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

被引:2
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
[11]   Turbulent drag reduction by anisotropic permeable substrates - analysis and direct numerical simulations [J].
Gomez-de-Segura, G. ;
Garcia-Mayoral, R. .
JOURNAL OF FLUID MECHANICS, 2019, 875 :124-172
[12]   Skin friction drag reduction over staggered three dimensional cavities [J].
Gowree, Erwin R. ;
Jagadeesh, Chetan ;
Atkin, Christopher J. .
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 84 (520-529) :520-529
[13]   Nature of sweep and ejection events in transitional and turbulent boundary layers [J].
Guo, H. ;
Borodulin, V. I. ;
Kachanov, Y. S. ;
Pan, C. ;
Wang, J. J. ;
Lian, Q. X. ;
Wang, S. F. .
JOURNAL OF TURBULENCE, 2010, 11 (34) :1-51
[14]  
Heinemann P., 55 AIAA AEROSPACE SC, DOI DOI 10.2514/6.2017-1390
[15]   Evidence of very long meandering features in the logarithmic region of turbulent boundary layers [J].
Hutchins, N. ;
Marusic, Ivan .
JOURNAL OF FLUID MECHANICS, 2007, 579 :1-28
[16]   A direct measure of the frequency response of hot-wire anemometers: temporal resolution issues in wall-bounded turbulence [J].
Hutchins, N. ;
Monty, J. P. ;
Hultmark, M. ;
Smits, A. J. .
EXPERIMENTS IN FLUIDS, 2015, 56 (01)
[17]   Accurate measurements of local skin friction coefficient using hot-wire anemometry [J].
Hutchins, N ;
Choi, KS .
PROGRESS IN AEROSPACE SCIENCES, 2002, 38 (4-5) :421-446
[18]   Hot-wire spatial resolution issues in wall-bounded turbulence [J].
Hutchins, N. ;
Nickels, T. B. ;
Marusic, I. ;
Chong, M. S. .
JOURNAL OF FLUID MECHANICS, 2009, 635 :103-136
[19]   Finite-length porous surfaces for control of a turbulent boundary layer [J].
Jafari, Azadeh ;
Cazzolato, Benjamin ;
Arjomandi, Maziar .
PHYSICS OF FLUIDS, 2022, 34 (04)
[20]   Effect of uniform blowing/suction in a turbulent boundary layer at moderate Reynolds number [J].
Kametani, Yukinori ;
Fukagata, Koji ;
Orlu, Ramis ;
Schlatter, Philipp .
INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 2015, 55 :132-142