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Publications in Math-Net.Ru |
Citations |
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2019 |
| 1. |
L. G. Gvozdeva, A. Yu. Chulyunin, “Numerical study of super-sound jet structure in two-dimensional nozzle depending on adiabat indicator”, Meždunar. nauč.-issled. žurn., 2019, no. 1(79), 27–32  |
| 2. |
M. V. Chernyshov, L. G. Gvozdeva, “Differential characteristics of the overexpanded gas jet flow field in the vicinity of the nozzle edge”, Zhurnal Tekhnicheskoi Fiziki, 89:4 (2019), 483–490  ; Tech. Phys., 64:4 (2019), 441–448 |
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2017 |
| 3. |
L. G. Gvozdeva, A. Yu. Chulyunin, “Study of dependence of flow structure in advanced super-surface nozzles from adiabatic indicator”, Meždunar. nauč.-issled. žurn., 2017, no. 12-5(66), 13–17 |
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2016 |
| 4. |
M. V. Sil'nikov, M. V. Chernyshov, L. G. Gvozdeva, “Analytic description of the domain of existence of triple configurations with a negative slope of reflected shock”, Zhurnal Tekhnicheskoi Fiziki, 86:11 (2016), 30–34 ; Tech. Phys., 61:11 (2016), 1633–1637 |
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| 5. |
O. A. Azarova, L. G. Gvozdeva, “Unsteady triple-shock configurations and vortex contact structures initiated by the interaction of an energy source with a shock layer in gases”, Pisma v Zhurnal Tekhnicheskoi Fiziki, 42:15 (2016), 59–66 ; Tech. Phys. Lett., 42:8 (2016), 799–803 |
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1996 |
| 6. |
D. I. Baklanov, L. G. Gvozdeva, “The effect of additional ignition on the stability of emergence of the mode of double nonstationary discontinuity in combustors”, TVT, 34:2 (1996), 299–302 ; High Temperature, 34:2 (1996), 294–297  |
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1995 |
| 7. |
D. I. Baklanov, L. G. Gvozdeva, “Nonstationary processes during propagation of detonation waves in channels of variable cross section”, TVT, 33:6 (1995), 958–961 ; High Temperature, 33:6 (1995), 955–958 |
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1987 |
| 8. |
L. G. Gvozdeva, V. N. Lyakhov, D. K. Raevskii, Yu. M. Faresov, “Shock-wave propagation in a gas and a porous medium”, Fizika Goreniya i Vzryva, 23:4 (1987), 125–129 ; Combustion, Explosion and Shock Waves, 23:4 (1987), 491–495 |
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1986 |
| 9. |
L. G. Gvozdeva, Yu. M. Faresov, “Approximate calculation of steady-state shock wave parameters in porous compressible materials”, Prikl. Mekh. Tekh. Fiz., 27:1 (1986), 120–125 ; J. Appl. Mech. Tech. Phys., 27:1 (1986), 107–111 |
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1985 |
| 10. |
T. V. Bazhenova, L. G. Gvozdeva, V. P. Fokeev, C. Paillard, J. Combourieu, G. Dupre, R. Lisbet, “Investigation of the detonation of HN$_3$ near limits”, Fizika Goreniya i Vzryva, 21:1 (1985), 120–124 ; Combustion, Explosion and Shock Waves, 21:1 (1985), 114–118 |
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| 11. |
L. G. Gvozdeva, Yu. M. Faresov, “CALCULATION OF STATIONARY SHOCK-WAVE PARAMETERS IN THE POROUS
COMPRESSIBLE MEDIUM”, Zhurnal Tekhnicheskoi Fiziki, 55:4 (1985), 773–775 |
| 12. |
L. G. Gvozdeva, Yu. M. Faresov, V. P. Fokeev, “Interaction of air shock waves with porous compressible materials”, Prikl. Mekh. Tekh. Fiz., 26:3 (1985), 111–115 ; J. Appl. Mech. Tech. Phys., 26:3 (1985), 401–405 |
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1977 |
| 13. |
L. G. Gvozdeva, V. P. Fokeev, “Transition from Mach to regular reflection and domains of various Mach reflection configurations”, Fizika Goreniya i Vzryva, 13:1 (1977), 102–110 ; Combustion, Explosion and Shock Waves, 13:1 (1977), 86–93 |
| 14. |
L. G. Gvozdeva, Yu. V. Zhilin, “Experimental investigation of gasdynamic processes at sudden start-up of a supersonic nozzle”, Prikl. Mekh. Tekh. Fiz., 18:4 (1977), 66–74 ; J. Appl. Mech. Tech. Phys., 18:4 (1977), 484–491 |
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1976 |
| 15. |
L. G. Gvozdeva, V. P. Fokeev, “Experimental study of irregular shock-wave reflection from the surface of a wedge”, Fizika Goreniya i Vzryva, 12:2 (1976), 260–269 ; Combustion, Explosion and Shock Waves, 12:2 (1976), 230–238 |
| 16. |
T. V. Bazhenova, L. G. Gvozdeva, Yu. V. Zhilin, “Изменение интенсивности ударной волны при огибании выпуклого угла (№ 859-76 Деп. от 22 III 1976)”, TVT, 14:2 (1976), 436 |
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1973 |
| 17. |
T. V. Bazhenova, L. G. Gvozdeva, V. S. Komarov, B. G. Sukhov, “Течение релаксирующего газа, возникающее при выходе ударной волны в расширяющийся канал”, TVT, 11:6 (1973), 1203–1212 |
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1965 |
| 18. |
L. G. Gvozdeva, O. A. Predvoditeleva, “An experimental investigation into the Mach reflection of shock waves moving with a velocity of $1000$–$3000$ m/sec.
in carbon dioxide gas, nitrogen or air”, Dokl. Akad. Nauk SSSR, 163:5 (1965), 1088–1091 |
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