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Widest scales in channel flow at Reτ = 550
KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics.ORCID iD: 0000-0002-7195-1650
Divisao de Engenharia Aeronáutica, ITA, 12228-900, Sao José dos Campos, SP, Brazil.ORCID iD: 0000-0003-4283-0232
KTH, School of Engineering Sciences (SCI), Centres, Linné Flow Center, FLOW. KTH, Centres, SeRC - Swedish e-Science Research Centre. KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics.ORCID iD: 0000-0001-9627-5903
KTH, School of Engineering Sciences (SCI), Centres, Linné Flow Center, FLOW. KTH, Centres, SeRC - Swedish e-Science Research Centre. KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics.ORCID iD: 0000-0001-6570-5499
(English)Manuscript (preprint) (Other academic)
Abstract [en]

The widest scales in turbulent channel flows are studied through the use of three periodic channel-flow simulations at friction Reynolds number Reτ=550. The length and height of the channels are the same in all cases (Lx/h=8π and Ly/h=2 respectively), while the width is progressively doubled: Lz/h = {4π, 8π, 16π}. The domain width has an effect on the turbulence statistics of a similar order as the error of convergence. Note that a channel flow similar to the smaller one from Del Álamo, Jiménez, Zandonade & Moser (J.~Fluid Mech., vol. 500, 2004, pp. 135--144), which was averaged over a very long time, was used for the comparison of the results. The one-dimensional spanwise spectrum of the streamwise velocity is performed with the aim of assessing the domain-size effect on the widest scales. Our results indicate that 90% of the total streamwise energetic fluctuations is recovered without a significant influence of the size of the domain. The remaining 10% of the energy reflects that the widest scales in the outer layer are the ones most significantly affected by the spanwise length of the domain.

Keywords [en]
Turbulence, simulations
National Category
Fluid Mechanics and Acoustics
Identifiers
URN: urn:nbn:se:kth:diva-319941OAI: oai:DiVA.org:kth-319941DiVA, id: diva2:1702757
Note

QC 20221012

Available from: 2022-10-11 Created: 2022-10-11 Last updated: 2022-10-12Bibliographically approved
In thesis
1. Study of adverse-pressure-gradient effects on a flat-plate boundary layer at high Reynolds numbers
Open this publication in new window or tab >>Study of adverse-pressure-gradient effects on a flat-plate boundary layer at high Reynolds numbers
2022 (English)Doctoral thesis, comprehensive summary (Other academic)
Alternative title[sv]
En studie av effekter av negativ tryckgradient på gränsskiktet över en plan platta vid höga Reynolds-tal
Abstract [en]

Turbulent boundary layers are present in many aspects of life, from the weather and wind currents to transportation, production of energy or mixing processes. Understanding turbulent motions can allow for an improvement and development of technical devices, techniques or diagnosis of phenomena where a fluid flow is in the turbulent regime. From the economical and environmental perspectives, knowledge of turbulent boundary layers may help to reduce the drag on aerodynamic surfaces in transportation, thus leading to a reduction in fuel consumption and emissions. It is also possible to enhance the production of energy from wind sources or the harvest of tidal energy. Otherturbulent motions that have recently impacted society are those related to diffusion such as the transport of aerial diseases, or the motions of air in the respiratory system. In all those examples, external pressure gradients or those produced by the curvature of wall surfaces affect the turbulent structures and thus, the outputs that we study such as drag, transport of substances, energetic output, etc. A relevant case is that of adverse pressure gradient, which enhances the wall-normal convection and redistributes the turbulent energy across the turbulent boundary later. In this work, we study a canonical case of an adverse-pressure-gradient turbulent boundary layer, which is the flow over a flat plate, under near-equilibrium adverse-pressure-gradient conditions. We have extended the previous datasets on flat-plate boundary layers under adverse pressure gradients which were obtained at low Reynolds numbers, with a new numerical simulation reaching high Reynolds numbers, comparable to those of experimental campaigns. This new data set allowed us to study both adverse-pressure-gradient and Reynolds-number effects, where the thicker boundary layer exhibits a clear separation of turbulent scales. The influence of the size of the domain and the wider turbulent scales are analyzed through a set of turbulent channel-flow simulations and the spectral analysis of the Reynolds stresses in high Reynolds numbers turbulent boundary layers. The impact of the wider scales was analyzed and scaling factors were found for different regions of the spectra of the Reynolds stresses. In particular, we propose a new scaling for the energy of the small scales that have been advected to the outer region of the boundary layer.

Place, publisher, year, edition, pages
Sweden 2022: KTH Royal Institute of Technology, 2022. p. 177
Series
TRITA-SCI-FOU ; 2022:47
Keywords
Turbulence, simulations, turbulent boundary layers, adverse pressure gradients.
National Category
Fluid Mechanics and Acoustics
Research subject
Engineering Mechanics
Identifiers
urn:nbn:se:kth:diva-319942 (URN)978-91-8040-353-5 (ISBN)
Public defence
2022-11-03, F3, Lindstedtsvägen 26, KTH, Stockholm, 14:00 (English)
Opponent
Supervisors
Note

QC 221012

Available from: 2022-10-12 Created: 2022-10-11 Last updated: 2022-10-24Bibliographically approved

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Pozuelo, RamonSchlatter, PhilippVinuesa, Ricardo

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