Friction drag reduction achievable by near-wall turbulence manipulation in spatially developing boundary-layer

被引:7
作者
Bannier, Amaury [1 ]
Garnier, Eric [1 ]
Sagaut, Pierre [2 ]
机构
[1] ONERA French Aerosp Lab, Appl Aerodynam Dept, F-92190 Meudon, France
[2] Aix Marseille Univ, CNRS, Cent Marseille, M2P2,UMR 7340, F-13451 Marseille, France
关键词
SKIN-FRICTION; STRESS; FLOW;
D O I
10.1063/1.4943625
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Various control strategies, such as active feedback control or riblets, end up restraining near-wall turbulence. An analytical study is conducted to estimate the drag-reduction achievable by such control in zero-pressure-gradient turbulent boundary-layers. Based on an idealized control which damps all fluctuations within a near-wall layer, a composite flow profile is established. It leads to explicit models for both the drag-reduction and the boundary-layer development rate. A skin-friction decomposition is applied and gives physical insights on the underlying phenomena. The control is found to alter the spatial development of the boundary-layer, resulting in detrimental impact on the skin-friction. However, the drag-reducing mechanism, attributed to the turbulence weakening, is found predominant and massive drag reductions remain achievable at high Reynolds number, although a minute part of the boundary-layer is manipulated. The model is finally assessed against Large Eddy Simulations of riblet-controlled flow. (C) 2016 AIP Publishing LLC.
引用
收藏
页数:16
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