Poplavskaya Tat'yana Vladimirovna

Publications in Math-Net.Ru

1. Effect of the jet pressure ratio in supersonic axisymmetric jets of a polyatomic gas SF$_6$ on their gas-dynamic structure
   
   Prikl. Mekh. Tekh. Fiz., 65:1 (2024),  47–57
2. Computational grids for engineering modeling of the laminar–turbulent flow
   
   Prikl. Mekh. Tekh. Fiz., 63:6 (2022),  91–95
3. 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
4. Controlling the aerodynamic drag of a cylinder with gas-permeable porous inserts by regulating base pressure
   
   Pisma v Zhurnal Tekhnicheskoi Fiziki, 47:8 (2021),  41–43
5. Determination of threshold $N$-factors of the laminar-turbulent transition in a subsonic boundary layer on a prolate spheroid
   
   Prikl. Mekh. Tekh. Fiz., 62:6 (2021),  3–7
6. Thermal methods of drag control for cylindrical bodies with porous inserts in a supersonic flow
   
   Prikl. Mekh. Tekh. Fiz., 62:2 (2021),  5–16
7. 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
8. Numerical study of the evolution of disturbances generated by roughness elements in a supersonic boundary layer on a blunted cone
   
   Prikl. Mekh. Tekh. Fiz., 60:3 (2019),  45–59
9. 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
10. Coefficients of transformation of long-wavelength perturbations of a supersonic incident flow around a wedge into pressure fluctuations on its surface
    
    Pisma v Zhurnal Tekhnicheskoi Fiziki, 42:21 (2016),  70–78
11. A numerical study of non-equilibrium flows with different vibrational relaxation models
    
    Pisma v Zhurnal Tekhnicheskoi Fiziki, 42:13 (2016),  72–79
12. Engineering modeling of the laminar–turbulent transition: Achievements and problems (Review)
    
    Prikl. Mekh. Tekh. Fiz., 56:5 (2015),  30–49
13. Modeling of a supersonic flow around a cylinder with a gas-permeable porous insert
    
    Prikl. Mekh. Tekh. Fiz., 56:4 (2015),  12–22
14. ANSYS Fluent application for studying the influence of acoustic waves on a hypersonic shock layer over a flat plate
    
    Matem. Mod., 25:9 (2013),  32–42
15. Control of disturbances of a hypersonic viscous shock layer on a flat plate
    
    Prikl. Mekh. Tekh. Fiz., 53:3 (2012),  38–47
16. 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
17. Bispectral analysis of numerical simulations of wave processes in hypersonic shock layers
    
    Prikl. Mekh. Tekh. Fiz., 53:1 (2012),  3–11
18. Wave processes in the shock layer on a flat plate at an angle of attack
    
    Prikl. Mekh. Tekh. Fiz., 51:4 (2010),  39–47
19. Application of high-order accuracy schemes to numerical simulation of unsteady supersonic flows
    
    Matem. Mod., 19:7 (2007),  39–55
20. Numerical simulation of receptivity of a hypersonic boundary layer to acoustic disturbances
    
    Prikl. Mekh. Tekh. Fiz., 48:3 (2007),  84–91
21. Experimental study and direct numerical simulation of the evolution of disturbances in a viscous shock layer on a flat plate
    
    Prikl. Mekh. Tekh. Fiz., 47:5 (2006),  3–15
22. Viscous Shock Layer on a Cone in Hypersonic Flow
    
    TVT, 40:2 (2002),  256–261
23. Numerical simulation of hypersonic flow around a sharp cone
    
    Prikl. Mekh. Tekh. Fiz., 42:3 (2001),  43–50
24. Investigation of aerodynamic heating of a plate in a viscous hypersonic flow
    
    TVT, 37:3 (1999),  415–419
25. The effect of the angle of attack on hypersonic flow on a plate
    
    TVT, 36:5 (1998),  754–760
26. A numerical study of a viscous shock layer on a plate
    
    Prikl. Mekh. Tekh. Fiz., 38:2 (1997),  91–100
27. Hypersonic flow on a flat plate. Experimental results and numerical modeling
    
    Prikl. Mekh. Tekh. Fiz., 36:6 (1995),  60–67
28. Computational analysis of a spatial compressed turbulent boundary layer on the upwind side of delta wings under supersonic flow
    
    Prikl. Mekh. Tekh. Fiz., 35:1 (1994),  68–74
29. Numerical calculation of a three-dimensional laminar compressible boundary layer on profiled triangular wings with supersonic front edges
    
    Prikl. Mekh. Tekh. Fiz., 34:5 (1993),  88–94
30. Calculation of a laminar boundary layer on the leeward side of a triangular plate with supersonic leading edges
    
    Prikl. Mekh. Tekh. Fiz., 30:1 (1989),  75–81
31. Compressible laminar boundary layer on a delta wing with attached shock wave
    
    Prikl. Mekh. Tekh. Fiz., 26:5 (1985),  23–29