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Characteristics of Reynolds Shear Stress in Adverse Pressure Gradient Turbulent Boundary Layers

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Abstract

The focus of the present work is to characterize the features of the turbulent inertia term (the wall-normal gradient of Reynolds shear stress) through the mean momentum balance and the Reynolds shear stress correlation coefficient (ρuv ). Effects of the Reynolds number and Clauser pressure-gradient parameter, β, are discussed. Large eddy simulations of low Reynolds number adverse pressure gradient turbulent boundary layers from Bobke et al. [1], low Reynolds number experimental data from Vila et al. [2] and Volino [3], and newly acquired experimental data at higher Reynolds number from the Flow Physics Facility at The University of New Hampshire are utilized for this analysis. Observations are compared to zero pressure gradient turbulent boundary layer direct numerical simulations of Schlatter and Örlu [4] and Sillero et al. [5], and experimental data from Zimmerman et al. [6] and Zimmerman [7]. These cases show that the correlation coefficient (ρuv ) decreases in magnitude with increasing Reynolds number and β. However, from these initial observations we find that ρuv is more sensitive to changes in the Reynolds number in comparison to the examined range of β. We also find that the location of zero-crossing of the turbulent inertia term seems to scale with δ+ while the minimum of ρuv scales with δ.

Original languageEnglish
Title of host publicationProgress in Turbulence IX - Proceedings of the iTi Conference in Turbulence, 2021
EditorsRamis Örlü, Alessandro Talamelli, Joachim Peinke, Martin Oberlack
PublisherSpringer Science and Business Media Deutschland GmbH
Pages173-179
Number of pages7
ISBN (Print)9783030807153
DOIs
StatePublished - 2021
Event9th iTi Conference on Turbulence, iTi 2021 - Virtual, Online
Duration: Feb 25 2021Feb 26 2021

Publication series

NameSpringer Proceedings in Physics
Volume267

Conference

Conference9th iTi Conference on Turbulence, iTi 2021
CityVirtual, Online
Period02/25/2102/26/21

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