Zobrazeno 1 - 10
of 41
pro vyhledávání: '"N. V. Semionov"'
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
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:
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:
A. V. Panina, Yury G. Yermolaev, Vasilii L. Kocharin, Alexander D. Kosinov, Aleksey A. Yatskikh, N. V. Semionov
Publikováno v:
Siberian Journal of Physics. 16:81-90
The results of experimental studies on the impact of periodic flow modulation on the development of natural disturbances and artificial localized wave packets in the boundary layer of a swept wing with a leading edge swept angle of 40 degrees at a Ma
Autor:
S. G. Shevel'kov, N. V. Semionov, Yu. G. Ermolaev, V. L. Kocharin, Alexander D. Kosinov, O. P. Minin, Aleksey A. Yatskikh, M. V. Piterimova
Publikováno v:
Thermophysics and Aeromechanics. 26:803-809
The impact of weak shock waves on the boundary-layer flow of a flat blunt plate installed along the stream was experimentally studied for different sweep angles of the leading edge of the plate at Mach number 2. The shock waves in the incoming flow i
Autor:
Aleksey A. Yatskikh, Alexander D. Kosinov, N. V. Semionov, G. L. Kolosov, Yury G. Yermolaev, B. V. Smorodsky, Alexander N. Semenov
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 234:96-101
The paper is devoted to an experimental and theoretical study of effect of moderate angle-of-attack variation on disturbances evolution and laminar-turbulent transition in a supersonic boundary layer on swept wing at Mach 2. Monotonous growth of the
Publikováno v:
Technical Physics Letters. 45:242-245
The results of experimental studies of the effect of the duration and current of a pulsed glow discharge on the generation of localized disturbances in the supersonic boundary layer of a flat plate at Mach numbers of the oncoming flow M = 3 and 4 hav