Linear development of controlled disturbances in the supersonic boundary layer on a swept wing at Mach 2

被引：19

作者：

Kosinov, A. D. ^{[1
,2
]}

Kolosov, G. L. ^{[1
,2
]}

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

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

机构：

[1] Russian Acad Sci, Khristianovich Inst Theoret & Appl Mech, Siberian Branch, Inst Skaya Str 4-1, Novosibirsk 630090, Russia

[2] Novosibirsk State Univ, Novosibirsk 630090, Russia

来源：

PHYSICS OF FLUIDS | 2016年 / 28卷 / 06期

基金：

俄罗斯基础研究基金会;

关键词：

NONLINEAR-INTERACTION; TRANSITION; STABILITY;

D O I：

10.1063/1.4952999

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

Experimental results are presented on the linear development of a wave train in a three-dimensional supersonic boundary layer on a swept wing with 45 degrees-sweep angle at Mach number M = 2.0. Artificial disturbances in the boundary layer were excited by periodical glow discharge mainly at frequencies 10 and 20 kHz. The maximum of the controlled pulsation amplitude was localized in the boundary layer in normal to the swept-wing surface direction for spatial amplitude distributions as well as for the amplitude wave spectra. The asymmetry of the wave characteristics of the unstable disturbances in the boundary layer of a swept wing caused by the presence of crossflow is confirmed. The stability characteristics, including dispersion relations and amplification rates over a wide range of wave inclination angles, are obtained for disturbances with prescribed frequencies 10 and 20 kHz. Published by AIP Publishing.

引用

页数：16

共 50 条

[1] Linear and nonlinear development of controlled disturbances in the supersonic boundary layer on a swept wing at Mach 2.5
Kolosov, G. L.
Kosinov, A. D.
[J]. ALL RUSSIAN CONFERENCE WITH THE SCHOOL FOR YOUNG SCIENTISTS THERMOPHYSICS AND PHYSICAL HYDRODYNAMICS - 2016, 2016, 754 (1-10):
[2] Linear evolution of controlled disturbances in the supersonic boundary layer on a swept wing
Ermolaev, Yu. G.
Kolosov, G. L.
Kosinov, A. D.
Semenov, N. V.
[J]. FLUID DYNAMICS, 2014, 49 (02) : 188 - 197
[3] Linear evolution of controlled disturbances in the supersonic boundary layer on a swept wing
Yu. G. Ermolaev
G. L. Kolosov
A. D. Kosinov
N. V. Semenov
[J]. Fluid Dynamics, 2014, 49 : 188 - 197
[4] On the Nonlinear Development of Controlled Disturbances in the Supersonic Boundary Layer of a Swept Wing
Kolosov, G. L.
Kosinov, A. D.
Yermolaev, Yu. G.
Semionov, N. V.
[J]. PROCEEDINGS OF THE XXV CONFERENCE ON HIGH-ENERGY PROCESSES IN CONDENSED MATTER (HEPCM 2017), 2017, 1893
[5] On the Oblique Breakdown Mechanism in a Supersonic Boundary Layer on a Swept Wing at Mach 2
Panina, A. V.
Kosinov, A. D.
Semionov, N. V.
Yermolaev, Yu. G.
[J]. PROCEEDINGS OF THE XXV CONFERENCE ON HIGH-ENERGY PROCESSES IN CONDENSED MATTER (HEPCM 2017), 2017, 1893
[6] Evolution of disturbances in a laminarized supersonic boundary layer on a swept wing
Semionov, N. V.
Ermolaev, Yu. G.
Kosinov, A. D.
[J]. JOURNAL OF APPLIED MECHANICS AND TECHNICAL PHYSICS, 2008, 49 (02) : 188 - 193
[7] Evolution of disturbances in a laminarized supersonic boundary layer on a swept wing
N. V. Semionov
Yu. G. Ermolaev
A. D. Kosinov
[J]. Journal of Applied Mechanics and Technical Physics, 2008, 49 : 188 - 193
[8] 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
Yermolaev, Yu G.
Kolosov, G. L.
Yatskikh, A. A.
[J]. XXXV SIBERIAN THERMOPHYSICAL SEMINAR, 2019, 2019, 1382
[9] On artificial disturbances development in spanwise modulated supersonic boundary layer at Mach 2
Kosinov, A. D.
Panina, A. V.
Semionov, N. V.
Yermolaev, Yu. G.
[J]. FMA '09: PROCEEDINGS OF THE 7TH IASME / WSEAS INTERNATIONAL CONFERENCE ON FLUID MECHANICS AND AERODYNAMICS, 2009, : 94 - 100
[10] Experimental study of evolution of disturbances in a supersonic boundary layer on a swept-wing model under controlled conditions
A. D. Kosinov
N. V. Semionov
Yu. G. Ermolaev
V. Ya. Levchenko
[J]. Journal of Applied Mechanics and Technical Physics, 2000, 41 (1) : 44 - 49

← 1 2 3 4 5 →