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Publications in Math-Net.Ru |
Citations |
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2010 |
| 1. |
V. M. Fomin, V. N. Vetlutskii, V. L. Ganimedov, M. I. Muchnaya, V. N. Shepelenko, M. N. Mel'nikov, A. A. Savina, “Air flow in the human nasal cavity”, Prikl. Mekh. Tekh. Fiz., 51:2 (2010), 107–115   ; J. Appl. Mech. Tech. Phys., 51:2 (2010), 233–240 |
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2009 |
| 2. |
V. N. Vetlutskii, V. L. Ganimedov, M. I. Muchnaya, “Flow in a viscous jet escaping through a supersonic nozzle into a semi-infinite ambient space”, Prikl. Mekh. Tekh. Fiz., 50:6 (2009), 6–15 ; J. Appl. Mech. Tech. Phys., 50:6 (2009), 918–926 |
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2005 |
| 3. |
V. N. Vetlutskii, V. L. Ganimedov, M. I. Muchnaya, “Investigation of a gas flow with solid particles in a supersonic nozzle”, Prikl. Mekh. Tekh. Fiz., 46:6 (2005), 65–77 ; J. Appl. Mech. Tech. Phys., 46:6 (2005), 824–834 |
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2004 |
| 4. |
V. N. Vetlutskii, V. L. Ganimedov, E. Krauze, “Numerical investigation of three-dimensional super- and hypersonic boundary layers at large Reynolds numbers”, Sib. Zh. Ind. Mat., 7:1 (2004), 9–20  |
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1999 |
| 5. |
V. N. Vetlutskii, E. M. Houtman, “Investigation of a turbulent boundary layer on a hypersonic aircraft model”, Prikl. Mekh. Tekh. Fiz., 40:1 (1999), 115–125 ; J. Appl. Mech. Tech. Phys., 40:1 (1999), 99–107 |
| 6. |
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 |
| 7. |
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 |
| 8. |
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 |
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1995 |
| 9. |
V. N. Vetlutskii, V. L. Ganimedov, M. I. Muchnaya, A. N. Shvorak, “Calculation of flow in a chemical reactor for chloroorganic waste utilization”, Fizika Goreniya i Vzryva, 31:4 (1995), 44–53 ; Combustion, Explosion and Shock Waves, 31:4 (1995), 441–449 |
| 10. |
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 |
| 11. |
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 |
| 12. |
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 |
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1991 |
| 13. |
V. N. Vetlutskii, “Computing the compressible laminar boundary layer on a sharp body of bielliptic section”, Prikl. Mekh. Tekh. Fiz., 32:1 (1991), 55–61 ; J. Appl. Mech. Tech. Phys., 32:1 (1991), 51–57 |
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1989 |
| 14. |
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 |
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1985 |
| 15. |
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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1975 |
| 16. |
V. N. Vetlutskii, V. L. Ganimedov, “Investigation of the supersonic flow around a pointed elliptical cone at an angle of attack”, Prikl. Mekh. Tekh. Fiz., 16:1 (1975), 114–120 ; J. Appl. Mech. Tech. Phys., 16:1 (1975), 89–94 |
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