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A comparison of opposition control in turbulent boundary layer and turbulent channel flow
KTH, School of Engineering Sciences (SCI), Mechanics, Stability, Transition and Control. KTH, School of Engineering Sciences (SCI), Centres, Linné Flow Center, FLOW.ORCID iD: 0000-0001-9627-5903
2015 (English)In: Physics of fluids, ISSN 1070-6631, E-ISSN 1089-7666, Vol. 27, no 7, 075101Article in journal (Refereed) Published
Abstract [en]

A comparison between classical opposition control applied in the configuration of a fully developed turbulent channel flow and applied locally in a spatially developing turbulent boundary layer is presented. It is found that the control scheme yields similar drag reduction rates if compared at the same friction Reynolds numbers. However, a detailed analysis of the dynamical contributions to the skin friction coefficient reveals significant differences in the mechanism behind the drag reduction. While drag reduction in turbulent channel flow is entirely based on the attenuation of the Reynolds shear stress, the modification of the spatial flow development is essential for the turbulent boundary layer in terms of achievable drag reduction. It is shown that drag reduction due to this spatial development contribution becomes more pronounced with increasing Reynolds number (up to Re-tau = 660, based on friction velocity and boundary layer thickness) and even exceeds drag reduction due to attenuation of the Reynolds shear stress. In terms of an overall energy balance, it is found that opposition control is less efficient in the turbulent boundary layer due to the inherently larger fluctuation intensities in the near wall region.

Place, publisher, year, edition, pages
2015. Vol. 27, no 7, 075101
National Category
Fluid Mechanics and Acoustics
URN: urn:nbn:se:kth:diva-172724DOI: 10.1063/1.4923234ISI: 000358872200030ScopusID: 2-s2.0-84939208971OAI: diva2:849331

QC 20150828

Available from: 2015-08-28 Created: 2015-08-27 Last updated: 2015-08-28Bibliographically approved

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Schlatter, Philipp
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Stability, Transition and ControlLinné Flow Center, FLOW
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