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Investigation of the impulse action of a membrane on the straight wing boundary layer. / Katasonov, M. M.; Pavlenko, A. M.; Kozlov, V. V.

в: Thermophysics and Aeromechanics, Том 25, № 6, 01.11.2018, стр. 801-807.

Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование

Harvard

Katasonov, MM, Pavlenko, AM & Kozlov, VV 2018, 'Investigation of the impulse action of a membrane on the straight wing boundary layer', Thermophysics and Aeromechanics, Том. 25, № 6, стр. 801-807. https://doi.org/10.1134/S0869864318060021

APA

Katasonov, M. M., Pavlenko, A. M., & Kozlov, V. V. (2018). Investigation of the impulse action of a membrane on the straight wing boundary layer. Thermophysics and Aeromechanics, 25(6), 801-807. https://doi.org/10.1134/S0869864318060021

Vancouver

Katasonov MM, Pavlenko AM, Kozlov VV. Investigation of the impulse action of a membrane on the straight wing boundary layer. Thermophysics and Aeromechanics. 2018 нояб. 1;25(6):801-807. doi: 10.1134/S0869864318060021

Author

Katasonov, M. M. ; Pavlenko, A. M. ; Kozlov, V. V. / Investigation of the impulse action of a membrane on the straight wing boundary layer. в: Thermophysics and Aeromechanics. 2018 ; Том 25, № 6. стр. 801-807.

BibTeX

@article{6bf2ac6dbb8b489b91dcf2d5d6518396,
title = "Investigation of the impulse action of a membrane on the straight wing boundary layer",
abstract = "The hot-wire anemometry technique is used to study the development of controlled disturbances in a straight wing boundary layer. Three-dimensional surface oscillations with large amplitude generate two types of disturbances: the localized longitudinal structures and wave packets. In downstream direction, the intensity of localized longitudinal structures decreases. The wave packets manifest themselves near the fronts of longitudinal localized structure in the flow region with adverse pressure gradient. In the separation flow area, an intensive growth of the wave packets amplitude is observed. The spatial development of the wave packets coincides with the development of three-dimen-sional Tollmien-Schlichting wave under similar conditions.",
keywords = "boundary layer, separation, laminar-turbulent transition, longitudinal localized structure, wave packet, EVOLUTION, WAVE",
author = "Katasonov, {M. M.} and Pavlenko, {A. M.} and Kozlov, {V. V.}",
year = "2018",
month = nov,
day = "1",
doi = "10.1134/S0869864318060021",
language = "English",
volume = "25",
pages = "801--807",
journal = "Thermophysics and Aeromechanics",
issn = "0869-8643",
publisher = "PLEIADES PUBLISHING INC",
number = "6",

}

RIS

TY - JOUR

T1 - Investigation of the impulse action of a membrane on the straight wing boundary layer

AU - Katasonov, M. M.

AU - Pavlenko, A. M.

AU - Kozlov, V. V.

PY - 2018/11/1

Y1 - 2018/11/1

N2 - The hot-wire anemometry technique is used to study the development of controlled disturbances in a straight wing boundary layer. Three-dimensional surface oscillations with large amplitude generate two types of disturbances: the localized longitudinal structures and wave packets. In downstream direction, the intensity of localized longitudinal structures decreases. The wave packets manifest themselves near the fronts of longitudinal localized structure in the flow region with adverse pressure gradient. In the separation flow area, an intensive growth of the wave packets amplitude is observed. The spatial development of the wave packets coincides with the development of three-dimen-sional Tollmien-Schlichting wave under similar conditions.

AB - The hot-wire anemometry technique is used to study the development of controlled disturbances in a straight wing boundary layer. Three-dimensional surface oscillations with large amplitude generate two types of disturbances: the localized longitudinal structures and wave packets. In downstream direction, the intensity of localized longitudinal structures decreases. The wave packets manifest themselves near the fronts of longitudinal localized structure in the flow region with adverse pressure gradient. In the separation flow area, an intensive growth of the wave packets amplitude is observed. The spatial development of the wave packets coincides with the development of three-dimen-sional Tollmien-Schlichting wave under similar conditions.

KW - boundary layer

KW - separation

KW - laminar-turbulent transition

KW - longitudinal localized structure

KW - wave packet

KW - EVOLUTION

KW - WAVE

UR - http://www.scopus.com/inward/record.url?scp=85062427926&partnerID=8YFLogxK

U2 - 10.1134/S0869864318060021

DO - 10.1134/S0869864318060021

M3 - Article

VL - 25

SP - 801

EP - 807

JO - Thermophysics and Aeromechanics

JF - Thermophysics and Aeromechanics

SN - 0869-8643

IS - 6

ER -

ID: 18646505