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On the development of controlled stationary and travelling disturbances in the supersonic boundary layer of a swept wing. / Kolosov, Gleb; Panina, Alexandra; Kosinov, Alexander.
In: EPJ Web of Conferences, Vol. 159, 0024, 25.10.2017.Research output: Contribution to journal › Article › peer-review
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TY - JOUR
T1 - On the development of controlled stationary and travelling disturbances in the supersonic boundary layer of a swept wing
AU - Kolosov, Gleb
AU - Panina, Alexandra
AU - Kosinov, Alexander
PY - 2017/10/25
Y1 - 2017/10/25
N2 - Experimental data on the evolution of controlled stationary and travelling disturbances in a 3D supersonic boundary layer, over a 45° swept-wing at Mach number 2.0, is presented. Travelling artificial disturbances were introduced in the boundary layer by periodical glow discharge, at a frequency of 20 kHz. Stationary disturbances were acquired by setting the roughness elements on the surface of the model. Spatial-temporal and spectral-wave characteristics of the wave train at the frequency 20 kHz, in the linear region of development, were obtained. It was found that the periodic modulation of mean flow can lead to the stabilization of unstable travelling disturbances in the supersonic boundary layer of a swept wing. These experiments have investigated the viability of using roughness elements to control laminar-turbulent transition.
AB - Experimental data on the evolution of controlled stationary and travelling disturbances in a 3D supersonic boundary layer, over a 45° swept-wing at Mach number 2.0, is presented. Travelling artificial disturbances were introduced in the boundary layer by periodical glow discharge, at a frequency of 20 kHz. Stationary disturbances were acquired by setting the roughness elements on the surface of the model. Spatial-temporal and spectral-wave characteristics of the wave train at the frequency 20 kHz, in the linear region of development, were obtained. It was found that the periodic modulation of mean flow can lead to the stabilization of unstable travelling disturbances in the supersonic boundary layer of a swept wing. These experiments have investigated the viability of using roughness elements to control laminar-turbulent transition.
UR - http://www.scopus.com/inward/record.url?scp=85033459484&partnerID=8YFLogxK
U2 - 10.1051/epjconf/201715900024
DO - 10.1051/epjconf/201715900024
M3 - Article
AN - SCOPUS:85033459484
VL - 159
JO - EPJ Web of Conferences
JF - EPJ Web of Conferences
SN - 2101-6275
M1 - 0024
ER -
ID: 9699116