An improvement of opposition control at high Reynolds numbers

被引:1
|
作者
Pamies, Mathieu [1 ]
Garnier, Eric [1 ]
Sagaut, Pierre [2 ]
Merlen, Alain [3 ]
机构
[1] Off Natl Etud & Rech Aerosp, Appl Aerodynam Dept, BP 72,29 Ave Div Leclerc, F-92322 Chatillon, France
[2] Univ Paris 06, Inst JeanRond Dalambert, F-75252 Paris 05, France
[3] Univ Sci & Technol Lille, Lab Mecanique Lille, F-59655 Villeneuve Dascq, France
关键词
flow control; drag reduction; turbulent boundary layer; LES;
D O I
10.1007/978-1-4020-6858-4_29
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Opposition control is a simple feedback control method traditionnally used to attenuate near-wall turbulence and reduce drag in wall-bounded turbulent flows. The idea is to impose blowing and suction at the wall to counteract near-wall quasi-streamwise vortical structures. Unfortunately, the efficiency of this method decreases as the Reynolds number increases. The present study proposes a simple but efficient modification of opposition control (OC) to increase its performance at large Reynolds numbers. We demonstrate a 300% improvement when performing a blowing-only opposition control (BOOC), where OC's suction part has been removed, on a spatially developing turbulent boundary layer at Re-tau = 920. It is shown that BOOC only applies blowing at the location of high skin friction events, which suppresses the latter without altering the "natural" low skin friction events. As a result, BOOC dramatically changes the probability density profile of wall shear stress but does not weaken turbulence intensity near the wall.
引用
收藏
页码:243 / +
页数:3
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