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New Insight Into The Spectra Of Turbulent Boundary Layers With Pressure Gradients.
KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics, Turbulent simulations laboratory.ORCID iD: 0000-0002-7195-1650
KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics.ORCID iD: 0000-0002-6390-0343
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, 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]

In this study, a new well-resolved large-eddy-simulation (LES) of an incompressible near-equilibrium adverse-pressure-gradient (APG) turbulent boundary layer (TBL) over a flat plate is presented. In this simulation, we have established a near-equilibrium APG over a wide Reynolds-number range. In this so-called region of interest (ROI), the Clauser–Rotta pressure-gradient parameter β exhibits an approximately constant value of around 1.4, and the Reynolds number based on momentum thickness reaches Reθ = 8700. To the authors’ knowledge, this is to date the highest Reθ achieved for a near-equilibrium APG TBL under an approximately constant moderate APG. We evaluated the self-similarity of the outer region using two scalings, namely the Zagarola–Smits and an alternative one based on edge velocity and displacement thickness. Our results reveal that outer-layer similarity is achieved, and the viscous scaling collapses the near-wall region of the mean flow in agreement with classical theory. Spectral analysis reveals that the APG displaces some small-scale energy from the near-wall to the outer region, an effect observed for all the components of the Reynolds-stress tensor, which becomes more evident at higher Reynolds numbers. Generally, the effects of the APG are more noticeable at lower Reynolds numbers. For instance, the outer peak of turbulent-kinetic-energy (TKE) production is less prominent at higher Re. While the scale separation increases with Re in zero-pressure-gradient (ZPG) TBLs, this effect becomes accentuated by the APG. Despite the reduction of the outer TKE production at higher Reynolds numbers, the mechanisms of energization of large scales are still present.

Keywords [en]
Turbulence
National Category
Fluid Mechanics and Acoustics
Research subject
Engineering Mechanics
Identifiers
URN: urn:nbn:se:kth:diva-319937OAI: oai:DiVA.org:kth-319937DiVA, id: diva2:1702759
Note

QC 20221012

Available from: 2022-10-11 Created: 2022-10-11 Last updated: 2024-08-14Bibliographically 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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Other links

https://arxiv.org/abs/2207.07777v2

Authority records

Pozuelo, RamonLi, QiangSchlatter, PhilippVinuesa, Ricardo

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Pozuelo, RamonLi, QiangSchlatter, PhilippVinuesa, Ricardo
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