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

被引:131
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
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