over Complex Shaped Bodies

    Keldysh Institute preprints, 1999, 012
  56. The Numerical Simulation of Subsonic Flows over Shaped Bodies

    Keldysh Institute preprints, 1998, 022
  57. Numerical and Experimental Investigation of Supersonic Flow around Blunt Body at the Existence of the Longitudinal Discharge

    Keldysh Institute preprints, 1997, 027
  58. A Numerical Algorithm for Calculation of Compressible Inviscid Subsonic Flows about Flying Vehicles

    Keldysh Institute preprints, 1996, 105
  59. 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

  60. Aleksei Valerievich Zabrodin (1933–2008)

    Zh. Vychisl. Mat. Mat. Fiz., 49:7 (2009),  1340–1344


© Steklov Math. Inst. of RAS, 2024