Výsledky vyhledávání - "V. L. Kocharin"

Experimental study of effect of a pair of weak shock waves on laminar-turbulent transition in the boundary layer of flat plate at Mach number 2

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

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::b35f7591b7df0bac1ce7b91c4de364bf
https://doi.org/10.25205/2541-9447-2022-17-2-30-40

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Experimental study of the influence of external disturbances on the position of the laminar-turbulent transition on swept wings at M = 2

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

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::32dfc9692286dbb6112518b5d27f43bb
https://doi.org/10.1134/s0869864321030021

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The impact of weak shock waves on the flow in the boundary layer of a flat plate with a variable sweep angle of the leading edge

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

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::4003559e47aaac977586bf53743d15b1
https://doi.org/10.1134/s0869864319060027

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Experimental Investigation of the Weak Shock Wave Influence on the Boundary Layer of a Flat Blunt Plate at the Mach Number 2.5

Autor: V. L. Kocharin, N. V. Semenov, Yu. G. Ermolaev, Alexander D. Kosinov, Aleksey A. Yatskikh

Publikováno v: Fluid Dynamics. 54:257-263

The generation of two weak shock waves by a two-dimensional roughness mounted on the side wall of the test section of a wind tunnel and their influence on the supersonic boundary layer of a flat blunt plate is experimentally investigated at the Mach

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::1cf1a2dd91d54e1388c3a0b33aba80b9
https://doi.org/10.1134/s0015462819020058

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Experimental Study of the Weak Shock Wave Action on the Boundary Layer of a Plate at the Mach Number 2.5

Autor: V. L. Kocharin, Nikolay Semionov, Yu. G. Yermolaev, Aleksey A. Yatskikh, A. D. Kosinov

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

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::41c75da12a6da1830c7f7431bbe9bf45
https://doi.org/10.25205/2541-9447-2019-14-2-46-55

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