Active control of pressure fluctuations in an incompressible turbulent cavity flow

被引:4
作者
Choi, Jun Nyeong [1 ]
Lee, Jae Hwa [1 ]
机构
[1] Ulsan Natl Inst Sci & Technol UNIST, Dept Mech Engn, 50 UNIST Gil, Ulsan 44919, South Korea
基金
新加坡国家研究基金会;
关键词
Turbulent cavity flow; Large -eddy simulation; Active control; SELF-SUSTAINED OSCILLATIONS; LARGE-EDDY SIMULATION; COMPRESSIBLE FLOW; BOUNDARY-LAYER; SUPPRESSION; LAMINAR;
D O I
10.1016/j.ast.2023.108512
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Large-eddy simulations of incompressible turbulent boundary layer flows over an open cavity are conducted to investigate the effects of wall-normal steady blowing on the suppression of pressure fluctuations on the cavity walls. The length (L) to depth (D) ratio (L/D) of the cavity is 2 and the Reynolds number based on the cavity depth (ReD) is 12,000. Wall-normal steady blowing is imposed through a limited transverse slot in an upstream region of the cavity leading edge while varying the momentum coefficient (C & mu;). As the value of C & mu; increases, the pressure fluctuations on the cavity walls decrease mostly due to weakened impingement of turbulent vortical structures residing in the shear layer on the aft wall by lifting effects, reaching a maximum reduction of -7.61% compared to a baseline when C & mu; = 0.015. However, as the value of C & mu; increases further, the pressure fluctuations increase gradually, exceeding that of a baseline when C & mu; > 0.05. Because intensified turbulent vortical structures in the shear layer with an increase of C & mu; lead to strong interactions of small-scale vortices with the cavity walls with an accompanying large motion of the primary recirculation zone within the cavity, additional pressure fluctuations generated on the cavity walls deteriorate the control performance due to the blowing. & COPY; 2023 Elsevier Masson SAS. All rights reserved.
引用
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页数:14
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