Gvozdeva Lyudmila Georgievna

Publications in Math-Net.Ru

1. 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. Differential characteristics of the overexpanded gas jet flow field in the vicinity of the nozzle edge
   
   Zhurnal Tekhnicheskoi Fiziki, 89:4 (2019),  483–490
3. 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
4. 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
5. 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
6. 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
7. Nonstationary processes during propagation of detonation waves in channels of variable cross section
   
   TVT, 33:6 (1995),  958–961
8. Shock-wave propagation in a gas and a porous medium
   
   Fizika Goreniya i Vzryva, 23:4 (1987),  125–129
9. Approximate calculation of steady-state shock wave parameters in porous compressible materials
   
   Prikl. Mekh. Tekh. Fiz., 27:1 (1986),  120–125
10. Investigation of the detonation of HN$_3$ near limits
    
    Fizika Goreniya i Vzryva, 21:1 (1985),  120–124
11. CALCULATION OF STATIONARY SHOCK-WAVE PARAMETERS IN THE POROUS COMPRESSIBLE MEDIUM
    
    Zhurnal Tekhnicheskoi Fiziki, 55:4 (1985),  773–775
12. Interaction of air shock waves with porous compressible materials
    
    Prikl. Mekh. Tekh. Fiz., 26:3 (1985),  111–115
13. Transition from Mach to regular reflection and domains of various Mach reflection configurations
    
    Fizika Goreniya i Vzryva, 13:1 (1977),  102–110
14. Experimental investigation of gasdynamic processes at sudden start-up of a supersonic nozzle
    
    Prikl. Mekh. Tekh. Fiz., 18:4 (1977),  66–74
15. Experimental study of irregular shock-wave reflection from the surface of a wedge
    
    Fizika Goreniya i Vzryva, 12:2 (1976),  260–269
16. Изменение интенсивности ударной волны при огибании выпуклого угла (№ 859-76 Деп. от 22 III 1976)
    
    TVT, 14:2 (1976),  436
17. Течение релаксирующего газа, возникающее при выходе ударной волны в расширяющийся канал
    
    TVT, 11:6 (1973),  1203–1212
18. 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