An adverse-pressure-gradient turbulent boundary layer with nearly constant β ≃ 1.4 up to Reθ ≃ 8700

被引:36
作者
Pozuelo, Ramon [1 ]
Li, Qiang [1 ]
Schlatter, Philipp [1 ]
Vinuesa, Ricardo [1 ]
机构
[1] KTH Royal Inst Technol, Engn Mech, Flow, SE-10044 Stockholm, Sweden
关键词
turbulence simulation; turbulent boundary layers; DIRECT NUMERICAL-SIMULATION; EQUILIBRIUM; FLOWS;
D O I
10.1017/jfm.2022.221
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
In this study, a new well-resolved large-eddy simulation of an incompressible near-equilibrium adverse-pressure-gradient (APG) turbulent boundary layer (TBL) over a flat plate is presented. In this simulation, we have established a near-equilibrium APG over a wide Reynolds-number range. In this so-called region of interest, the Rotta-Clauser pressure-gradient parameter beta exhibits an approximately constant value of around 1.4, and the Reynolds number based on momentum thickness reaches Re-theta = 8700. To the best of the authors' knowledge, this is to date the highest Re-theta achieved for a near-equilibrium APG TBL under an approximately constant moderate APG. We evaluated the self-similarity of the outer region using two scalings, namely the Zagarola-Smits and an alternative scaling based on edge velocity and displacement thickness. Our results reveal that outer-layer similarity is achieved, and the viscous scaling collapses the near-wall region of the mean flow in agreement with classical theory. Spectral analysis reveals that the APG displaces some small-scale energy from the near-wall to the outer region, an effect observed for all the components of the Reynolds-stress tensor, which becomes more evident at higher Reynolds numbers. In general, the effects of the APG are more noticeable at lower Reynolds numbers. For instance, the outer peak of turbulent-kinetic-energy (TKE) production is less prominent at higher Re. Although the scale separation increases with Re in zero-pressure-gradient TBLs, this effect becomes accentuated by the APG. Despite the reduction of the outer TKE production at higher Reynolds numbers, the mechanisms of energisation of large scales are still present.
引用
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页数:36
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共 51 条
[41]   A TURBULENT EQUILIBRIUM BOUNDARY-LAYER NEAR SEPARATION [J].
SKARE, PE ;
KROGSTAD, PA .
JOURNAL OF FLUID MECHANICS, 1994, 272 :319-348
[42]   Effect of adverse pressure gradients on turbulent wing boundary layers [J].
Tanarro, A. ;
Vinuesa, R. ;
Schlatter, P. .
JOURNAL OF FLUID MECHANICS, 2020, 883
[43]  
Townsend A.A., 1976, The Structure of Turbulent Shear Flow / a.a.Townsend, Vsecond
[44]   EQUILIBRIUM LAYERS AND WALL TURBULENCE [J].
TOWNSEND, AA .
JOURNAL OF FLUID MECHANICS, 1961, 11 (01) :97-120
[45]   THE PROPERTIES OF EQUILIBRIUM BOUNDARY LAYERS [J].
TOWNSEND, AA .
JOURNAL OF FLUID MECHANICS, 1956, 1 (06) :561-573
[46]   Experimental realisation of near-equilibrium adverse-pressure-gradient turbulent boundary layers [J].
Vila, C. Sanmiguel ;
Vinuesa, R. ;
Discetti, S. ;
Ianiro, A. ;
Schlatter, P. ;
Orlu, R. .
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2020, 112
[47]   Turbulent boundary layers around wing sections up to Rec=1, 000, 000 [J].
Vinuesa, R. ;
Negi, P. S. ;
Atzori, M. ;
Hanifi, A. ;
Henningson, D. S. ;
Schlatter, P. .
INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 2018, 72 :86-99
[48]   On determining characteristic length scales in pressure-gradient turbulent boundary layers [J].
Vinuesa, R. ;
Bobke, A. ;
Orlu, R. ;
Schlatter, P. .
PHYSICS OF FLUIDS, 2016, 28 (05)
[49]   Revisiting History Effects in Adverse-Pressure-Gradient Turbulent Boundary Layers [J].
Vinuesa, Ricardo ;
Orlu, Ramis ;
Sanmiguel Vila, Carlos ;
Ianiro, Andrea ;
Discetti, Stefano ;
Schlatter, Philipp .
FLOW TURBULENCE AND COMBUSTION, 2017, 99 (3-4) :565-587
[50]   Convergence of numerical simulations of turbulent wall-bounded flows and mean cross-flow structure of rectangular ducts [J].
Vinuesa, Ricardo ;
Prus, Cezary ;
Schlatter, Philipp ;
Nagib, Hassan M. .
MECCANICA, 2016, 51 (12) :3025-3042