Shiplyuk Aleksandr Nikolaevich

Publications in Math-Net.Ru

1. Numerical investigation of the effect of tangential helium injection on the linear stability of a compressible boundary layer on a flat plate
   
   Zhurnal Tekhnicheskoi Fiziki, 95:7 (2025),  1263–1270
2. Description of a small climatic wind tunnel based at the Khristianovich Institute of Theoretical and Applied Mechanics of the Siberian Branch of the Russian Academy of Sciences
   
   Prikl. Mekh. Tekh. Fiz., 64:6 (2023),  85–96
3. Investigations of high-speed boundary layer stabilization by using porous coatings (review)
   
   Prikl. Mekh. Tekh. Fiz., 64:4 (2023),  27–45
4. Experimental study of the effect of a passive porous coating on disturbances in a hypersonic boundary layer. 2. Effect of the porous coating position
   
   Prikl. Mekh. Tekh. Fiz., 57:5 (2016),  127–133
5. Experimental study of the effect of a passive porous coating on disturbances in a hypersonic boundary layer. 1. Effect of the porous coating length
   
   Prikl. Mekh. Tekh. Fiz., 54:4 (2013),  68–73
6. Experimental study of the influence of parameters of a passive porous coating on the development of disturbances in a hypersonic boundary layer
   
   Pisma v Zhurnal Tekhnicheskoi Fiziki, 38:23 (2012),  83–88
7. Numerical design of multimodal axisymmetric hypersonic nozzles for wind tunnels
   
   Prikl. Mekh. Tekh. Fiz., 51:2 (2010),  90–97
8. 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
9. Effect of porous coatings on stability of hypersonic boundary layers
   
   Prikl. Mekh. Tekh. Fiz., 45:2 (2004),  169–176
10. Nonlinear mechanisms of the initial stage of the laminar–turbulent transition at hypersonic velocities
    
    Prikl. Mekh. Tekh. Fiz., 44:5 (2003),  64–71
11. Optimal method for heat-flow registration
    
    Prikl. Mekh. Tekh. Fiz., 44:4 (2003),  174–184
12. 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
13. Relaminarization of a turbulent boundary layer with a Mach number $\mathrm{M}_\infty=4$
    
    Prikl. Mekh. Tekh. Fiz., 43:1 (2002),  91–99
14. Experimental investigation of stability of a hypersonic boundary layer on a cone–flare model
    
    Prikl. Mekh. Tekh. Fiz., 42:4 (2001),  31–39
15. Development of natural disturbances in a hypersonic boundary layer on a sharp cone
    
    Prikl. Mekh. Tekh. Fiz., 42:1 (2001),  65–71
16. Investigation of aerodynamic heating of a plate in a viscous hypersonic flow
    
    TVT, 37:3 (1999),  415–419
17. An experimental investigation of natural disturbances in a hypersonic boundary layer on a flat plate
    
    Prikl. Mekh. Tekh. Fiz., 38:1 (1997),  71–75
18. An experimental study of density fluctuations in the hypersonic boundary layer on a flat plate
    
    Prikl. Mekh. Tekh. Fiz., 37:6 (1996),  51–60
19. Hypersonic flow on a flat plate. Experimental results and numerical modeling
    
    Prikl. Mekh. Tekh. Fiz., 36:6 (1995),  60–67
20. Aerodynamic characteristics of a delta wing in hypersonic flow
    
    Prikl. Mekh. Tekh. Fiz., 35:2 (1994),  66–69