Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование
Impact of incident Mach wave on supersonic boundary layer. / Vaganov, A. V.; Ermolaev, Yu G.; Kolosov, G. L. и др.
в: Thermophysics and Aeromechanics, Том 23, № 1, 01.01.2016, стр. 43-48.Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование
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TY - JOUR
T1 - Impact of incident Mach wave on supersonic boundary layer
AU - Vaganov, A. V.
AU - Ermolaev, Yu G.
AU - Kolosov, G. L.
AU - Kosinov, A. D.
AU - Panina, A. V.
AU - Semionov, N. V.
AU - Yatskikh, A. A.
PY - 2016/1/1
Y1 - 2016/1/1
N2 - Results of an experimental study of the excitation of high-intensity disturbances by a weak external shock wave in laminar boundary layer on flat-plate models with sharp and blunted leading edges at М = 2.5 are reported. The field of disturbances produced by a 2D sticker in turbulent boundary layer on the wall of wind-tunnel test section in the free stream is shown to have the form of an N-wave. It is found that, on the blunted plate, the intensity of pulsations produced by weak external shock waves in boundary layer several times exceeds the intensity of pulsations produced in boundary layer on the model with a sharp leading edge.
AB - Results of an experimental study of the excitation of high-intensity disturbances by a weak external shock wave in laminar boundary layer on flat-plate models with sharp and blunted leading edges at М = 2.5 are reported. The field of disturbances produced by a 2D sticker in turbulent boundary layer on the wall of wind-tunnel test section in the free stream is shown to have the form of an N-wave. It is found that, on the blunted plate, the intensity of pulsations produced by weak external shock waves in boundary layer several times exceeds the intensity of pulsations produced in boundary layer on the model with a sharp leading edge.
KW - boundary layer
KW - experimental studies
KW - flat plate
KW - hot-wire anemometry
KW - sharp and blunt leading edges
KW - supersonic velocities
KW - wind tunnel
UR - http://www.scopus.com/inward/record.url?scp=84963760177&partnerID=8YFLogxK
U2 - 10.1134/S0869864316010054
DO - 10.1134/S0869864316010054
M3 - Article
AN - SCOPUS:84963760177
VL - 23
SP - 43
EP - 48
JO - Thermophysics and Aeromechanics
JF - Thermophysics and Aeromechanics
SN - 0869-8643
IS - 1
ER -
ID: 25840502