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Publications in Math-Net.Ru |
Citations |
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2024 |
1. |
I. S. Tsyryulnikov, N. A. Maslov, S. G. Mironov, T. V. Poplavskaya, “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 ; J. Appl. Mech. Tech. Phys., 65:1 (2024), 40–49 |
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2022 |
2. |
A. V. Boiko, S. V. Kirilovskiy, T. V. Poplavskaya, “Computational grids for engineering modeling of the laminar–turbulent flow”, Prikl. Mekh. Tekh. Fiz., 63:6 (2022), 91–95 ; J. Appl. Mech. Tech. Phys., 63:6 (2022), 984–987 |
2
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3. |
S. G. Mironov, T. V. Poplavskaya, S. V. Kirilovskiy, I. R. Valiullin, T. S. Militsyna, A. A. Maslov, “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 |
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2021 |
4. |
S. G. Mironov, I. R. Valiullin, T. V. Poplavskaya, “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 ; Tech. Phys. Lett., 47:5 (2021), 396–398 |
5. |
A. V. Boiko, K. V. Demyanko, S. V. Kirilovskiy, Yu. M. Nechepurenko, T. V. Poplavskaya, “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 ; J. Appl. Mech. Tech. Phys., 62:6 (2021), 891–894 |
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6. |
S. G. Mironov, S. V. Kirilovskiy, T. V. Poplavskaya, I. S. Tsyryulnikov, “Thermal methods of drag control for cylindrical bodies with porous inserts in a supersonic flow”, Prikl. Mekh. Tekh. Fiz., 62:2 (2021), 5–16 ; J. Appl. Mech. Tech. Phys., 62:2 (2021), 183–192 |
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2020 |
7. |
S. G. Mironov, S. V. Kirilovskiy, T. V. Poplavskaya, I. S. Tsyryulnikov, A. A. Maslov, “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 ; J. Appl. Mech. Tech. Phys., 61:5 (2020), 693–699 |
6
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2019 |
8. |
D. V. Khotyanovsky, S. V. Kirilovskiy, T. V. Poplavskaya, A. N. Kudryavtsev, “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 ; J. Appl. Mech. Tech. Phys., 60:3 (2019), 438–450 |
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2018 |
9. |
S. G. Mironov, T. V. Poplavskaya, S. V. Kirilovskiy, A. A. Maslov, “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 ; Tech. Phys. Lett., 44:3 (2018), 225–228 |
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2016 |
10. |
I. S. Tsyryulnikov, S. V. Kirilovskiy, T. V. Poplavskaya, “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 ; Tech. Phys. Lett., 42:11 (2016), 1094–1098 |
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11. |
N. V. Petrov, S. V. Kirilovskiy, T. V. Poplavskaya, G. V. Shoev, “A numerical study of non-equilibrium flows with different vibrational relaxation models”, Pisma v Zhurnal Tekhnicheskoi Fiziki, 42:13 (2016), 72–79 ; Tech. Phys. Lett., 42:7 (2016), 697–700 |
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2015 |
12. |
A. V. Boiko, S. V. Kirilovskiy, A. A. Maslov, T. V. Poplavskaya, “Engineering modeling of the laminar–turbulent transition: Achievements and problems (Review)”, Prikl. Mekh. Tekh. Fiz., 56:5 (2015), 30–49 ; J. Appl. Mech. Tech. Phys., 56:5 (2015), 761–776 |
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13. |
S. G. Mironov, A. A. Maslov, T. V. Poplavskaya, S. V. Kirilovskiy, “Modeling of a supersonic flow around a cylinder with a gas-permeable porous insert”, Prikl. Mekh. Tekh. Fiz., 56:4 (2015), 12–22 ; J. Appl. Mech. Tech. Phys., 56:4 (2015), 549–557 |
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2013 |
14. |
S. V. Kirilovskiy, T. V. Poplavskaya, I. S. Tsyryulnikov, “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 |
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2012 |
15. |
S. V. Kirilovskiy, T. V. Poplavskaya, I. S. Tsyryulnikov, “Control of disturbances of a hypersonic viscous shock layer on a flat plate”, Prikl. Mekh. Tekh. Fiz., 53:3 (2012), 38–47 ; J. Appl. Mech. Tech. Phys., 53:3 (2012), 340–348 |
16. |
A. A. Maslov, S. G. Mironov, T. V. Poplavskaya, I. S. Tsyryulnikov, S. V. Kirilovskiy, “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 ; J. Appl. Mech. Tech. Phys., 53:2 (2012), 162–172 |
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17. |
D. A. Bountin, A. A. Maslov, S. G. Mironov, T. V. Poplavskaya, I. S. Tsyryulnikov, “Bispectral analysis of numerical simulations of wave processes in hypersonic shock layers”, Prikl. Mekh. Tekh. Fiz., 53:1 (2012), 3–11 ; J. Appl. Mech. Tech. Phys., 53:1 (2012), 1–8 |
1
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2010 |
18. |
A. A. Maslov, S. G. Mironov, T. V. Poplavskaya, I. S. Tsyryulnikov, “Wave processes in the shock layer on a flat plate at an angle of attack”, Prikl. Mekh. Tekh. Fiz., 51:4 (2010), 39–47 ; J. Appl. Mech. Tech. Phys., 51:4 (2010), 482–488 |
4
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2007 |
19. |
A. N. Kudryavtsev, T. V. Poplavskaya, D. V. Khotyanovsky, “Application of high-order accuracy schemes to numerical simulation of unsteady supersonic flows”, Matem. Mod., 19:7 (2007), 39–55 |
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20. |
A. A. Maslov, A. N. Kudryavtsev, S. G. Mironov, T. V. Poplavskaya, I. S. Tsyryulnikov, “Numerical simulation of receptivity of a hypersonic boundary layer to acoustic disturbances”, Prikl. Mekh. Tekh. Fiz., 48:3 (2007), 84–91 ; J. Appl. Mech. Tech. Phys., 48:3 (2007), 368–374 |
10
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2006 |
21. |
A. N. Kudryavtsev, S. G. Mironov, T. V. Poplavskaya, I. S. Tsyryulnikov, “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 ; J. Appl. Mech. Tech. Phys., 47:5 (2006), 617–627 |
12
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2002 |
22. |
T. V. Poplavskaya, “Viscous Shock Layer on a Cone in Hypersonic Flow”, TVT, 40:2 (2002), 256–261 ; High Temperature, 40:2 (2002), 228–233 |
1
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2001 |
23. |
T. V. Poplavskaya, S. G. Mironov, “Numerical simulation of hypersonic flow around a sharp cone”, Prikl. Mekh. Tekh. Fiz., 42:3 (2001), 43–50 ; J. Appl. Mech. Tech. Phys., 42:3 (2001), 420–426 |
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1999 |
24. |
A. A. Maslov, S. G. Mironov, T. V. Poplavskaya, A. N. Shiplyuk, V. N. Vetlutskii, “Investigation of aerodynamic heating of a plate in a viscous hypersonic flow”, TVT, 37:3 (1999), 415–419 ; High Temperature, 37:3 (1999), 388–392 |
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1998 |
25. |
A. A. Maslov, S. G. Mironov, T. V. Poplavskaya, V. N. Vetlutskii, “The effect of the angle of attack on hypersonic flow on a plate”, TVT, 36:5 (1998), 754–760 ; High Temperature, 36:5 (1998), 730–736 |
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1997 |
26. |
T. V. Poplavskaya, V. N. Vetlutskii, “A numerical study of a viscous shock layer on a plate”, Prikl. Mekh. Tekh. Fiz., 38:2 (1997), 91–100 ; J. Appl. Mech. Tech. Phys., 38:2 (1997), 250–258 |
1
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1995 |
27. |
V. N. Vetlutskii, A. A. Maslov, S. G. Mironov, T. V. Poplavskaya, A. N. Shiplyuk, “Hypersonic flow on a flat plate. Experimental results and numerical modeling”, Prikl. Mekh. Tekh. Fiz., 36:6 (1995), 60–67 ; J. Appl. Mech. Tech. Phys., 36:6 (1995), 848–854 |
3
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1994 |
28. |
V. N. Vetlutskii, T. V. Poplavskaya, “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 ; J. Appl. Mech. Tech. Phys., 35:1 (1994), 69–74 |
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1993 |
29. |
V. N. Vetlutskii, T. V. Poplavskaya, “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 ; J. Appl. Mech. Tech. Phys., 34:5 (1993), 677–682 |
1
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1989 |
30. |
V. N. Vetlutskii, T. V. Poplavskaya, “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 ; J. Appl. Mech. Tech. Phys., 30:1 (1989), 71–77 |
1
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1985 |
31. |
V. N. Vetlutskii, T. V. Poplavskaya, “Compressible laminar boundary layer on a delta wing with attached shock wave”, Prikl. Mekh. Tekh. Fiz., 26:5 (1985), 23–29 ; J. Appl. Mech. Tech. Phys., 26:5 (1985), 624–629 |
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