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Hot-wire measurements of the evolution of total temperature and mass flow pulsations in supersonic boundary layer on flat plate with coating permeability. / Kosinov, A. D.; Semionov, N. V.; Yermolaev, Yu G. и др.

19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. ред. / Fomin. Том 2027 American Institute of Physics Inc., 2018. 040087 (AIP Conference Proceedings; Том 2027).

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

Harvard

Kosinov, AD, Semionov, NV, Yermolaev, YG, Kolosov, GL, Yatskikh, AA & Kocharin, VL 2018, Hot-wire measurements of the evolution of total temperature and mass flow pulsations in supersonic boundary layer on flat plate with coating permeability. в Fomin (ред.), 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. Том. 2027, 040087, 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/10.1063/1.5065361

APA

Kosinov, A. D., Semionov, N. V., Yermolaev, Y. G., Kolosov, G. L., Yatskikh, A. A., & Kocharin, V. L. (2018). Hot-wire measurements of the evolution of total temperature and mass flow pulsations in supersonic boundary layer on flat plate with coating permeability. в Fomin (Ред.), 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018 (Том 2027). [040087] (AIP Conference Proceedings; Том 2027). American Institute of Physics Inc.. https://doi.org/10.1063/1.5065361

Vancouver

Kosinov AD, Semionov NV, Yermolaev YG, Kolosov GL, Yatskikh AA, Kocharin VL. Hot-wire measurements of the evolution of total temperature and mass flow pulsations in supersonic boundary layer on flat plate with coating permeability. в Fomin, Редактор, 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. Том 2027. American Institute of Physics Inc. 2018. 040087. (AIP Conference Proceedings). doi: 10.1063/1.5065361

Author

Kosinov, A. D. ; Semionov, N. V. ; Yermolaev, Yu G. и др. / Hot-wire measurements of the evolution of total temperature and mass flow pulsations in supersonic boundary layer on flat plate with coating permeability. 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{62cf6d84c1ae4aa7b631843616975360,
title = "Hot-wire measurements of the evolution of total temperature and mass flow pulsations in supersonic boundary layer on flat plate with coating permeability",
abstract = "An experimental study of supersonic boundary layer on a flat plate with coating permeability at two Mach numbers 2 and 2.5 was carried out. The flow disturbances were measured by a constant-temperature anemometer (CTA), operating in the scanning regime. The procedure for calibrating a constant-temperature anemometer has been performed. It was shown that the coefficients of sensitivity to pulsations of mass flow rate and stagnation temperature are practically independent of the Mach number of the oncoming flow. In experiments on a flat plate with porosity, the positions of the laminar-turbulent transition were determined. The obtained experimental data can be used in calculations and numerical prediction of a laminar-turbulent transition in a supersonic boundary layer.",
author = "Kosinov, {A. D.} and Semionov, {N. V.} and Yermolaev, {Yu G.} and Kolosov, {G. L.} and Yatskikh, {A. A.} and Kocharin, {V. 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 = "10.1063/1.5065361",
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 - Hot-wire measurements of the evolution of total temperature and mass flow pulsations in supersonic boundary layer on flat plate with coating permeability

AU - Kosinov, A. D.

AU - Semionov, N. V.

AU - Yermolaev, Yu G.

AU - Kolosov, G. L.

AU - Yatskikh, A. A.

AU - Kocharin, V. L.

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

PY - 2018/11/2

Y1 - 2018/11/2

N2 - An experimental study of supersonic boundary layer on a flat plate with coating permeability at two Mach numbers 2 and 2.5 was carried out. The flow disturbances were measured by a constant-temperature anemometer (CTA), operating in the scanning regime. The procedure for calibrating a constant-temperature anemometer has been performed. It was shown that the coefficients of sensitivity to pulsations of mass flow rate and stagnation temperature are practically independent of the Mach number of the oncoming flow. In experiments on a flat plate with porosity, the positions of the laminar-turbulent transition were determined. The obtained experimental data can be used in calculations and numerical prediction of a laminar-turbulent transition in a supersonic boundary layer.

AB - An experimental study of supersonic boundary layer on a flat plate with coating permeability at two Mach numbers 2 and 2.5 was carried out. The flow disturbances were measured by a constant-temperature anemometer (CTA), operating in the scanning regime. The procedure for calibrating a constant-temperature anemometer has been performed. It was shown that the coefficients of sensitivity to pulsations of mass flow rate and stagnation temperature are practically independent of the Mach number of the oncoming flow. In experiments on a flat plate with porosity, the positions of the laminar-turbulent transition were determined. The obtained experimental data can be used in calculations and numerical prediction of a laminar-turbulent transition in a supersonic boundary layer.

UR - http://www.scopus.com/inward/record.url?scp=85056308330&partnerID=8YFLogxK

U2 - 10.1063/1.5065361

DO - 10.1063/1.5065361

M3 - Conference contribution

AN - SCOPUS:85056308330

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: 17411705