RUS  ENG
Full version
PEOPLE

Shumsky Valentin Vital'evich

Publications in Math-Net.Ru

  1. Composition of the test gas in the test section of a high-enthalpy wind tunnel

    Fizika Goreniya i Vzryva, 48:1 (2012),  28–37
  2. Short-duration wind tunnel with combined heating and stabilization of parameters

    Prikl. Mekh. Tekh. Fiz., 53:6 (2012),  3–10
  3. Experimental verification of the method of calculating the flow parameters in the test section of the hotshot wind tunnel

    Prikl. Mekh. Tekh. Fiz., 53:5 (2012),  79–89
  4. Specific features of combustion of hydrocarbon gases in composite porous inserts

    Fizika Goreniya i Vzryva, 47:6 (2011),  50–55
  5. Analysis of efficiency of using hybrid propulsion for accelerating small-size rockets starting from the Earth surface

    Prikl. Mekh. Tekh. Fiz., 51:6 (2010),  21–30
  6. Chemical heating of the working gas in a short-duration high-enthalpy facility

    Fizika Goreniya i Vzryva, 43:5 (2007),  31–43
  7. Gas dynamics of a low-pressure chamber in a high-enthalpy short-duration wind tunnel

    Prikl. Mekh. Tekh. Fiz., 46:1 (2005),  29–43
  8. Gas-dynamic method of determining combustion efficiency in a model with combustion

    Fizika Goreniya i Vzryva, 40:4 (2004),  23–34
  9. Chemical reactions of fuel combustion and nitrous-oxide decomposition used to generate and heat the test gas in a high-enthalpy short-duration facility

    Fizika Goreniya i Vzryva, 39:3 (2003),  50–57
  10. Effect of the fuel type on the characteristics of air-breathing engines

    Fizika Goreniya i Vzryva, 37:4 (2001),  25–33
  11. Conditions of self-ignition upon pulsed high-pressure injection of combustible gases into a bounded space

    Fizika Goreniya i Vzryva, 36:3 (2000),  3–10
  12. Special features of the combustion process in a channel with a supersonic velocity at the entrance

    Fizika Goreniya i Vzryva, 35:4 (1999),  24–32
  13. Effect of model dimensions on the thrust characteristics of ramjet engines in tests in a short-duration facility

    Fizika Goreniya i Vzryva, 35:1 (1999),  3–10
  14. Effect of the gasdynamics of a two-regime combustor on the power characteristics of a model with combustion

    Fizika Goreniya i Vzryva, 31:6 (1995),  49–63
  15. Some methodological aspects of the study of gas-dynamic models with heat and mass inflow in a pulsed wind tunnel

    Fizika Goreniya i Vzryva, 23:5 (1987),  45–54
  16. Pressure distribution and heat exchange in a gasdynamic model with combustion over which a high-enthalpy air stream flows

    Prikl. Mekh. Tekh. Fiz., 26:5 (1985),  56–65
  17. Force characteristics and flow parameters in combustion models

    Prikl. Mekh. Tekh. Fiz., 25:1 (1984),  103–109
  18. Self-ignition of a fuel gas escaping into an oxidizing medium

    Fizika Goreniya i Vzryva, 19:5 (1983),  73–80
  19. Investigation of gasdynamics of a model with combustion in a shock tunnel

    Prikl. Mekh. Tekh. Fiz., 24:6 (1983),  58–66
  20. Self-ignition of liquid fuels in a supersonic air flow

    Fizika Goreniya i Vzryva, 18:4 (1982),  22–26
  21. Injection of liquid into a supersonic flow of a high-enthalpy gas

    Fizika Goreniya i Vzryva, 17:3 (1981),  72–76


© Steklov Math. Inst. of RAS, 2024