Scaling and statistics of large-defect adverse pressure gradient turbulent boundary layers

A. G. Gungor*, Y. Maciel, M. P. Simens, J. Soria

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

56 Citations (Scopus)

Abstract

The purpose of this article is to test similarity laws and scaling ideas, as well as characterize turbulence behaviour of large-defect adverse-pressure gradient turbulent boundary layers using six experimental and numerical databases including a new direct numerical simulation of a strongly decelerated non-equilibrium turbulent boundary layer. In the latter flow, at a moderate Reynolds number, the mean velocity profiles depart from the classical law of the wall throughout the inner region including in the viscous sublayer and they do not follow the log law. However, the agreement is excellent with the extended law of the wall that accounts for the pressure gradient for the viscous sublayer. The Reynolds stress components are not self-similar in the viscous sublayer when the velocity defect is important, but they scale reasonably well with the pressure-viscous scales.Detailed comparisons of the six different flows are made in the outer region. In order to do such comparisons, an outer region velocity scale analogous to the commonly defined free shear layer velocity scales is introduced. It is found that the investigated one-point velocity statistics in the upper half of large-defect boundary layers resemble those of a mixing layer: mean velocity defect, Reynolds stresses, turbulent kinetic energy budgets, uv correlation factor and structure parameter -〈uv〉/2k. The dominant peaks of turbulence production and Reynolds stresses are located roughly in the middle of the boundary layer. The profiles of the uv correlation factor reveal that u and v become less correlated throughout the boundary layer as the mean velocity defect increases, especially near the wall. The structure parameter is low in the large-defect disequilibrium boundary layers, similar to large-defect equilibrium flows and mixing layers and decreases as the mean velocity defect increases. All large-velocity-defect boundary layers analysed are found to be less efficient in extracting turbulent energy from the mean flow than zero-pressure-gradient turbulent boundary layers, even throughout the outer region.

Original languageEnglish
Pages (from-to)109-124
Number of pages16
JournalInternational Journal of Heat and Fluid Flow
Volume59
DOIs
Publication statusPublished - 1 Jun 2016

Bibliographical note

Publisher Copyright:
© 2016 Elsevier Inc.

Funding

Funded in part by the Multiflow program of the European Research Council under grant ERC-2010. AdG-20100224. YM and JS were supported in part respectively by NSERC Discovery Grant of Canada and ARC Discovery Grant of Australia DP130103621. YM thanks TUBITAK (2221 Program) for supports during the collaboration stay in Turkey. The computations were made possible by generous grants of computer time from Barcelona Supercomputing Center (Spain) under Project number FI-2015-2- 0031 and from the National Center for High Performance Computing of Turkey (UYBHM) under Grant number 1002222012. The authors would like to thank Prof. Jiménez for organizing the First Multiflow Summer Workshop and for suggesting the idea of comparing large-defect boundary layers with mixing layers.

FundersFunder number
National Center for High Performance Computing of Turkey
UYBHM1002222012
Natural Sciences and Engineering Research Council of Canada
European Research CouncilERC-2010
Australian Research CouncilDP130103621
Barcelona Supercomputing CenterFI-2015-2- 0031

    Keywords

    • Adverse pressure gradient
    • Direct numerical simulation
    • Turbulent boundary layer

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