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A new perspective on skin-friction contributions in adverse-pressure-gradient turbulent boundary layers
KTH, Centres, SeRC - Swedish e-Science Research Centre. KTH, School of Engineering Sciences (SCI), Centres, Linné Flow Center, FLOW. KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics.ORCID iD: 0000-0003-0790-8460
KTH, School of Engineering Sciences (SCI), Centres, Linné Flow Center, FLOW. KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics.ORCID iD: 0000-0003-4109-0009
KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics.ORCID iD: 0000-0002-7195-1650
Department of Mechanical Engineering, Keio University, 223-8522 Yokohama, Japan.ORCID iD: 0000-0003-4805-238X
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(English)Manuscript (preprint) (Other academic)
Abstract [en]

For adverse-pressure-gradient turbulent boundary layers, the study of integral skin-friction contributions still poses significant challenges. Beyond questions related to the integration boundaries and the derivation procedure, which have been thoroughly investigated in the literature, an important issue is how different terms should be aggregated. The nature of these flows, which exhibit significant in-homogeneity in the streamwise direction, usually results in cancellation between several contributions with high absolute values. We propose a formulation of the identity derived by Fukagata, Iwamoto \& Kasagi (Phys. Fluids, vol. 14, 2002, pp. 73--76), which we obtained from the convective form of the governing equations. A new skin-friction contribution is defined, considering wall-tangential convection and pressure gradient together. This contribution is related to the evolution of the dynamic pressure in the mean flow. The results of the decomposition are examined for a broad range of pressure-gradient conditions and different flow-control strategies. We found that the new formulation of the identity allows to readily identify the different regimes of near-equilibrium conditions and approaching separation. It also provides a more effective description of control effects. A similar aggregation between convection and pressure-gradient terms is also possible for any other decomposition where in-homogeneity contributions are considered explicitly. 

Keywords [en]
Turbulence, skin friction, turbulent boundary layers
National Category
Fluid Mechanics
Identifiers
URN: urn:nbn:se:kth:diva-319940OAI: oai:DiVA.org:kth-319940DiVA, id: diva2:1702761
Note

QC 20221012

Available from: 2022-10-11 Created: 2022-10-11 Last updated: 2025-02-09Bibliographically 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
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: 2025-02-09Bibliographically approved

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Atzori, MarcoMallor, FerminPozuelo, RamonVinuesa, RicardoSchlatter, Philipp

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Atzori, MarcoMallor, FerminPozuelo, RamonFukagata, KojiVinuesa, RicardoSchlatter, Philipp
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