RUS  ENG
Full version
PEOPLE

Maslov Anatolii Aleksandrovich

Publications in Math-Net.Ru

  1. Similarity parameter for the drag coefficient of a cylinder with a high-porosity frontal insert aligned at an angle of attack in a supersonic flow

    Prikl. Mekh. Tekh. Fiz., 63:6 (2022),  82–90
  2. Numerical simulation of the flow in a sensor for measuring the flow stagnation temperature in pulsed aerodynamic installations

    Prikl. Mekh. Tekh. Fiz., 63:3 (2022),  75–87
  3. Physical and mathematical modeling of a supersonic flow around bodies with gas-permeable porous inserts at an angle of attack

    Prikl. Mekh. Tekh. Fiz., 61:5 (2020),  14–20
  4. A similarity criterion for supersonic flow past a cylinder with a frontal high-porosity cellular insert

    Pisma v Zhurnal Tekhnicheskoi Fiziki, 44:6 (2018),  3–10
  5. The effect of temperature of a cone nose-tip on the spectra of disturbances in the hypersound boundary layer

    Pisma v Zhurnal Tekhnicheskoi Fiziki, 43:20 (2017),  12–19
  6. An experimental study of subsonic microjets escaping from a flat nozzle

    Pisma v Zhurnal Tekhnicheskoi Fiziki, 43:14 (2017),  3–9
  7. Analysis of the development of perturbations in a hypersonic boundary layer behind a wavy surface

    Pisma v Zhurnal Tekhnicheskoi Fiziki, 43:13 (2017),  65–72
  8. Turbulization of the wake behind a single roughness element on a blunted body at a hypersonic Mach number

    Prikl. Mekh. Tekh. Fiz., 58:5 (2017),  102–110
  9. Influence of vibrational relaxation on perturbations in a shock layer on a plate

    Zhurnal Tekhnicheskoi Fiziki, 85:5 (2015),  12–22
  10. The influence of the laminar–turbulent transition on the interaction between the shock wave and boundary layer at a low supersonic Mach number

    Pisma v Zhurnal Tekhnicheskoi Fiziki, 41:19 (2015),  29–37
  11. An experimental study of the structure of supersonic flat underexpanded microjets

    Pisma v Zhurnal Tekhnicheskoi Fiziki, 41:10 (2015),  97–103
  12. The efficiency of the method of sound-absorbing coatings in vibrationally excited hypersonic flow

    Pisma v Zhurnal Tekhnicheskoi Fiziki, 41:4 (2015),  61–67
  13. Engineering modeling of the laminar–turbulent transition: Achievements and problems (Review)

    Prikl. Mekh. Tekh. Fiz., 56:5 (2015),  30–49
  14. Modeling of a supersonic flow around a cylinder with a gas-permeable porous insert

    Prikl. Mekh. Tekh. Fiz., 56:4 (2015),  12–22
  15. Controlling aerodynamic forces with the aid of gas-permeable porous materials

    Pisma v Zhurnal Tekhnicheskoi Fiziki, 40:19 (2014),  83–88
  16. Relaminarization in supersonic microjets at low Reynolds numbers

    Pisma v Zhurnal Tekhnicheskoi Fiziki, 39:16 (2013),  47–54
  17. Comparison of flows induced by a dielectric barrier discharge and a sliding discharge

    Prikl. Mekh. Tekh. Fiz., 54:3 (2013),  21–29
  18. Investigation of a nonstationary flow field generated by a dielectric barrier discharge

    Zhurnal Tekhnicheskoi Fiziki, 82:4 (2012),  31–41
  19. Stability of a subsonic gas microjet

    Zhurnal Tekhnicheskoi Fiziki, 82:2 (2012),  17–23
  20. Internal pressure measurements in microchannels of different shapes

    Nanosystems: Physics, Chemistry, Mathematics, 3:2 (2012),  37–46
  21. Short-duration wind tunnel with combined heating and stabilization of parameters

    Prikl. Mekh. Tekh. Fiz., 53:6 (2012),  3–10
  22. Experimental verification of the method of calculating the flow parameters in the test section of the hotshot wind tunnel

    Prikl. Mekh. Tekh. Fiz., 53:5 (2012),  79–89
  23. Effect of sound-absorbing materials on intensity of disturbances in the shock layer on a flat plate aligned at an angle of attack

    Prikl. Mekh. Tekh. Fiz., 53:2 (2012),  21–32
  24. Bispectral analysis of numerical simulations of wave processes in hypersonic shock layers

    Prikl. Mekh. Tekh. Fiz., 53:1 (2012),  3–11
  25. Effect of nozzle size on supersonic microjet length

    Pisma v Zhurnal Tekhnicheskoi Fiziki, 37:22 (2011),  10–15
  26. Nonstationary flow field generated by dielectric barrier discharge

    Pisma v Zhurnal Tekhnicheskoi Fiziki, 37:10 (2011),  33–41
  27. Experimental determination of the friction factor coefficient in microchannels

    Prikl. Mekh. Tekh. Fiz., 52:1 (2011),  24–30
  28. Electric discharge control of flow separation on oblique airfoil

    Pisma v Zhurnal Tekhnicheskoi Fiziki, 36:7 (2010),  22–30
  29. Correlations study in shock wave/turbulent boundary layer interaction

    Pisma v Zhurnal Tekhnicheskoi Fiziki, 36:3 (2010),  23–30
  30. Wave processes in the shock layer on a flat plate at an angle of attack

    Prikl. Mekh. Tekh. Fiz., 51:4 (2010),  39–47
  31. Control of the vortex flow around a cone with a spark discharge

    Prikl. Mekh. Tekh. Fiz., 51:2 (2010),  81–89
  32. Effect of streamwise structures on heat transfer in a hypersonic flow in a compression corner

    Prikl. Mekh. Tekh. Fiz., 50:4 (2009),  112–120
  33. Generation and registration of disturbances in a gas flow. 2. Experiments with arrays of tubular microheaters and microsensors

    Prikl. Mekh. Tekh. Fiz., 50:3 (2009),  112–117
  34. Generation and registration of disturbances in a gas flow. 1. Formation of arrays of tubular microheaters and microsensors

    Prikl. Mekh. Tekh. Fiz., 50:2 (2009),  145–151
  35. Numerical simulation of receptivity of a hypersonic boundary layer to acoustic disturbances

    Prikl. Mekh. Tekh. Fiz., 48:3 (2007),  84–91
  36. Effect of porous coatings on stability of hypersonic boundary layers

    Prikl. Mekh. Tekh. Fiz., 45:2 (2004),  169–176
  37. Nonlinear mechanisms of the initial stage of the laminar–turbulent transition at hypersonic velocities

    Prikl. Mekh. Tekh. Fiz., 44:5 (2003),  64–71
  38. Experimental and numerical study of a hypersonic separated flow in the vicinity of a cone-flare model

    Prikl. Mekh. Tekh. Fiz., 43:6 (2002),  100–112
  39. Experimental study of stability of strongly underexpanded laminar free and impact jets

    Prikl. Mekh. Tekh. Fiz., 42:6 (2001),  39–46
  40. Flow regimes formed by a counterflow jet in a supersonic flow

    Prikl. Mekh. Tekh. Fiz., 42:5 (2001),  27–36
  41. Investigation of aerodynamic heating of a plate in a viscous hypersonic flow

    TVT, 37:3 (1999),  415–419
  42. The effect of the angle of attack on hypersonic flow on a plate

    TVT, 36:5 (1998),  754–760
  43. An experimental investigation of natural disturbances in a hypersonic boundary layer on a flat plate

    Prikl. Mekh. Tekh. Fiz., 38:1 (1997),  71–75
  44. An experimental study of generation of unstable disturbances on the leading edge of a plate at $\mathrm{M}=2$

    Prikl. Mekh. Tekh. Fiz., 38:1 (1997),  51–57
  45. An experimental investigation of supersonic boundary layer receptivity

    Dokl. Akad. Nauk, 350:3 (1996),  335–337
  46. An experimental study of density fluctuations in the hypersonic boundary layer on a flat plate

    Prikl. Mekh. Tekh. Fiz., 37:6 (1996),  51–60
  47. Hypersonic flow on a flat plate. Experimental results and numerical modeling

    Prikl. Mekh. Tekh. Fiz., 36:6 (1995),  60–67
  48. Aerodynamic characteristics of a delta wing in hypersonic flow

    Prikl. Mekh. Tekh. Fiz., 35:2 (1994),  66–69
  49. Influence of a fan of rarefaction waves on the development of a disturbance in a supersonic boundary layer

    Prikl. Mekh. Tekh. Fiz., 33:2 (1992),  52–55
  50. Wave structure of artificial perturbations in a supersonic boundary layer on a plate

    Prikl. Mekh. Tekh. Fiz., 31:2 (1990),  95–98
  51. Stability of a supersonic boundary layer behind a fan of rarefaction waves

    Prikl. Mekh. Tekh. Fiz., 30:3 (1989),  113–117
  52. Experimental study of the influence of blunt leading edge of a flat plate on the growth of three-dimensional waves in supersonic flow

    Prikl. Mekh. Tekh. Fiz., 28:2 (1987),  53–56
  53. Experimental investigation of the wave structure of a supersonic boundary layer

    Prikl. Mekh. Tekh. Fiz., 27:5 (1986),  107–112
  54. Effects of cooling on supersonic boundary-layer stability

    Dokl. Akad. Nauk SSSR, 264:6 (1982),  1318–1321
  55. Development of small perturbations in a slightly nonparallel supersonic flow

    Prikl. Mekh. Tekh. Fiz., 23:3 (1982),  98–102
  56. Laminar-turbulent transition of supersonic boundary layer on a cooled surface

    Prikl. Mekh. Tekh. Fiz., 22:3 (1981),  30–36
  57. Stability of a supersonic boundary layer with respect to three-dimensional disturbances

    Prikl. Mekh. Tekh. Fiz., 15:1 (1974),  37–41
  58. Numerical investigation of stability of a supersonic laminar boundary layer

    Prikl. Mekh. Tekh. Fiz., 13:5 (1972),  181–184
  59. Numerical and asymptotic solution of the problem concerning the complete stabilization of a boundary layer

    Prikl. Mekh. Tekh. Fiz., 13:3 (1972),  60–64
  60. Numerical solution to the problem of the complete stabilization of a supersonic boundary layer

    Prikl. Mekh. Tekh. Fiz., 13:2 (1972),  39–43

© Steklov Math. Inst. of RAS, 2026