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Experimental investigation of the natural and controlled disturbance development in a supersonic boundary layer on the swept wing. / Panina, A. V.; Kosonov, A. D.; Semenov, N. V. et al.

In: Journal of Physics: Conference Series, Vol. 1382, No. 1, 012029, 28.11.2019.

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

Harvard

Panina, AV, Kosonov, AD, Semenov, NV, Yermolaev, YG, Kolosov, GL & Yatskikh, AA 2019, 'Experimental investigation of the natural and controlled disturbance development in a supersonic boundary layer on the swept wing', Journal of Physics: Conference Series, vol. 1382, no. 1, 012029. https://doi.org/10.1088/1742-6596/1382/1/012029

APA

Panina, A. V., Kosonov, A. D., Semenov, N. V., Yermolaev, Y. G., Kolosov, G. L., & Yatskikh, A. A. (2019). Experimental investigation of the natural and controlled disturbance development in a supersonic boundary layer on the swept wing. Journal of Physics: Conference Series, 1382(1), [012029]. https://doi.org/10.1088/1742-6596/1382/1/012029

Vancouver

Panina AV, Kosonov AD, Semenov NV, Yermolaev YG, Kolosov GL, Yatskikh AA. Experimental investigation of the natural and controlled disturbance development in a supersonic boundary layer on the swept wing. Journal of Physics: Conference Series. 2019 Nov 28;1382(1):012029. doi: 10.1088/1742-6596/1382/1/012029

Author

Panina, A. V. ; Kosonov, A. D. ; Semenov, N. V. et al. / Experimental investigation of the natural and controlled disturbance development in a supersonic boundary layer on the swept wing. In: Journal of Physics: Conference Series. 2019 ; Vol. 1382, No. 1.

BibTeX

@article{09c6722f5ff7415ba0d2211e137a84ab,
title = "Experimental investigation of the natural and controlled disturbance development in a supersonic boundary layer on the swept wing",
abstract = "The results of investigation of the transverse flow inhomogeneity effect on the natural and controlled disturbance development in 3D supersonic boundary layer are considered. The transition curves were measured on a model of a smooth swept wing and on a swept wing with roughness elements of two configurations. The influence of periodic surface roughness on the growth of natural pulsations (without using a discharge) in the boundary layer is determined. In experiments with artificial disturbances it is found that the periodic modulation of mean flow can lead to stabilization of controlled disturbances in supersonic boundary layer on a swept wing. It was found out that the weak flow inhomogeneity can influence the effectiveness of the active/passive technology of supersonic boundary layer transition control, including the surface microroughness on a swept wing.",
keywords = "TRANSITION, ROUGHNESS, STABILITY",
author = "Panina, {A. V.} and Kosonov, {A. D.} and Semenov, {N. V.} and Yermolaev, {Yu G.} and Kolosov, {G. L.} and Yatskikh, {A. A.}",
year = "2019",
month = nov,
day = "28",
doi = "10.1088/1742-6596/1382/1/012029",
language = "English",
volume = "1382",
journal = "Journal of Physics: Conference Series",
issn = "1742-6588",
publisher = "IOP Publishing Ltd.",
number = "1",
note = "3th Siberian Thermophysical Seminar, STS 2019 ; Conference date: 27-08-2019 Through 29-08-2019",

}

RIS

TY - JOUR

T1 - Experimental investigation of the natural and controlled disturbance development in a supersonic boundary layer on the swept wing

AU - Panina, A. V.

AU - Kosonov, A. D.

AU - Semenov, N. V.

AU - Yermolaev, Yu G.

AU - Kolosov, G. L.

AU - Yatskikh, A. A.

PY - 2019/11/28

Y1 - 2019/11/28

N2 - The results of investigation of the transverse flow inhomogeneity effect on the natural and controlled disturbance development in 3D supersonic boundary layer are considered. The transition curves were measured on a model of a smooth swept wing and on a swept wing with roughness elements of two configurations. The influence of periodic surface roughness on the growth of natural pulsations (without using a discharge) in the boundary layer is determined. In experiments with artificial disturbances it is found that the periodic modulation of mean flow can lead to stabilization of controlled disturbances in supersonic boundary layer on a swept wing. It was found out that the weak flow inhomogeneity can influence the effectiveness of the active/passive technology of supersonic boundary layer transition control, including the surface microroughness on a swept wing.

AB - The results of investigation of the transverse flow inhomogeneity effect on the natural and controlled disturbance development in 3D supersonic boundary layer are considered. The transition curves were measured on a model of a smooth swept wing and on a swept wing with roughness elements of two configurations. The influence of periodic surface roughness on the growth of natural pulsations (without using a discharge) in the boundary layer is determined. In experiments with artificial disturbances it is found that the periodic modulation of mean flow can lead to stabilization of controlled disturbances in supersonic boundary layer on a swept wing. It was found out that the weak flow inhomogeneity can influence the effectiveness of the active/passive technology of supersonic boundary layer transition control, including the surface microroughness on a swept wing.

KW - TRANSITION

KW - ROUGHNESS

KW - STABILITY

UR - http://www.scopus.com/inward/record.url?scp=85077245017&partnerID=8YFLogxK

U2 - 10.1088/1742-6596/1382/1/012029

DO - 10.1088/1742-6596/1382/1/012029

M3 - Conference article

AN - SCOPUS:85077245017

VL - 1382

JO - Journal of Physics: Conference Series

JF - Journal of Physics: Conference Series

SN - 1742-6588

IS - 1

M1 - 012029

T2 - 3th Siberian Thermophysical Seminar, STS 2019

Y2 - 27 August 2019 through 29 August 2019

ER -

ID: 22993348