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 , Tomek Jaroslawski , 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><</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><</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 ). A streamwise sinusoidal pattern with an amplitude denoted as and a wavelength was imposed on the ridges while maintaining fixed the spanwise spacing between the ridges, , smaller than the boundary layer thickness, (). Two sinusoidal ridges are tested plus the standard straight configuration; the wavelengths being and . 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.
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.