Zobrazeno 1 - 10
of 63
pro vyhledávání: '"Nikolay Semionov"'
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
Publikováno v:
Siberian Journal of Physics. 14:46-55
Experimental study of the effect of a weak shock wave from the protuberance of two-dimensional roughness installed on the side wall of the test section of the wind tunnel on the supersonic boundary layer of the blunted flat plate at the Mach number 2
Autor:
O. P. Minin, L. V. Afanasev, A. A. Yatskih, S. G. Shevelkov, A. D. Kosinov, Yu. G. Yermolaev, Nikolay Semionov
Publikováno v:
Siberian Journal of Physics. 14:77-85
Experimental study of the influence of flow pulsation in settling chamber on the supersonic free stream disturbances was carried out. Data on the pulsations in the settling chamber and the efficiency of deturbulization system as well as the correlati
Publikováno v:
AIP Conference Proceedings.
Autor:
V. L. Kocharin, A. V. Panina, Yu. G. Ermolaev, Nikolay Semionov, Aleksey A. Yatskikh, A. D. Kosinov
Publikováno v:
AIP Conference Proceedings.
Autor:
V. L. Kocharin, L. V. Afanasev, Nikolay Semionov, Aleksey A. Yatskikh, Yu. G. Yermolaev, A. D. Kosinov
Publikováno v:
AIP Conference Proceedings.
Autor:
L. V. Afanasev, V. L. Kocharin, A. V. Panina, A. D. Kosinov, Aleksey A. Yatskikh, D. S. Prishchepova, Nikolay Semionov, Yu. G. Yermolaev
Publikováno v:
AIP Conference Proceedings.
Publikováno v:
AIP Conference Proceedings.
Autor:
Nikolay Semionov, Aleksey A. Yatskikh, S. N. Tagaev, Yu. G. Yermolaev, A. D. Kosinov, V. L. Kocharin
Publikováno v:
AIP Conference Proceedings.
This work is devoted to the results of an experimental study of the laminar-turbulent transition in the boundary layer of the wing with a sweep angle of the leading edge of 72 degrees. Experiments were performed in a supersonic low noise wind tunnel
Autor:
Aleksey A. Yatskikh, V. L. Kocharin, Nikolay Semionov, Yu. G. Yermolaev, M. V. Piterimova, Alexander D. Kosinov
Publikováno v:
HIGH-ENERGY PROCESSES IN CONDENSED MATTER (HEPCM 2020): Proceedings of the XXVII Conference on High-Energy Processes in Condensed Matter, dedicated to the 90th anniversary of the birth of RI Soloukhin.