The experimental study of the weak shock wave action on the boundary layer of the sweep flat plate

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The experimental study of the weak shock wave action on the boundary layer of the sweep flat plate. / Kocharin, V. L.; Kosinov, A. D.; Yatskikh, A. A. и др.

в: Journal of Physics: Conference Series, Том 1404, № 1, 012083, 06.12.2019.

Результаты исследований: Научные публикации в периодических изданиях › статья по материалам конференции › Рецензирование

BibTeX

@article{5688542ff853481489716c8a40cfe095,

title = "The experimental study of the weak shock wave action on the boundary layer of the sweep flat plate",

abstract = "The weak shock waves impact on the flow in the boundary layer of the sweep flat plate at Mach number 2 is studied experimentally. The model was installed at a zero angle of attack. Shock waves in the oncoming flow were generated by a two-dimensional roughness on the side wall of the wind tunnel test section. The data were obtained with a two-dimensional roughness on the wall of the wind tunnel and with a smooth wall at sweep angles (35 and 40 degrees) of the leading edge of the flat blunt plate. The measurements were carried out with a constant temperature anemometer.",

author = "Kocharin, {V. L.} and Kosinov, {A. D.} and Yatskikh, {A. A.} and Afanasev, {L. V.} and Ermolaev, {Yu G.} and Semionov, {N. V.}",

year = "2019",

month = dec,

day = "6",

doi = "10.1088/1742-6596/1404/1/012083",

language = "English",

volume = "1404",

journal = "Journal of Physics: Conference Series",

issn = "1742-6588",

publisher = "IOP Publishing Ltd.",

number = "1",

note = "16th All-Russian Seminar with International Participation on Dynamics of Multiphase Media, DMM 2019 ; Conference date: 30-09-2019 Through 05-10-2019",

}

RIS

TY - JOUR

T1 - The experimental study of the weak shock wave action on the boundary layer of the sweep flat plate

AU - Kocharin, V. L.

AU - Kosinov, A. D.

AU - Yatskikh, A. A.

AU - Afanasev, L. V.

AU - Ermolaev, Yu G.

AU - Semionov, N. V.

PY - 2019/12/6

Y1 - 2019/12/6

N2 - The weak shock waves impact on the flow in the boundary layer of the sweep flat plate at Mach number 2 is studied experimentally. The model was installed at a zero angle of attack. Shock waves in the oncoming flow were generated by a two-dimensional roughness on the side wall of the wind tunnel test section. The data were obtained with a two-dimensional roughness on the wall of the wind tunnel and with a smooth wall at sweep angles (35 and 40 degrees) of the leading edge of the flat blunt plate. The measurements were carried out with a constant temperature anemometer.

AB - The weak shock waves impact on the flow in the boundary layer of the sweep flat plate at Mach number 2 is studied experimentally. The model was installed at a zero angle of attack. Shock waves in the oncoming flow were generated by a two-dimensional roughness on the side wall of the wind tunnel test section. The data were obtained with a two-dimensional roughness on the wall of the wind tunnel and with a smooth wall at sweep angles (35 and 40 degrees) of the leading edge of the flat blunt plate. The measurements were carried out with a constant temperature anemometer.

UR - http://www.scopus.com/inward/record.url?scp=85077819817&partnerID=8YFLogxK

U2 - 10.1088/1742-6596/1404/1/012083

DO - 10.1088/1742-6596/1404/1/012083

M3 - Conference article

AN - SCOPUS:85077819817

VL - 1404

JO - Journal of Physics: Conference Series

JF - Journal of Physics: Conference Series

SN - 1742-6588

IS - 1

M1 - 012083

T2 - 16th All-Russian Seminar with International Participation on Dynamics of Multiphase Media, DMM 2019

Y2 - 30 September 2019 through 5 October 2019

ER -

ID: 23120287