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Investigation of laminar-turbulent transition of supersonic boundary layer by scanning constant temperature hot-wire anemometer. / Yatskikh, Aleksey A.; Kosinov, Alexander D.; Semionov, Nickolay V. и др.

19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. ред. / Fomin. Том 2027 American Institute of Physics Inc., 2018. 040041 (AIP Conference Proceedings; Том 2027).

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

Harvard

Yatskikh, AA, Kosinov, AD, Semionov, NV, Smorodsky, BV, Ermolaev, YG & Kolosov, GL 2018, Investigation of laminar-turbulent transition of supersonic boundary layer by scanning constant temperature hot-wire anemometer. в Fomin (ред.), 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. Том. 2027, 040041, 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/10.1063/1.5065315

APA

Yatskikh, A. A., Kosinov, A. D., Semionov, N. V., Smorodsky, B. V., Ermolaev, Y. G., & Kolosov, G. L. (2018). Investigation of laminar-turbulent transition of supersonic boundary layer by scanning constant temperature hot-wire anemometer. в Fomin (Ред.), 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018 (Том 2027). [040041] (AIP Conference Proceedings; Том 2027). American Institute of Physics Inc.. https://doi.org/10.1063/1.5065315

Vancouver

Yatskikh AA, Kosinov AD, Semionov NV, Smorodsky BV, Ermolaev YG, Kolosov GL. Investigation of laminar-turbulent transition of supersonic boundary layer by scanning constant temperature hot-wire anemometer. в Fomin, Редактор, 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. Том 2027. American Institute of Physics Inc. 2018. 040041. (AIP Conference Proceedings). doi: 10.1063/1.5065315

Author

Yatskikh, Aleksey A. ; Kosinov, Alexander D. ; Semionov, Nickolay V. и др. / Investigation of laminar-turbulent transition of supersonic boundary layer by scanning constant temperature hot-wire anemometer. 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{d9e7623e2803437d9f6881a2f8acead8,
title = "Investigation of laminar-turbulent transition of supersonic boundary layer by scanning constant temperature hot-wire anemometer",
abstract = "The work is devoted to the experimental study of the regularities of laminar-turbulent transition in supersonic boundary layers. The experiments were carried out in the low-noise supersonic wind tunnel T-325 of ITAM SB RAS. The measurements were made by a constant-temperature hot-wire anemometer in the scanning mode. The procedure of decomposition of the fluctuations of the boundary layer into temperature and mass flux disturbances was carried out. The level of pulsations in the free flow of the test section of the T-325 wind tunnel was determined. The laminar-turbulent transition of two-dimensional supersonic boundary layer was experimentally investigated at Mach number M = 2 and 2.5. The levels of total temperature and mass flow pulsations were measured. It was found that at the laminar-turbulent transition process the ratio of the mass flow and total temperature pulsations remains almost constant.",
author = "Yatskikh, {Aleksey A.} and Kosinov, {Alexander D.} and Semionov, {Nickolay V.} and Smorodsky, {Boris V.} and Ermolaev, {Yury G.} and Kolosov, {Gleb L.}",
note = "Publisher Copyright: {\textcopyright} 2018 Author(s).; 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018 ; Conference date: 13-08-2018 Through 19-08-2018",
year = "2018",
month = nov,
day = "2",
doi = "10.1063/1.5065315",
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",

}

RIS

TY - GEN

T1 - Investigation of laminar-turbulent transition of supersonic boundary layer by scanning constant temperature hot-wire anemometer

AU - Yatskikh, Aleksey A.

AU - Kosinov, Alexander D.

AU - Semionov, Nickolay V.

AU - Smorodsky, Boris V.

AU - Ermolaev, Yury G.

AU - Kolosov, Gleb L.

N1 - Publisher Copyright: © 2018 Author(s).

PY - 2018/11/2

Y1 - 2018/11/2

N2 - The work is devoted to the experimental study of the regularities of laminar-turbulent transition in supersonic boundary layers. The experiments were carried out in the low-noise supersonic wind tunnel T-325 of ITAM SB RAS. The measurements were made by a constant-temperature hot-wire anemometer in the scanning mode. The procedure of decomposition of the fluctuations of the boundary layer into temperature and mass flux disturbances was carried out. The level of pulsations in the free flow of the test section of the T-325 wind tunnel was determined. The laminar-turbulent transition of two-dimensional supersonic boundary layer was experimentally investigated at Mach number M = 2 and 2.5. The levels of total temperature and mass flow pulsations were measured. It was found that at the laminar-turbulent transition process the ratio of the mass flow and total temperature pulsations remains almost constant.

AB - The work is devoted to the experimental study of the regularities of laminar-turbulent transition in supersonic boundary layers. The experiments were carried out in the low-noise supersonic wind tunnel T-325 of ITAM SB RAS. The measurements were made by a constant-temperature hot-wire anemometer in the scanning mode. The procedure of decomposition of the fluctuations of the boundary layer into temperature and mass flux disturbances was carried out. The level of pulsations in the free flow of the test section of the T-325 wind tunnel was determined. The laminar-turbulent transition of two-dimensional supersonic boundary layer was experimentally investigated at Mach number M = 2 and 2.5. The levels of total temperature and mass flow pulsations were measured. It was found that at the laminar-turbulent transition process the ratio of the mass flow and total temperature pulsations remains almost constant.

UR - http://www.scopus.com/inward/record.url?scp=85056337541&partnerID=8YFLogxK

U2 - 10.1063/1.5065315

DO - 10.1063/1.5065315

M3 - Conference contribution

AN - SCOPUS:85056337541

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: 17411560