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Experimental study of the effects of couple weak waves on laminar-turbulent transition on attachment-line of a swept cylinder. / Yermolaev, Yu G.; Yatskih, A. A.; Kosinov, A. D. и др.

International Conference on the Methods of Aerophysical Research, ICMAR 2016: Proceedings of the 18th International Conference on the Methods of Aerophysical Research. ред. / Vasily Fomin. American Institute of Physics Inc., 2016. 120012 (AIP Conference Proceedings; Том 1770).

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

Harvard

Yermolaev, YG, Yatskih, AA, Kosinov, AD, Semionov, NV, Kolosov, GL & Panina, AV 2016, Experimental study of the effects of couple weak waves on laminar-turbulent transition on attachment-line of a swept cylinder. в V Fomin (ред.), International Conference on the Methods of Aerophysical Research, ICMAR 2016: Proceedings of the 18th International Conference on the Methods of Aerophysical Research., 120012, AIP Conference Proceedings, Том. 1770, American Institute of Physics Inc., 18th International Conference on the Methods of Aerophysical Research, ICMAR 2016, Perm, Российская Федерация, 27.06.2016. https://doi.org/10.1063/1.4963935

APA

Yermolaev, Y. G., Yatskih, A. A., Kosinov, A. D., Semionov, N. V., Kolosov, G. L., & Panina, A. V. (2016). Experimental study of the effects of couple weak waves on laminar-turbulent transition on attachment-line of a swept cylinder. в V. Fomin (Ред.), International Conference on the Methods of Aerophysical Research, ICMAR 2016: Proceedings of the 18th International Conference on the Methods of Aerophysical Research [120012] (AIP Conference Proceedings; Том 1770). American Institute of Physics Inc.. https://doi.org/10.1063/1.4963935

Vancouver

Yermolaev YG, Yatskih AA, Kosinov AD, Semionov NV, Kolosov GL, Panina AV. Experimental study of the effects of couple weak waves on laminar-turbulent transition on attachment-line of a swept cylinder. в Fomin V, Редактор, International Conference on the Methods of Aerophysical Research, ICMAR 2016: Proceedings of the 18th International Conference on the Methods of Aerophysical Research. American Institute of Physics Inc. 2016. 120012. (AIP Conference Proceedings). doi: 10.1063/1.4963935

Author

Yermolaev, Yu G. ; Yatskih, A. A. ; Kosinov, A. D. и др. / Experimental study of the effects of couple weak waves on laminar-turbulent transition on attachment-line of a swept cylinder. International Conference on the Methods of Aerophysical Research, ICMAR 2016: Proceedings of the 18th International Conference on the Methods of Aerophysical Research. Редактор / Vasily Fomin. American Institute of Physics Inc., 2016. (AIP Conference Proceedings).

BibTeX

@inproceedings{ff6a4e9bae71426fb8ed2d675981a90d,
title = "Experimental study of the effects of couple weak waves on laminar-turbulent transition on attachment-line of a swept cylinder",
abstract = "An experiment on a swept cylinder with 68°-sweep angle at Mach number M = 2.5 is described. The flow attachment line was disturbed by two weak shock waves. Shock waves were generated by a two-dimensional surface inhomogeneity on the wall of the test section of wind tunnel. It was found that the laminar-turbulent transition on the attachment-line of the cylinder is accompanied by an uneven growth of pulsations. Influence of Mach waves on the transition when their fall on the cylinder far away from domain of measuring is not observed. The laminar-turbulent transition occurs at a much lower unit Reynolds numbers in the case when a pair of waves falling on the attachment-line near the measurement field.",
author = "Yermolaev, {Yu G.} and Yatskih, {A. A.} and Kosinov, {A. D.} and Semionov, {N. V.} and Kolosov, {G. L.} and Panina, {A. V.}",
year = "2016",
month = oct,
day = "13",
doi = "10.1063/1.4963935",
language = "English",
series = "AIP Conference Proceedings",
publisher = "American Institute of Physics Inc.",
editor = "Vasily Fomin",
booktitle = "International Conference on the Methods of Aerophysical Research, ICMAR 2016",
note = "18th International Conference on the Methods of Aerophysical Research, ICMAR 2016 ; Conference date: 27-06-2016 Through 03-07-2016",

}

RIS

TY - GEN

T1 - Experimental study of the effects of couple weak waves on laminar-turbulent transition on attachment-line of a swept cylinder

AU - Yermolaev, Yu G.

AU - Yatskih, A. A.

AU - Kosinov, A. D.

AU - Semionov, N. V.

AU - Kolosov, G. L.

AU - Panina, A. V.

PY - 2016/10/13

Y1 - 2016/10/13

N2 - An experiment on a swept cylinder with 68°-sweep angle at Mach number M = 2.5 is described. The flow attachment line was disturbed by two weak shock waves. Shock waves were generated by a two-dimensional surface inhomogeneity on the wall of the test section of wind tunnel. It was found that the laminar-turbulent transition on the attachment-line of the cylinder is accompanied by an uneven growth of pulsations. Influence of Mach waves on the transition when their fall on the cylinder far away from domain of measuring is not observed. The laminar-turbulent transition occurs at a much lower unit Reynolds numbers in the case when a pair of waves falling on the attachment-line near the measurement field.

AB - An experiment on a swept cylinder with 68°-sweep angle at Mach number M = 2.5 is described. The flow attachment line was disturbed by two weak shock waves. Shock waves were generated by a two-dimensional surface inhomogeneity on the wall of the test section of wind tunnel. It was found that the laminar-turbulent transition on the attachment-line of the cylinder is accompanied by an uneven growth of pulsations. Influence of Mach waves on the transition when their fall on the cylinder far away from domain of measuring is not observed. The laminar-turbulent transition occurs at a much lower unit Reynolds numbers in the case when a pair of waves falling on the attachment-line near the measurement field.

UR - http://www.scopus.com/inward/record.url?scp=84994067471&partnerID=8YFLogxK

U2 - 10.1063/1.4963935

DO - 10.1063/1.4963935

M3 - Conference contribution

AN - SCOPUS:84994067471

T3 - AIP Conference Proceedings

BT - International Conference on the Methods of Aerophysical Research, ICMAR 2016

A2 - Fomin, Vasily

PB - American Institute of Physics Inc.

T2 - 18th International Conference on the Methods of Aerophysical Research, ICMAR 2016

Y2 - 27 June 2016 through 3 July 2016

ER -

ID: 25838670