• Open Access

Separating adverse-pressure-gradient and Reynolds-number effects in turbulent boundary layers

C. Sanmiguel Vila, R. Vinuesa, S. Discetti, A. Ianiro, P. Schlatter, and R. Örlü
Phys. Rev. Fluids 5, 064609 – Published 17 June 2020

Abstract

Zero pressure-gradient (ZPG) turbulent boundary layers (TBLs) at high Reynolds numbers (Re) and TBLs with adverse pressure gradients (APGs) share some similarities such as the emergence of an outer peak in the streamwise variance profile related to the enhancement of large-scale energy. Reynolds-number and pressure-gradient effects tend to cause such an energizing of the outer-layer structures, which makes it difficult to distinguish them, mainly because both effects are usually coupled. Using two experimental data sets of ZPG and APG TBLs in which Re and pressure gradient are analyzed independently, the present paper shows that the two effects have different imprints on the flow. In particular, the analysis shows that (1) the small-scale energy in APG TBLs is, contrary to canonical ZPG TBLs, not universal, but is dependent on the APG strength, (2) the APG enhances both the small- and large-scale energy in the outer region, and (3) the outer-peak location and the amplitude of the streamwise variance scale differently for increasing Re and APG magnitude. These findings may have ramifications on the development of turbulence models since the pressure gradient has a direct influence on the near-wall dynamics.

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  • Received 15 October 2019
  • Accepted 21 May 2020

DOI:https://doi.org/10.1103/PhysRevFluids.5.064609

Published by the American Physical Society under the terms of the Creative Commons Attribution 4.0 International license. Further distribution of this work must maintain attribution to the author(s) and the published article's title, journal citation, and DOI. Funded by Bibsam.

Published by the American Physical Society

Physics Subject Headings (PhySH)

Fluid Dynamics

Authors & Affiliations

C. Sanmiguel Vila1, R. Vinuesa2, S. Discetti1, A. Ianiro1, P. Schlatter2, and R. Örlü2,*

  • 1Aerospace Engineering Research Group, Universidad Carlos III de Madrid, 28911 Leganés, Spain
  • 2SimEx/FLOW, Engineering Mechanics, KTH Royal Institute of Technology, 100 44 Stockholm, Sweden

  • *Corresponding author: orlu@kth.se

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Vol. 5, Iss. 6 — June 2020

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