The features of nonlinear development disturbances in a supersonic boundary layer in conditions of controllable experiments.

被引：0

作者：

Yermolaev, Yu. G. ^{[1
]}

Kosinov, A. D. ^{[1
]}

Semionov, N. V. ^{[1
]}

机构：

[1] Inst Theoret & Appl Mech SB RAS, Novosibirsk 630090, Russia

来源：

FMA'08: PROCEEDINGS OF THE 6TH IASME/WSEAS INTERNATIONAL CONFERENCE ON FLUID MECHANICS AND AERODYNAMICS: NEW ASPECTS OF FLUID MECHANICS AND AERODYNAMICS | 2008年

关键词：

supersonic boundary layer; instability; wave train; nonlinear; laminar-turbulent transition;

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The results of an experimental research of nonlinear interaction of the artificial disturbances with a natural pulsations of a supersonic boundary layer on flat plate model at Mach number M=2 arc presented in paper. The spectra of pulsations were determined and the estimations of bicoherence coefficients were made. It was detected, that the interaction of artificial pulsations with natural disturbances in a supersonic boundary layer on the initial stage is observed in the band from 10 up to 20 kHz. The result of a most intensive interaction happens away from the wave train center of the artificial disturbances in spanwise direction. It was obtained, that in controlled experiments only the energy generated random disturbances gives the main contribution (up to 90 %) in increasing of level total pulsations and can play the important role in the earlier laminar-turbulent transition.

引用

页码：174 / 179

页数：6

共 47 条

[1] On artificial disturbances development in spanwise modulated supersonic boundary layer at Mach 2
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Panina, A. V.
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FMA '09: PROCEEDINGS OF THE 7TH IASME / WSEAS INTERNATIONAL CONFERENCE ON FLUID MECHANICS AND AERODYNAMICS, 2009, : 94 - 100
[2] SPECIFIC FEATURES OF WAVE TRAIN DEVELOPMENT IN A STREAMWISE DISTURBANCE OF A SUPERSONIC BOUNDARY LAYER
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Yatskikh, A. A.
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JOURNAL OF APPLIED MECHANICS AND TECHNICAL PHYSICS, 2024, 65 (04) : 647 - 664
[3] Experimental and numerical investigation of controlled disturbances development from two sources in supersonic boundary layer
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Advances in Aerodynamics, 1
[4] Experimental and numerical investigation of controlled disturbances development from two sources in supersonic boundary layer
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ADVANCES IN AERODYNAMICS, 2019, 1 (01)
[5] “Anomalous” nonlinear wave phenomena in a supersonic boundary layer
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Journal of Applied Mechanics and Technical Physics, 1999, 40 (5) : 858 - 864
[6] Linear evolution of controlled disturbances in the supersonic boundary layer on a swept wing
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Kolosov, G. L.
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FLUID DYNAMICS, 2014, 49 (02) : 188 - 197
[7] Three-Wave Interactions between Disturbances in a Supersonic Boundary Layer
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Terekhova, N. M.
FLUID DYNAMICS, 2020, 55 (05) : 583 - 591
[8] Linear evolution of controlled disturbances in the supersonic boundary layer on a swept wing
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G. L. Kolosov
A. D. Kosinov
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Fluid Dynamics, 2014, 49 : 188 - 197
[9] Numerical Study of the Evolution of Disturbances Generated by Roughness Elements in a Supersonic Boundary Layer on a Blunted Cone
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[10] Experiments on the Nonlinear Development of Controlled Disturbances in the Region of Artificial Flow Inhomogeneity in the Flat-Plate Boundary Layer at Mach Number 2.5
Kosinov, A. D.
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Smorodskii, B. V.
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FLUID DYNAMICS, 2025, 60 (01)

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