On secondary instability of a transitional separation bubble

被引:19
作者
Yang, Zhiyin [1 ]
Abdalla, Ibrahim E. [2 ]
机构
[1] Univ Derby, Coll Engn & Technol, Sch Mech Engn & Built Environm, Derby DE22 3AW, England
[2] Jubail Univ Coll, Dept Mech Engn, Al Jubail 35716, Saudi Arabia
关键词
Secondary instability; Transition; Separation bubble; large-eddy simulation; Elliptical Instability; LARGE-EDDY SIMULATION; PLANE MIXING LAYER; 3-DIMENSIONAL EVOLUTION; FLOW; DYNAMICS; AIRFOIL;
D O I
10.1016/j.compfluid.2018.11.028
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
It is well established in the natural transition of an attached boundary layer that the transition process starts with a two-dimensional primary instability (Tollmien-Schlichting wave, denoted as TS wave), followed by usually a three-dimensional secondary instability (fundamental mode or subharmonic mode) leading to the breakdown to turbulence. However, the transition process of a separation bubble (laminar flow or laminar boundary layer at separation and transition occurs downstream of the separation, leading to turbulence at reattachment) is less well understood, especially on the nature of secondary instability. The focus of this paper is on trying to advance our understanding of secondary instability of a transitional separation bubble on a flat plate with a blunt leading edge (separation is induced geometrically at the leading edge) under a very low free-stream turbulence level (<0.1%). Large-Eddy Simulation (LES) is employed in the current study with a dynamic sub-grid-scale model. The numerical flow visualisation together with the spectral analysis has indicated that a three dimensional secondary instability, the elliptical instability, which occurs for fundamental frequency is the main mechanism at work whereas the subharmonic mode in the form of vortex-pairing is hardly active. There is no evidence for the existence of hyperbolic instability in the braid region either. (C) 2018 Elsevier Ltd. All rights reserved.
引用
收藏
页码:595 / 603
页数:9
相关论文
共 47 条
[1]   Numerical study of a separated-reattached flow on a blunt plate [J].
Abdalla, IE ;
Yang, ZY .
AIAA JOURNAL, 2005, 43 (12) :2465-2474
[2]   Numerical study of the instability mechanism in transitional separating-reattaching flow [J].
Abdalla, IE ;
Yang, ZY .
INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 2004, 25 (04) :593-605
[3]   3-DIMENSIONAL SHEAR LAYERS VIA VORTEX DYNAMICS [J].
ASHURST, WT ;
MEIBURG, E .
JOURNAL OF FLUID MECHANICS, 1988, 189 :87-116
[4]   STREAMWISE VORTEX STRUCTURE IN PLANE MIXING LAYERS [J].
BERNAL, LP ;
ROSHKO, A .
JOURNAL OF FLUID MECHANICS, 1986, 170 :499-525
[5]   Time-resolved and volumetric PIV measurements of a transitional separation bubble on an SD7003 airfoil [J].
Burgmann, S. ;
Dannemann, J. ;
Schroeder, W. .
EXPERIMENTS IN FLUIDS, 2008, 44 (04) :609-622
[6]   Transition Mechanisms in Laminar Separated Flow Under Simulated Low Pressure Turbine Aerofoil Conditions [J].
Daehnert, Jerrit ;
Lyko, Christoph ;
Peitsch, Dieter .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2013, 135 (01)
[7]   A DYNAMIC SUBGRID-SCALE EDDY VISCOSITY MODEL [J].
GERMANO, M ;
PIOMELLI, U ;
MOIN, P ;
CABOT, WH .
PHYSICS OF FLUIDS A-FLUID DYNAMICS, 1991, 3 (07) :1760-1765
[8]   SECONDARY INSTABILITY OF BOUNDARY-LAYERS [J].
HERBERT, T .
ANNUAL REVIEW OF FLUID MECHANICS, 1988, 20 :487-526
[9]   PERTURBED FREE SHEAR LAYERS [J].
HO, CM ;
HUERRE, P .
ANNUAL REVIEW OF FLUID MECHANICS, 1984, 16 :365-424
[10]   SMALL-SCALE TRANSITION IN A PLANE MIXING LAYER [J].
HUANG, LS ;
HO, CM .
JOURNAL OF FLUID MECHANICS, 1990, 210 :475-500