Modification of near-wall turbulence in turbulent boundary layers due to a perforated structure

被引:1
作者
Hoang, V. T. [1 ]
Jafari, A. [1 ]
Cazzolato, B. [1 ]
Arjomandi, M. [1 ]
机构
[1] Univ Adelaide, Sch Elect & Mech Engn, Adelaide, SA 5005, Australia
基金
澳大利亚研究理事会;
关键词
DRAG REDUCTION; SPATIAL-RESOLUTION; REGION; SMOOTH; PLATE;
D O I
10.1063/5.0213907
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This study investigates the potential of a perforated structure for the control of near-wall turbulence in turbulent boundary layers. The perforated structure consists of a perforated plate, underneath of which is a backing chamber. The near-wall turbulent structures were analyzed using hot-wire measurements. Different inner-scaled chamber volumes from V+ = 2.4 x 10(6) to 11.5 x 10(6) were considered to manipulate turbulent boundary layers at two Reynolds numbers of Re-theta = 1165 and 2294. The findings reveal significant effects of the perforated structure on near-wall turbulent structures. Statistical analysis utilizing a variable-interval time-averaging technique illustrated a reduction of up to about 9% in sweep and ejection intensity, a decrease in about 25% in ejection frequency, and a decrease in approximately 33.5% in sweep frequency within the near-wall region, y(+) <= 30, indicating that the perforated structure weakened burst events in this region. In addition, the perforated structure lifted the turbulence energy further from the wall. Consequently, there was a reduction of up to approximately 9% in turbulence intensities near the wall, contributing to locally diminished shear stresses and skin friction drag. When the inner-scaled chamber volume increased, the reduction in near-wall turbulence became more pronounced. (c) 2024 Author(s). All article content, except where otherwise noted, is licensed under a Creative Commons Attribution-NonCommercial 4.0International (CC BY-NC) license (https://creativecommons.org/licenses/by-nc/4.0/).
引用
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页数:18
相关论文
共 51 条
[1]  
[Anonymous], 1987, Analysis of the motions and effects of hairpin vortices
[2]   RESPONSE OF A TURBULENT BOUNDARY LAYER TO A STEP CHANGE IN SURFACE ROUGHNESS .1. SMOOTH TO ROUGH [J].
ANTONIA, RA ;
LUXTON, RE .
JOURNAL OF FLUID MECHANICS, 1971, 48 (AUG27) :721-&
[3]   Numerical modeling of anisotropic drag for a perforated plate with cylindrical holes [J].
Bae, Youngmin ;
Kim, Young In .
CHEMICAL ENGINEERING SCIENCE, 2016, 149 :78-87
[4]   Mechanism of control of the near-wall turbulence using a micro-cavity array [J].
Bhat, S. S. ;
Silvestri, A. ;
Cazzolato, B. S. ;
Arjomandi, M. .
PHYSICS OF FLUIDS, 2021, 33 (07)
[5]   Skin-friction reduction using periodic blowing through streamwise slits [J].
Cheng, X. Q. ;
Qiao, Z. X. ;
Zhang, X. ;
Quadrio, M. ;
Zhou, Y. .
JOURNAL OF FLUID MECHANICS, 2021, 920
[6]  
Coxe D., 2019, Drag reduction in turbulent pipe flow by transverse wall oscillations at low and moderate Reynolds number
[7]   Reynolds-number scaling of the flat-plate turbulent boundary layer [J].
DeGraaff, DB ;
Eaton, JK .
JOURNAL OF FLUID MECHANICS, 2000, 422 :319-346
[8]   Development of a turbulent boundary layer after a step from smooth to rough surface [J].
Efros, Vladislav ;
Krogstad, Per-Age .
EXPERIMENTS IN FLUIDS, 2011, 51 (06) :1563-1575
[9]  
Gak-El-Hak M., 1996, Appl. Mech. Rev, V49, P365, DOI [10.1115/1.3101931, DOI 10.1115/1.3101931]
[10]   Analysis of the turbulent boundary layer in the vicinity of a self-excited cylindrical Helmholtz resonator [J].
Ghanadi, Farzin ;
Arjomandi, Maziar ;
Cazzolato, Benjamin S. ;
Zander, Anthony C. .
JOURNAL OF TURBULENCE, 2015, 16 (08) :705-728