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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. et al.

In: Journal of Physics: Conference Series, Vol. 1404, No. 1, 012083, 06.12.2019.

Research output: Contribution to journal › Conference article › peer-review

Harvard

Kocharin, VL, Kosinov, AD, Yatskikh, AA, Afanasev, LV, Ermolaev, YG & Semionov, NV 2019, 'The experimental study of the weak shock wave action on the boundary layer of the sweep flat plate', Journal of Physics: Conference Series, vol. 1404, no. 1, 012083. https://doi.org/10.1088/1742-6596/1404/1/012083

APA

Kocharin, V. L., Kosinov, A. D., Yatskikh, A. A., Afanasev, L. V., Ermolaev, Y. G., & Semionov, N. V. (2019). The experimental study of the weak shock wave action on the boundary layer of the sweep flat plate. Journal of Physics: Conference Series, 1404(1), [012083]. https://doi.org/10.1088/1742-6596/1404/1/012083

Vancouver

Kocharin VL, Kosinov AD, Yatskikh AA, Afanasev LV, Ermolaev YG, Semionov NV. The experimental study of the weak shock wave action on the boundary layer of the sweep flat plate. Journal of Physics: Conference Series. 2019 Dec 6;1404(1):012083. doi: 10.1088/1742-6596/1404/1/012083

Author

Kocharin, V. L. ; Kosinov, A. D. ; Yatskikh, A. A. et al. / The experimental study of the weak shock wave action on the boundary layer of the sweep flat plate. In: Journal of Physics: Conference Series. 2019 ; Vol. 1404, No. 1.

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