The response of a turbulent boundary layer to a sudden ridge-type roughness array with a sinusoidal pattern

IF 2.8 2区 工程技术 Q2 ENGINEERING, MECHANICAL Experimental Thermal and Fluid Science Pub Date : 2025-02-19 DOI:10.1016/j.expthermflusci.2025.111444
Francesco Scarano , Tomek Jaroslawski , Erwin R. Gowree
{"title":"The response of a turbulent boundary layer to a sudden ridge-type roughness array with a sinusoidal pattern","authors":"Francesco Scarano ,&nbsp;Tomek Jaroslawski ,&nbsp;Erwin R. Gowree","doi":"10.1016/j.expthermflusci.2025.111444","DOIUrl":null,"url":null,"abstract":"<div><div>An experimental investigation was conducted to analyze the impact of a sinusoidal ridge-type roughness patch on the response of a moderate Reynolds number turbulent boundary layer (friction Reynolds number <span><math><mrow><mi>R</mi><msub><mrow><mi>e</mi></mrow><mrow><mi>τ</mi></mrow></msub><mo>&lt;</mo><mn>1100</mn></mrow></math></span>). A streamwise sinusoidal pattern with an amplitude denoted as <span><math><mi>A</mi></math></span> and a wavelength <span><math><mi>Λ</mi></math></span> was imposed on the ridges while maintaining fixed the spanwise spacing between the ridges, <span><math><mi>S</mi></math></span>, smaller than the boundary layer thickness, <span><math><msub><mrow><mi>δ</mi></mrow><mrow><mo>.</mo><mn>99</mn></mrow></msub></math></span> (<span><math><mrow><mi>S</mi><mo>/</mo><msub><mrow><mi>δ</mi></mrow><mrow><mo>.</mo><mn>99</mn></mrow></msub><mo>&lt;</mo><mn>1</mn></mrow></math></span>). Two sinusoidal ridges are tested plus the standard straight configuration; the wavelengths being <span><math><mrow><mn>2</mn><mo>.</mo><mn>6</mn><msub><mrow><mi>δ</mi></mrow><mrow><mo>.</mo><mn>99</mn></mrow></msub></mrow></math></span> and <span><math><mrow><mn>1</mn><mo>.</mo><mn>3</mn><msub><mrow><mi>δ</mi></mrow><mrow><mo>.</mo><mn>99</mn></mrow></msub></mrow></math></span>. Oil droplet interferometric measurement conducted downstream the ridges, in the recessed part, revealed a local reduction in skin friction for the sinusoidal ridged configurations. Hot-wire anemometry was employed to measure the boundary layer on the smooth wall downstream of the roughness array. The measurements revealed a modification of the mean velocity profile and an increase in the shape factor. Significant modifications in spectral content between configurations with aligned and sinusoidal ridge-type roughness are shown. The presence of ridges caused a noticeable upward shift of energy and the emergence of an outer peak in the contour of the premultiplied energy spectrogram. The outer peak is located at a wall normal distance in wall units between 80 and 180 depending on the Reynolds number. Interestingly, configurations with sinusoidal patterns exhibited a more pronounced upward shift of energy in the premultiplied spectra. The energy associated with the outer peak for the configuration having shorter wavelength is doubled compared with standard straight ridges. These findings suggest that the response of the turbulent boundary layer is influenced not solely by the spanwise spacing of ridges but also by the waviness of the ridges, which further contributes to its intensification.</div></div>","PeriodicalId":12294,"journal":{"name":"Experimental Thermal and Fluid Science","volume":"165 ","pages":"Article 111444"},"PeriodicalIF":2.8000,"publicationDate":"2025-02-19","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Experimental Thermal and Fluid Science","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S089417772500038X","RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ENGINEERING, MECHANICAL","Score":null,"Total":0}
引用次数: 0

Abstract

An experimental investigation was conducted to analyze the impact of a sinusoidal ridge-type roughness patch on the response of a moderate Reynolds number turbulent boundary layer (friction Reynolds number Reτ<1100). A streamwise sinusoidal pattern with an amplitude denoted as A and a wavelength Λ was imposed on the ridges while maintaining fixed the spanwise spacing between the ridges, S, smaller than the boundary layer thickness, δ.99 (S/δ.99<1). Two sinusoidal ridges are tested plus the standard straight configuration; the wavelengths being 2.6δ.99 and 1.3δ.99. Oil droplet interferometric measurement conducted downstream the ridges, in the recessed part, revealed a local reduction in skin friction for the sinusoidal ridged configurations. Hot-wire anemometry was employed to measure the boundary layer on the smooth wall downstream of the roughness array. The measurements revealed a modification of the mean velocity profile and an increase in the shape factor. Significant modifications in spectral content between configurations with aligned and sinusoidal ridge-type roughness are shown. The presence of ridges caused a noticeable upward shift of energy and the emergence of an outer peak in the contour of the premultiplied energy spectrogram. The outer peak is located at a wall normal distance in wall units between 80 and 180 depending on the Reynolds number. Interestingly, configurations with sinusoidal patterns exhibited a more pronounced upward shift of energy in the premultiplied spectra. The energy associated with the outer peak for the configuration having shorter wavelength is doubled compared with standard straight ridges. These findings suggest that the response of the turbulent boundary layer is influenced not solely by the spanwise spacing of ridges but also by the waviness of the ridges, which further contributes to its intensification.
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
求助全文
约1分钟内获得全文 去求助
来源期刊
Experimental Thermal and Fluid Science
Experimental Thermal and Fluid Science 工程技术-工程:机械
CiteScore
6.70
自引率
3.10%
发文量
159
审稿时长
34 days
期刊介绍: Experimental Thermal and Fluid Science provides a forum for research emphasizing experimental work that enhances fundamental understanding of heat transfer, thermodynamics, and fluid mechanics. In addition to the principal areas of research, the journal covers research results in related fields, including combined heat and mass transfer, flows with phase transition, micro- and nano-scale systems, multiphase flow, combustion, radiative transfer, porous media, cryogenics, turbulence, and novel experimental techniques.
期刊最新文献
Editorial Board Collision and spreading behavior of rapid tin droplets on stainless-steel substrate surfaces under ultrasonic vibration Heating at different zones on the airfoil: Experimental study on boundary layer flow and convection heat transfer scaling Spreading characteristics of water droplets impacting onto a moving hydrophilic surface The response of a turbulent boundary layer to a sudden ridge-type roughness array with a sinusoidal pattern
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1