Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › научная › Рецензирование
On the artificial wave packet development in a spanwise modulated boundary layer on the swept wing at Mach 2. / Panina, A.; Kosinov, A.; Semionov, N. и др.
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. ред. / Vasily M. Fomin. American Institute of Physics Inc., 2020. 030031 (AIP Conference Proceedings; Том 2288).Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › научная › Рецензирование
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TY - GEN
T1 - On the artificial wave packet development in a spanwise modulated boundary layer on the swept wing at Mach 2
AU - Panina, A.
AU - Kosinov, A.
AU - Semionov, N.
AU - Yermolaev, Yu
AU - Yatskikh, A.
N1 - Publisher Copyright: © 2020 Author(s). Copyright: Copyright 2020 Elsevier B.V., All rights reserved.
PY - 2020/10/26
Y1 - 2020/10/26
N2 - The results of an experimental study of the perturbation development created by pulsed glow discharge on the swept wing surface with periodic distributed roughness along the leading edge at Mach 2 are presented. The influence of periodic roughness on the model surface on the excitation and development of wide-spectrum disturbances in the process of laminar-turbulent transition is determined. It was found that the mean flow modulation in the boundary layer of a swept wing with a sweep angle of 40 degrees leads to a strengthening of the oblique breakdown mechanism.
AB - The results of an experimental study of the perturbation development created by pulsed glow discharge on the swept wing surface with periodic distributed roughness along the leading edge at Mach 2 are presented. The influence of periodic roughness on the model surface on the excitation and development of wide-spectrum disturbances in the process of laminar-turbulent transition is determined. It was found that the mean flow modulation in the boundary layer of a swept wing with a sweep angle of 40 degrees leads to a strengthening of the oblique breakdown mechanism.
KW - TRANSITION
KW - ROUGHNESS
KW - STABILITY
UR - http://www.scopus.com/inward/record.url?scp=85096636701&partnerID=8YFLogxK
U2 - 10.1063/5.0028368
DO - 10.1063/5.0028368
M3 - Conference contribution
AN - SCOPUS:85096636701
T3 - AIP Conference Proceedings
BT - High-Energy Processes in Condensed Matter, HEPCM 2020
A2 - Fomin, Vasily M.
PB - American Institute of Physics Inc.
T2 - 27th Conference on High-Energy Processes in Condensed Matter, HEPCM 2020
Y2 - 29 June 2020 through 3 July 2020
ER -
ID: 26097965