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Hot-wire measurements of the evolution of total temperature and mass flow pulsations in a modulated 3D supersonic boundary layer. / Kosinov, A. D.; Kolosov, G. L.; Yatskikh, A. A. et al.

19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. ed. / Fomin. Vol. 2027 American Institute of Physics Inc., 2018. 020016 (AIP Conference Proceedings; Vol. 2027).

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

Harvard

Kosinov, AD, Kolosov, GL, Yatskikh, AA, Semionov, NV, Yermolaev, YG & Panina, AV 2018, Hot-wire measurements of the evolution of total temperature and mass flow pulsations in a modulated 3D supersonic boundary layer. in Fomin (ed.), 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. vol. 2027, 020016, AIP Conference Proceedings, vol. 2027, American Institute of Physics Inc., 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018, Akademgorodok, Novosibirsk, Russian Federation, 13.08.2018. https://doi.org/10.1063/1.5065094

APA

Kosinov, A. D., Kolosov, G. L., Yatskikh, A. A., Semionov, N. V., Yermolaev, Y. G., & Panina, A. V. (2018). Hot-wire measurements of the evolution of total temperature and mass flow pulsations in a modulated 3D supersonic boundary layer. In Fomin (Ed.), 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018 (Vol. 2027). [020016] (AIP Conference Proceedings; Vol. 2027). American Institute of Physics Inc.. https://doi.org/10.1063/1.5065094

Vancouver

Kosinov AD, Kolosov GL, Yatskikh AA, Semionov NV, Yermolaev YG, Panina AV. Hot-wire measurements of the evolution of total temperature and mass flow pulsations in a modulated 3D supersonic boundary layer. In Fomin, editor, 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. Vol. 2027. American Institute of Physics Inc. 2018. 020016. (AIP Conference Proceedings). doi: 10.1063/1.5065094

Author

Kosinov, A. D. ; Kolosov, G. L. ; Yatskikh, A. A. et al. / Hot-wire measurements of the evolution of total temperature and mass flow pulsations in a modulated 3D supersonic boundary layer. 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. editor / Fomin. Vol. 2027 American Institute of Physics Inc., 2018. (AIP Conference Proceedings).

BibTeX

@inproceedings{f93875e16fa44d97ad7242a170167984,
title = "Hot-wire measurements of the evolution of total temperature and mass flow pulsations in a modulated 3D supersonic boundary layer",
abstract = "The paper is devoted to the experimental study of the growth of mass flux pulsations and disturbances of total temperature at the laminar-turbulent transition process in a modulated swept-wing boundary layer at Mach number of the oncoming flow M = 2 and 2.5. Total temperature and mass flow pulsations were measured by a constant-temperature anemometer (CTA), operating in the scanning regime. It was found that at laminar-turbulent transition process the ratio of the mass flow and total temperature pulsations remains almost constant.",
author = "Kosinov, {A. D.} and Kolosov, {G. L.} and Yatskikh, {A. A.} and Semionov, {N. V.} and Yermolaev, {Yu G.} and Panina, {A. V.}",
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 = "10.1063/1.5065094",
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 a modulated 3D supersonic boundary layer

AU - Kosinov, A. D.

AU - Kolosov, G. L.

AU - Yatskikh, A. A.

AU - Semionov, N. V.

AU - Yermolaev, Yu G.

AU - Panina, A. V.

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

PY - 2018/11/2

Y1 - 2018/11/2

N2 - The paper is devoted to the experimental study of the growth of mass flux pulsations and disturbances of total temperature at the laminar-turbulent transition process in a modulated swept-wing boundary layer at Mach number of the oncoming flow M = 2 and 2.5. Total temperature and mass flow pulsations were measured by a constant-temperature anemometer (CTA), operating in the scanning regime. It was found that at laminar-turbulent transition process the ratio of the mass flow and total temperature pulsations remains almost constant.

AB - The paper is devoted to the experimental study of the growth of mass flux pulsations and disturbances of total temperature at the laminar-turbulent transition process in a modulated swept-wing boundary layer at Mach number of the oncoming flow M = 2 and 2.5. Total temperature and mass flow pulsations were measured by a constant-temperature anemometer (CTA), operating in the scanning regime. It was found that at 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=85056350358&partnerID=8YFLogxK

U2 - 10.1063/1.5065094

DO - 10.1063/1.5065094

M3 - Conference contribution

AN - SCOPUS:85056350358

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: 17412963