Two separate experimental campaigns of a spatially developing turbulent boundary layer under approximately zero-pressure-gradient at moderate Reynolds numbers () are conducted with stereoscopic Particle Image Velocimetry (PIV) and one component Hot Wire Anemometry. This range of Reynolds numbers is found to be of particular interest for turbulent boundary layer control investigations. The motivations behind this work rely on the lack of recent studies that provide a rigorous experimental database on a flat plate turbulent boundary layer, openly available online. This is critical as, in most of the cases, the modification of the statistics resulting from turbulent boundary layer control strategies are compared with a smooth baseline reference. The statistics of the velocity fields, obtained with the two techniques, show a good match with the direct numerical simulation in literature results. We focused on the skin friction evaluation by means of Clauser's chart technique. The near wall turbulence activity and the associated coherent structures are investigated by means of the Variable Interval Time Averaging technique using the hot wire signal. The influence of the acquisition and algorithm parameters as well as the effect of the Reynolds number are reported. The logarithmic and outer structures are investigated by applying the Uniform Momentum Zones technique to the PIV dataset. The hierarchical distribution of the uniform momentum zones as a function of the wall distance as well as their variation with the Reynolds number confirm the validity of the attached eddy model even at the moderate Reynolds numbers of the current investigation.
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November 2022
Research Article|
November 18 2022
On the turbulent boundary layer over a flat plate at moderate Reynolds numbers Available to Purchase
Francesco Scarano
;
Francesco Scarano
a)
(Conceptualization, Data curation, Investigation, Methodology, Writing – original draft, Writing – review & editing)
1
Département Aérodynamique et Propulsion (DAEP) ISAE-SUPAERO, Université de Toulouse
, 10, avenue Edouard Belin 31400, Toulouse, France
a)Author to whom correspondence should be addressed: [email protected]
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Marc C. Jacob
;
Marc C. Jacob
(Conceptualization, Funding acquisition, Project administration, Supervision, Writing – review & editing)
2
Laboratoire de Mécanique des Fluides et d'Acoustique, Ecole Centrale de Lyon
, France
; Institut National des Sciences Appliquées Lyon
, France
; and Université Claude Bernard Lyon I, Centre National de Recherche Scientifique, Université de Lyon
, 36 av. Guy de Collongue, F-69134 Ecully, France
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Xavier Carbonneau
;
Xavier Carbonneau
(Supervision)
1
Département Aérodynamique et Propulsion (DAEP) ISAE-SUPAERO, Université de Toulouse
, 10, avenue Edouard Belin 31400, Toulouse, France
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Erwin R. Gowree
Erwin R. Gowree
(Conceptualization, Funding acquisition, Investigation, Supervision, Writing – review & editing)
1
Département Aérodynamique et Propulsion (DAEP) ISAE-SUPAERO, Université de Toulouse
, 10, avenue Edouard Belin 31400, Toulouse, France
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Francesco Scarano
1,a)
Marc C. Jacob
2
Xavier Carbonneau
1
Erwin R. Gowree
1
1
Département Aérodynamique et Propulsion (DAEP) ISAE-SUPAERO, Université de Toulouse
, 10, avenue Edouard Belin 31400, Toulouse, France
2
Laboratoire de Mécanique des Fluides et d'Acoustique, Ecole Centrale de Lyon
, France
; Institut National des Sciences Appliquées Lyon
, France
; and Université Claude Bernard Lyon I, Centre National de Recherche Scientifique, Université de Lyon
, 36 av. Guy de Collongue, F-69134 Ecully, France
a)Author to whom correspondence should be addressed: [email protected]
Physics of Fluids 34, 115150 (2022)
Article history
Received:
September 06 2022
Accepted:
October 28 2022
Citation
Francesco Scarano, Marc C. Jacob, Xavier Carbonneau, Erwin R. Gowree; On the turbulent boundary layer over a flat plate at moderate Reynolds numbers. Physics of Fluids 1 November 2022; 34 (11): 115150. https://doi.org/10.1063/5.0124498
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