Sidorenko Andrei Anatol'evich

Publications in Math-Net.Ru

1. A method for constructing a complete bifurcation picture of a boundary value problem for nonlinear partial differential equations: application of the Kolmogorov-Arnold theorem
   
   Izvestiya VUZ. Applied Nonlinear Dynamics, 33:4 (2025),  435–465
2. Influence of a jet vortex generator on a turbulent boundary layer. 1. Reynolds stresses
   
   Prikl. Mekh. Tekh. Fiz., 66:4 (2025),  74–91
3. Evolution of disturbances generated by a heat source in a supersonic boundary layer during shock wave interaction
   
   Prikl. Mekh. Tekh. Fiz., 66:2 (2025),  42–54
4. Investigations of shock wave boundary layer interaction by panoramic methods
   
   Prikl. Mekh. Tekh. Fiz., 66:2 (2025),  29–41
5. Comparison of the results of RANS- and ILES-based calculations for a thick dropd-shaped profile at low Reynolds numbers
   
   Prikl. Mekh. Tekh. Fiz., 65:2 (2024),  62–80
6. 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
7. Numerical simulation of the development of perturbations induced by a periodic heat source in a supersonic boundary layer
   
   Prikl. Mekh. Tekh. Fiz., 64:5 (2023),  139–143
8. Problems of flow separation detection by pressure sensors on a unmanned aerial vehicles with a propeller
   
   Pisma v Zhurnal Tekhnicheskoi Fiziki, 48:3 (2022),  40–43
9. Problem of using the PIV-method for measurements in thin high-velocity shear layers
   
   Prikl. Mekh. Tekh. Fiz., 61:5 (2020),  77–87
10. Investigation of various approaches to the modeling of laminar-turbulent transition in compressible separated flows
    
    Prikl. Mekh. Tekh. Fiz., 61:5 (2020),  40–51
11. Suppressing a laminar flow separation zone by spark discharge at Mach number M = 1.43
    
    Pisma v Zhurnal Tekhnicheskoi Fiziki, 44:18 (2018),  60–68
12. Nonstationary phenomena in the region of shock-wave interaction with a boundary layer at transonic flow velocities
    
    Pisma v Zhurnal Tekhnicheskoi Fiziki, 43:12 (2017),  59–67
13. 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
14. 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
15. Comparison of flows induced by a dielectric barrier discharge and a sliding discharge
    
    Prikl. Mekh. Tekh. Fiz., 54:3 (2013),  21–29
16. Investigation of a nonstationary flow field generated by a dielectric barrier discharge
    
    Zhurnal Tekhnicheskoi Fiziki, 82:4 (2012),  31–41
17. Nonstationary flow field generated by dielectric barrier discharge
    
    Pisma v Zhurnal Tekhnicheskoi Fiziki, 37:10 (2011),  33–41
18. Electric discharge control of flow separation on oblique airfoil
    
    Pisma v Zhurnal Tekhnicheskoi Fiziki, 36:7 (2010),  22–30
19. Correlations study in shock wave/turbulent boundary layer interaction
    
    Pisma v Zhurnal Tekhnicheskoi Fiziki, 36:3 (2010),  23–30
20. Control of the vortex flow around a cone with a spark discharge
    
    Prikl. Mekh. Tekh. Fiz., 51:2 (2010),  81–89
21. 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
22. Development of natural disturbances in a hypersonic boundary layer on a sharp cone
    
    Prikl. Mekh. Tekh. Fiz., 42:1 (2001),  65–71
23. An experimental investigation of natural disturbances in a hypersonic boundary layer on a flat plate
    
    Prikl. Mekh. Tekh. Fiz., 38:1 (1997),  71–75