Zobrazeno 1 - 10
of 155
pro vyhledávání: '"A. D. Kosinov"'
Publikováno v:
SIBERIAN JOURNAL OF PHYSICS. 17:58-71
The paper describes a digital signal processing technique for determining the relationship between disturbances in a supersonic flow and pulsations of the boundary layer of a flat plate model. Estimates of the error of the proposed data processing me
Autor:
M. V. Piterimova, А. D. Kosinov, N. V. Semionov, A. A. Yatskikh, V. L. Kocharin, Yu. G. Yermolaev
Publikováno v:
SIBERIAN JOURNAL OF PHYSICS. 17:30-40
An experimental study of the effect of longitudinal vortices generated by weak shock waves on the laminar-turbulent transition in the boundary layer of a flat plate at a Mach number 2 is conducted. To amplify the effect of the longitudinal vortices g
Publikováno v:
SIBERIAN JOURNAL OF PHYSICS. 17:41-47
A study of the effect of distributed gas with high specific heat capacity blowing into the supersonic boundary layer on its stability to artificial disturbances was conducted. It is shown that the injection of gas with high heat capacity Cp at certai
Autor:
L. V. Afanasev, A. D. Kosinov, A. A. Yatskikh, N. V. Semionov, Yu. G. Yermolaev, V. L. Kocharin
Publikováno v:
ACTUAL PROBLEMS OF CONTINUUM MECHANICS: EXPERIMENT, THEORY, AND APPLICATIONS.
Publikováno v:
ACTUAL PROBLEMS OF CONTINUUM MECHANICS: EXPERIMENT, THEORY, AND APPLICATIONS.
Autor:
Boris V. Smorodsky, Sergey A. Gaponov, Vladimir I. Lysenko, Alexander D. Kosinov, Michael I. Yaroslavtsev
Publikováno v:
ACTUAL PROBLEMS OF CONTINUUM MECHANICS: EXPERIMENT, THEORY, AND APPLICATIONS.
Autor:
A. A. Yatskikh, A. D. Kosinov, N. V. Semionov, Yu. G. Ermolaev, L. V. Afanasev, V. L. Kocharin, A. V. Shmakova
Publikováno v:
ACTUAL PROBLEMS OF CONTINUUM MECHANICS: EXPERIMENT, THEORY, AND APPLICATIONS.
Publikováno v:
ACTUAL PROBLEMS OF CONTINUUM MECHANICS: EXPERIMENT, THEORY, AND APPLICATIONS.
Autor:
Yu. G. Ermolaev, A. D. Kosinov, V. L. Kocharin, A. N. Semenov, N. V. Semionov, S. A. Shipul’, A. A. Yatskikh
Publikováno v:
Fluid Dynamics. 57:30-36
Autor:
Yu. G. Ermolaev, S. A. Shipul, Nikolay Semionov, A. D. Kosinov, Aleksey A. Yatskikh, Alexander N. Semenov, V. L. Kocharin
Publikováno v:
Thermophysics and Aeromechanics. 28:319-325
The influence of external vortex disturbances on the position of the laminar-turbulent transition in boundary layers on swept wings at the Mach number M = 2 is experimentally studied. The experiments are performed with two wing models; the sweep angl