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The wave packet development in the 3D supersonic boundary layers. / Yermolaev, Yury G.; Kosinov, Alexander D.; Semionov, Nickolay V.

19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. ред. / Fomin. Том 2027 American Institute of Physics Inc., 2018. 030102 (AIP Conference Proceedings; Том 2027).

Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › научная › Рецензирование

Harvard

Yermolaev, YG, Kosinov, AD & Semionov, NV 2018, The wave packet development in the 3D supersonic boundary layers. в Fomin (ред.), 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. Том. 2027, 030102, AIP Conference Proceedings, Том. 2027, American Institute of Physics Inc., 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018, Akademgorodok, Novosibirsk, Российская Федерация, 13.08.2018. https://doi.org/10.1063/1.5065196

APA

Yermolaev, Y. G., Kosinov, A. D., & Semionov, N. V. (2018). The wave packet development in the 3D supersonic boundary layers. в Fomin (Ред.), 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018 (Том 2027). [030102] (AIP Conference Proceedings; Том 2027). American Institute of Physics Inc.. https://doi.org/10.1063/1.5065196

Vancouver

Yermolaev YG, Kosinov AD, Semionov NV. The wave packet development in the 3D supersonic boundary layers. в Fomin, Редактор, 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. Том 2027. American Institute of Physics Inc. 2018. 030102. (AIP Conference Proceedings). doi: 10.1063/1.5065196

Author

Yermolaev, Yury G. ; Kosinov, Alexander D. ; Semionov, Nickolay V. / The wave packet development in the 3D supersonic boundary layers. 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. Редактор / Fomin. Том 2027 American Institute of Physics Inc., 2018. (AIP Conference Proceedings).

BibTeX

@inproceedings{0affc80112994d8aa40cf8aac4044175,
title = "The wave packet development in the 3D supersonic boundary layers",
abstract = "The evolution of the artificial wave packet in the supersonic boundary layer of swept wing was experimentally studied for the first time by hot-wire measurements. The localized disturbances were generated by pulse glow discharge. Analysis of the mean flow, integral dependences, the averaged waveforms of wave packet and spectral data analysis in supersonic boundary layer of swept wing has been executed. Estimates of the velocity of propagation of controlled disturbances downstream are made. A comparison of the wave packet development in the boundary layer of a swept wing at two Mach numbers is given.",
keywords = "EVOLUTION",
author = "Yermolaev, {Yury G.} and Kosinov, {Alexander D.} and Semionov, {Nickolay V.}",
year = "2018",
month = nov,
day = "2",
doi = "10.1063/1.5065196",
language = "English",
volume = "2027",
series = "AIP Conference Proceedings",
publisher = "American Institute of Physics Inc.",
editor = "Fomin",
booktitle = "19th International Conference on the Methods of Aerophysical Research, ICMAR 2018",
note = "19th International Conference on the Methods of Aerophysical Research, ICMAR 2018 ; Conference date: 13-08-2018 Through 19-08-2018",

}

RIS

TY - GEN

T1 - The wave packet development in the 3D supersonic boundary layers

AU - Yermolaev, Yury G.

AU - Kosinov, Alexander D.

AU - Semionov, Nickolay V.

PY - 2018/11/2

Y1 - 2018/11/2

N2 - The evolution of the artificial wave packet in the supersonic boundary layer of swept wing was experimentally studied for the first time by hot-wire measurements. The localized disturbances were generated by pulse glow discharge. Analysis of the mean flow, integral dependences, the averaged waveforms of wave packet and spectral data analysis in supersonic boundary layer of swept wing has been executed. Estimates of the velocity of propagation of controlled disturbances downstream are made. A comparison of the wave packet development in the boundary layer of a swept wing at two Mach numbers is given.

AB - The evolution of the artificial wave packet in the supersonic boundary layer of swept wing was experimentally studied for the first time by hot-wire measurements. The localized disturbances were generated by pulse glow discharge. Analysis of the mean flow, integral dependences, the averaged waveforms of wave packet and spectral data analysis in supersonic boundary layer of swept wing has been executed. Estimates of the velocity of propagation of controlled disturbances downstream are made. A comparison of the wave packet development in the boundary layer of a swept wing at two Mach numbers is given.

KW - EVOLUTION

UR - http://www.scopus.com/inward/record.url?scp=85056340497&partnerID=8YFLogxK

U2 - 10.1063/1.5065196

DO - 10.1063/1.5065196

M3 - Conference contribution

AN - SCOPUS:85056340497

VL - 2027

T3 - AIP Conference Proceedings

BT - 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018

A2 - Fomin, null

PB - American Institute of Physics Inc.

T2 - 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018

Y2 - 13 August 2018 through 19 August 2018

ER -

ID: 17413589