Polivanov Pavel Aleksandrovich

Publications in Math-Net.Ru

1. Influence of a jet vortex generator on a turbulent boundary layer. 1. Reynolds stresses
   
   Prikl. Mekh. Tekh. Fiz., 66:4 (2025),  74–91
2. Investigation of the laminar-turbulent transition with the use of a surface hot-wire probe
   
   Prikl. Mekh. Tekh. Fiz., 65:4 (2024),  41–51
3. Surface sensors of thermal anemometer used to analyze PIV data
   
   Prikl. Mekh. Tekh. Fiz., 65:2 (2024),  110–114
4. 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
5. 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
6. Numerical and experimental study of the effect of blowing/suction through a perforated surface on the boundary layer at a supersonic Mach number
   
   Pisma v Zhurnal Tekhnicheskoi Fiziki, 47:21 (2021),  19–23
7. Problem of using the PIV-method for measurements in thin high-velocity shear layers
   
   Prikl. Mekh. Tekh. Fiz., 61:5 (2020),  77–87
8. Investigation of various approaches to the modeling of laminar-turbulent transition in compressible separated flows
   
   Prikl. Mekh. Tekh. Fiz., 61:5 (2020),  40–51
9. 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
10. 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
11. 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
12. 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
13. Comparison of flows induced by a dielectric barrier discharge and a sliding discharge
    
    Prikl. Mekh. Tekh. Fiz., 54:3 (2013),  21–29
14. Investigation of a nonstationary flow field generated by a dielectric barrier discharge
    
    Zhurnal Tekhnicheskoi Fiziki, 82:4 (2012),  31–41
15. 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
16. Nonstationary flow field generated by dielectric barrier discharge
    
    Pisma v Zhurnal Tekhnicheskoi Fiziki, 37:10 (2011),  33–41
17. Correlations study in shock wave/turbulent boundary layer interaction
    
    Pisma v Zhurnal Tekhnicheskoi Fiziki, 36:3 (2010),  23–30