Zobrazeno 1 - 7
of 7
pro vyhledávání: '"S. A. Shipul"'
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:
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
Publikováno v:
ACTUAL PROBLEMS OF CONTINUUM MECHANICS: EXPERIMENT, THEORY, AND APPLICATIONS.
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:
AIP Conference Proceedings.
Influence of small attack angles on the transition on the wing with the subsonic leading edge at M=2
Autor:
S. A. Shipul, Nikolay Semionov, Yu. G. Yermolaev, Aleksey A. Yatskikh, Alexander D. Kosinov, V. L. Kocharin
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.
The paper is devoted to an experimental study of laminar-turbulent transition in supersonic boundary layers on swept wings. The experiments were fulfilled in the low nose supersonic wind tunnel T-325 of Khristianovich Institute of Theoretical and App
Autor:
S. A. Shipul, Aleksey A. Yatskikh, Nikolay Semionov, Alexander N. Semenov, V. L. Kocharin, Yu. G. Yermolaev, Alexander D. Kosinov, A. V. Panina
Publikováno v:
Journal of Physics: Conference Series. 1404:012097
The paper is devoted to an experimental study of laminar-turbulent transition in supersonic boundary layers on swept wings at Mach 2. The experiments were fulfilled in the low nose supersonic wind tunnel T-325 of Khristianovich Institute of Theoretic