History effects and near equilibrium in adverse-pressure-gradient turbulent boundary layers

被引:147
作者
Bobke, A. [1 ,2 ]
Vinuesa, R. [1 ,2 ]
Orlu, R. [1 ]
Schlatter, P. [1 ,2 ]
机构
[1] KTH Mech, Linne FLOW Ctr, SE-10044 Stockholm, Sweden
[2] Swedish E Sci Res Ctr SeRC, Stockholm, Sweden
基金
瑞典研究理事会;
关键词
turbulent boundary layers; turbulent flows; DIRECT NUMERICAL-SIMULATION; REYNOLDS-NUMBER; WING SECTION; EVOLUTION;
D O I
10.1017/jfm.2017.236
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Turbulent boundary layers under adverse pressure gradients are studied using well-resolved large-eddy simulations (LES) with the goal of assessing the influence of the streamwise pressure-gradient development. Near-equilibrium boundary layers were characterized through the Clauser pressure-gradient parameter beta. In order to fulfil the near-equilibrium conditions, the free stream velocity was prescribed such that it followed a power-law distribution. The turbulence statistics pertaining to cases with a constant value of beta (extending up to approximately 40 boundary-layer thicknesses) were compared with cases with non-constant beta distributions at matched values of beta and friction Reynolds number Re-tau. An additional case at matched Reynolds number based on displacement thickness Re-delta* was also considered. It was noticed that non-constant beta cases appear to approach the conditions of equivalent constant beta cases after long streamwise distances (approximately 7 boundary-layer thicknesses). The relevance of the constant beta cases lies in the fact that they define a 'canonical' state of the boundary layer, uniquely characterized by beta and Re. The investigations on the flat plate were extended to the flow around a wing section overlapping in terms of beta and Re. Comparisons with the flat-plate cases at matched values of beta and Re revealed that the different development history of the turbulent boundary layer on the wing section leads to a less pronounced wake in the mean velocity as well as a weaker second peak in the Reynolds stresses. This is due to the weaker accumulated effect of the beta history. Furthermore, a scaling law suggested by Kitsios et al. (Intl J. Heat Fluid Flow, vol. 61, 2016, pp. 129-136), proposing the edge velocity and the displacement thickness as scaling parameters, was tested on two constant-pressure-gradient parameter cases. The mean velocity and Reynolds-stress profiles were found to be dependent on the downstream development. The present work is the first step towards assessing history effects in adverse-pressure-gradient turbulent boundary layers and highlights the fact that the values of the Clauser pressure-gradient parameter and the Reynolds number are not sufficient to characterize the state of the boundary layer.
引用
收藏
页码:667 / 692
页数:26
相关论文
共 37 条
[1]   A new formulation for the streamwise turbulence intensity distribution in wall-bounded turbulent flows [J].
Alfredsson, P. Henrik ;
Orlu, Ramis ;
Segalini, Antonio .
EUROPEAN JOURNAL OF MECHANICS B-FLUIDS, 2012, 36 :167-175
[2]   A new scaling for the streamwise turbulence intensity in wall-bounded turbulent flows and what it tells us about the "outer" peak [J].
Alfredsson, P. Henrik ;
Segalini, Antonio ;
Orlu, Ramis .
PHYSICS OF FLUIDS, 2011, 23 (04)
[3]  
ATKINSON C., 2016, P 18 INT S APPL LAS
[4]   Obtaining accurate mean velocity measurements in high Reynolds number turbulent boundary layers using Pitot tubes [J].
Bailey, S. C. C. ;
Hultmark, M. ;
Monty, J. P. ;
Alfredsson, P. H. ;
Chong, M. S. ;
Duncan, R. D. ;
Fransson, J. H. M. ;
Hutchins, N. ;
Marusic, I. ;
McKeon, B. J. ;
Nagib, H. M. ;
Orlu, R. ;
Segalini, A. ;
Smits, A. J. ;
Vinuesa, R. .
JOURNAL OF FLUID MECHANICS, 2013, 715 :642-670
[5]   Large-eddy simulations of adverse pressure gradient turbulent boundary layers [J].
Bobke, Alexandra ;
Vinuesa, Ricardo ;
Orlu, Ramis ;
Schlatter, Philipp .
2ND MULTIFLOW SUMMER SCHOOL ON TURBULENCE, 2016, 708
[6]   Simulations of turbulent asymptotic suction boundary layers [J].
Bobke, Alexandra ;
Orlu, Ramis ;
Schlatter, Philipp .
JOURNAL OF TURBULENCE, 2016, 17 (02) :157-180
[7]  
CHEVALIER M., 2007, 200707 TRITA MEK KTH
[8]   Simulation and validation of a spatially evolving turbulent boundary layer up to Reθ=8300 [J].
Eitel-Amor, Georg ;
Orlu, Ramis ;
Schlatter, Philipp .
INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 2014, 47 :57-69
[9]  
Fischer P., 2008, nek5000
[10]   Pressure gradient effects on the large-scale structure of turbulent boundary layer [J].
Harun, Zambri ;
Monty, Jason P. ;
Mathis, Romain ;
Marusic, Ivan .
JOURNAL OF FLUID MECHANICS, 2013, 715 :477-498