Lutsky Alexander Evgenjevich

Publications in Math-Net.Ru

1. Flow and heat flux features for supersonic flow past aircraft model
   
   Mat. Model., 38:1 (2026),  174–190
2. Secondary vortices formation during the tip vortex interaction with the surface
   
   Pisma v Zhurnal Tekhnicheskoi Fiziki, 52:2 (2026),  51–54
3. About one kinetic model for describing turbulent flows taking into account heat transfer
   
   Dokl. RAN. Math. Inf. Proc. Upr., 525 (2025),  71–77
4. Using a kinetic model to find the pulsation moments of a turbulent flow
   
   Mat. Model., 37:2 (2025),  170–184
5. Description of turbulent flows using a kinetic model
   
   Dokl. RAN. Math. Inf. Proc. Upr., 516 (2024),  51–58
6. Vortex structures investigation in flow around delta wing
   
   Keldysh Institute preprints, 2024, 078, 20 pp.
7. Numerical investigation of vortices generator influence on the supersonic flow around wing
   
   Mat. Model., 36:4 (2024),  3–23
8. Numerical simulation of 3D flow past an inlet model
   
   Mat. Model., 36:3 (2024),  51–66
9. 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.
10. Comparison of turbulence models for a supersonic tip vortex simulation
    
    Keldysh Institute preprints, 2022, 071, 24 pp.
11. Influence of porous wingtips on the formation of tip vortices
    
    Keldysh Institute preprints, 2022, 035, 16 pp.
12. Investigation of vortex structures in supersonic flow around tandem wings
    
    Mat. Model., 34:6 (2022),  92–110
13. High-speed channel flow control with porous inserts
    
    Mat. Model., 34:4 (2022),  100–112
14. Calculation of high-speed flows based on a hyperbolic quasi-gas dynamic system
    
    Mat. Model., 34:2 (2022),  17–31
15. 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
16. 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
17. Numerical simulation of interaction and evolution of discontinuities in a channel based on a compact form of quasi-gasdynamic equations
    
    Mat. Model., 32:5 (2020),  44–58
18. The influence of the acoustic type perturbations on three-dimensional transonic flow
    
    Keldysh Institute preprints, 2019, 135, 16 pp.
19. Conservation laws and a compact quasi-gasdynamic system
    
    Mat. Model., 31:12 (2019),  21–32
20. Numerical simulation of recirculation flow during supersonic separation of moving bodies
    
    Mat. Model., 31:9 (2019),  21–38
21. 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.
22. Simulation of supersonic flow in the wake behind a wing at $M=2$–$4$
    
    Keldysh Institute preprints, 2018, 050, 19 pp.
23. Numerical study of the flow around spacecraft model
    
    Keldysh Institute preprints, 2017, 130, 19 pp.
24. 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.
25. Quadrature-free WENO reconstruction on unstructured meshes
    
    Keldysh Institute preprints, 2017, 039, 26 pp.
26. Active impact on the flow around hypersonic flying vehicles
    
    Keldysh Institute preprints, 2016, 137, 14 pp.
27. Numerical simulation of shock waves interaction with boundary layers on adaptive grids
    
    Keldysh Institute preprints, 2016, 136, 15 pp.
28. Numerical study of flow X-43 hypersonic aircraft using adaptive grids
    
    Keldysh Institute preprints, 2016, 102, 24 pp.
29. 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.
30. Numerical simulation of the pseudo-shock region formation in the channel
    
    Keldysh Institute preprints, 2016, 002, 24 pp.
31. Numerical simulation of the wake influence on the flow around truncated cone
    
    Mat. Model., 28:7 (2016),  45–55
32. Algorithm of local mesh adaptation based on wavelet analysis with the use of free boundary method
    
    Keldysh Institute preprints, 2015, 094, 20 pp.
33. Estimation of typical frequencies of pressure pulsations in a flow over a rectangular cavity
    
    Keldysh Institute preprints, 2015, 080, 24 pp.
34. Numerical investigation of flow reconstruction features on a hammerhead cylinder-conic model
    
    Mat. Model., 27:10 (2015),  65–80
35. Numerical simulation of the energy deposition influence on the base flow
    
    Mat. Model., 27:9 (2015),  33–48
36. 3d problem of the flow around aircraft model with active influence on the flow
    
    Yakutian Mathematical Journal, 22:2 (2015),  83–91
37. On technology of adaptive numerical simulations of gas dynamic flows based on wavelet analysis
    
    Keldysh Institute preprints, 2014, 110, 30 pp.
38. Numerical simulation of supersonic flows in the wing wake and its interaction with crossing shock waves
    
    Keldysh Institute preprints, 2014, 098, 16 pp.
39. The use of free boundary method for solving the problem of the flow past moving bodies
    
    Keldysh Institute preprints, 2014, 093, 16 pp.
40. GridMan3D — a subroutine library for parallel computing on unstructured grids
    
    Keldysh Institute preprints, 2014, 078, 22 pp.
41. Parallel implicit scheme implementation LU-SGS method for 3D turbulent flows
    
    Mat. Model., 26:10 (2014),  64–78
42. Numerical modeling of flow turbulization and relaminarization due to external active influence
    
    Mat. Model., 26:3 (2014),  3–13
43. The minimal realization of the wall functions method
    
    Keldysh Institute preprints, 2013, 038, 22 pp.
44. 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.
45. Localization of gas-dynamic fields singularities and adaptation of grid to the singularities position
    
    Mat. Model., 24:12 (2012),  49–54
46. Adapting of the code, simulating viscous fluids flows, to a hybrid computing systems based on CUDA-MPI
    
    Mat. Model., 24:7 (2012),  33–44
47. Simulation of a supersonic flowfield in the tip vortex core at Mach number of 6
    
    Mat. Model., 24:6 (2012),  67–82
48. Mathematical simulation of turbulent separated transonic flows about the bodies of revolution
    
    Mat. Model., 23:5 (2011),  71–80
49. Wavelet study of localised structures in the ideal and viscous models
    
    Mat. Model., 23:1 (2011),  41–50
50. Numerical simulation of separated transonic flow about the boat-tailed objects
    
    Keldysh Institute preprints, 2010, 007, 12 pp.
51. Energy deposition in boundary gas layer during initiation of nanosecond sliding surface discharge
    
    Pisma v Zhurnal Tekhnicheskoi Fiziki, 36:17 (2010),  35–41
52. Aerodynamic characteristics of a body of revolution with gas-permeable surface areas
    
    Prikl. Mekh. Tekh. Fiz., 51:1 (2010),  79–88
53. Localised structures in the ideal and viscous models. Wavelet study
    
    Keldysh Institute preprints, 2009, 078, 10 pp.
54. Multi-scale analysis of gas-dynamic fields singularities
    
    Keldysh Institute preprints, 2008, 098, 17 pp.
55. Localization of singularities in gas-dynamic fields with the aid of wavelet analyses
    
    Mat. Model., 20:7 (2008),  65–84
56. Numerical studies of flow around aircraft using the multiprocessor computer systems
    
    Avtomat. i Telemekh., 2007, no. 5,  141–156
57. An investigation of surface energy input to gas during initiation of a nanosecond distributed surface discharge
    
    TVT, 45:4 (2007),  580–587
58. The evolution and interaction of channel flow discontinuities under the instant volume energy release influence
    
    Keldysh Institute preprints, 2005, 088
59. The numerical analysis of viscous flows on the multiprocessor computers
    
    Keldysh Institute preprints, 2005, 035, 22 pp.
60. The influence of viscosity to the parameters of supersonic flow over the wing section
    
    Keldysh Institute preprints, 2004, 026, 27 pp.
61. Параллельные вычисления при решении современных задач науки и технологий
    
    Informatsionnye Tekhnologii i Vychslitel'nye Sistemy, 2003, no. 4,  14–22
62. The Numerical Simulation Supersonic Flows over Complex Shaped Bodies
    
    Keldysh Institute preprints, 1999, 012
63. The Numerical Simulation of Subsonic Flows over Shaped Bodies
    
    Keldysh Institute preprints, 1998, 022
64. Numerical and Experimental Investigation of Supersonic Flow around Blunt Body at the Existence of the Longitudinal Discharge
    
    Keldysh Institute preprints, 1997, 027
65. A Numerical Algorithm for Calculation of Compressible Inviscid Subsonic Flows about Flying Vehicles
    
    Keldysh Institute preprints, 1996, 105
66. 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


67. Aleksei Valerievich Zabrodin (1933–2008)
    
    Zh. Vychisl. Mat. Mat. Fiz., 49:7 (2009),  1340–1344