Zobrazeno 1 - 10
of 56
pro vyhledávání: '"M. A. Goldfeld"'
Publikováno v:
Combustion, Explosion, and Shock Waves. 58:536-545
Publikováno v:
Combustion, Explosion, and Shock Waves. 58:546-554
Publikováno v:
Физика горения и взрыва. 58:33-43
Publikováno v:
Физика горения и взрыва. 58:44-53
Publikováno v:
Физика горения и взрыва. 58:3-11
Autor:
M. A. Goldfeld, N. N. Fedorova
Publikováno v:
Technical Physics Letters. 47:50-55
A computational study of turbulent supersonic flows in a channel with a backward-facing step under the counter injection of argon and hydrogen jets is presented. The calculations are performed at the Mach number of 4 at the channel entrance for condi
Autor:
M. A. Goldfeld
Publikováno v:
Thermophysics and Aeromechanics. 27:573-584
The paper presents a study for conditions for hydrogen self-ignition and flame spreading in a supersonic combustion chamber at the Mach number for the inlet flow equal to 4. The experimental model is a rectangular channel with a flame stabilizer perf
Publikováno v:
Thermophysics and Aeromechanics. 26:639-650
In the present paper, we report on the results of a study that was performed as part of the program for developing a method for calculating the flow and the mass-flow-rate coefficient in narrow cylindrical bleed channels under conditions of impingeme
Autor:
A. V. Starov, M. A. Goldfeld
Publikováno v:
Combustion, Explosion, and Shock Waves. 55:274-281
Kerosene concentration distributions measured in the combustion chamber of a hotshot wind tunnel in the attached pipeline regime with the input Mach number of 2.89 are reported. Kerosene is injected through 12 jet injectors at an angle to the flow fr
Autor:
M. A. Goldfeld, A. V. Starov
Publikováno v:
Siberian Journal of Physics. 14:51-62
The results of a numerical and experimental study of a hypersonic air inlet with spatial compression and a compact cross section of the internal channel are presented. Reducing the surface area of the channel simplifies the heat protection of the air