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On the oblique breakdown mechanism in a supersonic boundary layer on a swept wing at Mach 2. / Panina, A. V.; Kosinov, A. D.; Semionov, N. V. et al.

Proceedings of the XXV Conference on High-Energy Processes in Condensed Matter, HEPCM 2017: Dedicated to the 60th Anniversary of the Khristianovich Institute of Theoretical and Applied Mechanics SB RAS. ed. / Fomin. Vol. 1893 American Institute of Physics Inc., 2017. 030079 (AIP Conference Proceedings; Vol. 1893).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Research › peer-review

Harvard

Panina, AV, Kosinov, AD, Semionov, NV & Yermolaev, YG 2017, On the oblique breakdown mechanism in a supersonic boundary layer on a swept wing at Mach 2. in Fomin (ed.), Proceedings of the XXV Conference on High-Energy Processes in Condensed Matter, HEPCM 2017: Dedicated to the 60th Anniversary of the Khristianovich Institute of Theoretical and Applied Mechanics SB RAS. vol. 1893, 030079, AIP Conference Proceedings, vol. 1893, American Institute of Physics Inc., 25th Conference on High-Energy Processes in Condensed Matter, HEPCM 2017, Novosibirsk, Russian Federation, 05.06.2017. https://doi.org/10.1063/1.5007538

APA

Panina, A. V., Kosinov, A. D., Semionov, N. V., & Yermolaev, Y. G. (2017). On the oblique breakdown mechanism in a supersonic boundary layer on a swept wing at Mach 2. In Fomin (Ed.), Proceedings of the XXV Conference on High-Energy Processes in Condensed Matter, HEPCM 2017: Dedicated to the 60th Anniversary of the Khristianovich Institute of Theoretical and Applied Mechanics SB RAS (Vol. 1893). [030079] (AIP Conference Proceedings; Vol. 1893). American Institute of Physics Inc.. https://doi.org/10.1063/1.5007538

Vancouver

Panina AV, Kosinov AD, Semionov NV, Yermolaev YG. On the oblique breakdown mechanism in a supersonic boundary layer on a swept wing at Mach 2. In Fomin, editor, Proceedings of the XXV Conference on High-Energy Processes in Condensed Matter, HEPCM 2017: Dedicated to the 60th Anniversary of the Khristianovich Institute of Theoretical and Applied Mechanics SB RAS. Vol. 1893. American Institute of Physics Inc. 2017. 030079. (AIP Conference Proceedings). doi: 10.1063/1.5007538

Author

Panina, A. V. ; Kosinov, A. D. ; Semionov, N. V. et al. / On the oblique breakdown mechanism in a supersonic boundary layer on a swept wing at Mach 2. Proceedings of the XXV Conference on High-Energy Processes in Condensed Matter, HEPCM 2017: Dedicated to the 60th Anniversary of the Khristianovich Institute of Theoretical and Applied Mechanics SB RAS. editor / Fomin. Vol. 1893 American Institute of Physics Inc., 2017. (AIP Conference Proceedings).

BibTeX

@inproceedings{b918386d9f3548fc92b44f49004ae29a,
title = "On the oblique breakdown mechanism in a supersonic boundary layer on a swept wing at Mach 2",
abstract = "The results of an experimental study of the controlled pulsations development in the spanwise modulated boundary layer of a swept wing are presented in the paper. The experiments were conducted at Mach 2 and unit Reynolds number Re1 = 6×106 m-1. The square stickers were applied to induce the spanwise modulation of mean flow in the boundary layer. It was obtained, that the presence of roughness leads to a decrease of the disturbance source efficiency at the subharmonic and fundamental frequency, and the oblique breakdown mechanism begins to appear at smaller values of the longitudinal coordinate × as compared with the case of a smooth wing.",
keywords = "STABILITY, TRANSITION, WAVE",
author = "Panina, {A. V.} and Kosinov, {A. D.} and Semionov, {N. V.} and Yermolaev, {Yu G.}",
year = "2017",
month = oct,
day = "26",
doi = "10.1063/1.5007538",
language = "English",
volume = "1893",
series = "AIP Conference Proceedings",
publisher = "American Institute of Physics Inc.",
editor = "Fomin",
booktitle = "Proceedings of the XXV Conference on High-Energy Processes in Condensed Matter, HEPCM 2017",
note = "25th Conference on High-Energy Processes in Condensed Matter, HEPCM 2017 ; Conference date: 05-06-2017 Through 09-06-2017",

}

RIS

TY - GEN

T1 - On the oblique breakdown mechanism in a supersonic boundary layer on a swept wing at Mach 2

AU - Panina, A. V.

AU - Kosinov, A. D.

AU - Semionov, N. V.

AU - Yermolaev, Yu G.

PY - 2017/10/26

Y1 - 2017/10/26

N2 - The results of an experimental study of the controlled pulsations development in the spanwise modulated boundary layer of a swept wing are presented in the paper. The experiments were conducted at Mach 2 and unit Reynolds number Re1 = 6×106 m-1. The square stickers were applied to induce the spanwise modulation of mean flow in the boundary layer. It was obtained, that the presence of roughness leads to a decrease of the disturbance source efficiency at the subharmonic and fundamental frequency, and the oblique breakdown mechanism begins to appear at smaller values of the longitudinal coordinate × as compared with the case of a smooth wing.

AB - The results of an experimental study of the controlled pulsations development in the spanwise modulated boundary layer of a swept wing are presented in the paper. The experiments were conducted at Mach 2 and unit Reynolds number Re1 = 6×106 m-1. The square stickers were applied to induce the spanwise modulation of mean flow in the boundary layer. It was obtained, that the presence of roughness leads to a decrease of the disturbance source efficiency at the subharmonic and fundamental frequency, and the oblique breakdown mechanism begins to appear at smaller values of the longitudinal coordinate × as compared with the case of a smooth wing.

KW - STABILITY

KW - TRANSITION

KW - WAVE

UR - http://www.scopus.com/inward/record.url?scp=85034211009&partnerID=8YFLogxK

U2 - 10.1063/1.5007538

DO - 10.1063/1.5007538

M3 - Conference contribution

AN - SCOPUS:85034211009

VL - 1893

T3 - AIP Conference Proceedings

BT - Proceedings of the XXV Conference on High-Energy Processes in Condensed Matter, HEPCM 2017

A2 - Fomin, null

PB - American Institute of Physics Inc.

T2 - 25th Conference on High-Energy Processes in Condensed Matter, HEPCM 2017

Y2 - 5 June 2017 through 9 June 2017

ER -

ID: 9674574