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The unsteady wall shear stress vector of a high Reynolds number turbulent pipe flow obtained with multi-aperture defocusing microscopic particle tracking

Klinner, Joachim und Willert, Christian und Magnani, Lorenzo und Talamelli, Alessandro und Bellani, Gabrielle (2026) The unsteady wall shear stress vector of a high Reynolds number turbulent pipe flow obtained with multi-aperture defocusing microscopic particle tracking. In: Proceedings of the 21st International Symposium on Applications of Laser and Imaging Techniques to Fluid Mechanics. 22st International Symposium on Applications of Laser and Imaging Techniques to Fluid Mechanics, 2026-06-29 - 2026-07-02, Lisbon, Portugal. ISBN ISBN 978-989-53637-2-8.

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Offizielle URL: https://www.lisbonsymposia.org/22nd-lxsymp

Kurzfassung

This study presents the first unsteady measurement of the wall shear stress (WSS) vector in a turbulent pipe flow up to Re_tau = 28400 using a single-camera, 3d-3c multi-aperture microscopic particle tracking velocimetry (MA-µPTV) system. By illuminating tracer particles from the side, the setup achieves higher scattering efficiency and reduces light scattering from window inclusions compared to backscattering configurations, doubling the number of successfully reconstructed particle triplets. This enables a spatial resolution of binaveraged statistics of 8 µm - approximately half the smallest viscous length scale - allowing direct access to the viscous sublayer and capturing near-wall turbulence with unprecedented fidelity. Velocity statistics up to the fourth moment are resolved at wall distances up to 600 µm. The probability density functions (PDFs) and joint PDFs of the WSS and its rate of change exhibit strong Reynolds number independence, indicating self-similar near-wall dynamics governed by local viscous scaling. While streamwise WSS fluctuations follow expected scaling, the spanwise component tau_z,rms remains significantly underestimated compared to flat plate turbulent boundary layer (TBL) correlations, even after extrapolation to y+ = 0. In contrast, the spanwise component agrees with pipe flow direct numerical simulation (DNS) data within measurement uncertainty, likely due to geometric confinement and suppression of large-scale spanwise coherent structures compared to flat plate flow. These results contribute to establishing a new experimental benchmark for high-Reynolds-number wall-bounded turbulence.

elib-URL des Eintrags:https://elib.dlr.de/226517/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:The unsteady wall shear stress vector of a high Reynolds number turbulent pipe flow obtained with multi-aperture defocusing microscopic particle tracking
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Klinner, JoachimJoachim.Klinner (at) dlr.dehttps://orcid.org/0000-0003-2709-9664226780458
Willert, ChristianChris.Willert (at) dlr.dehttps://orcid.org/0000-0002-1668-0181NICHT SPEZIFIZIERT
Magnani, LorenzoUniversity of Bologna, ItalyNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Talamelli, AlessandroUniversity of Bologna, ItalyNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Bellani, GabrielleUniversity of Bologna, ItalyNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:29 Juni 2026
Erschienen in:Proceedings of the 21st International Symposium on Applications of Laser and Imaging Techniques to Fluid Mechanics
Referierte Publikation:Ja
Open Access:Ja
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
ISBN:ISBN 978-989-53637-2-8
Status:veröffentlicht
Stichwörter:fluid flow measurement, turbulent boundary layer, pipe flow, aperture encoding, particle tracking, PTV
Veranstaltungstitel:22st International Symposium on Applications of Laser and Imaging Techniques to Fluid Mechanics
Veranstaltungsort:Lisbon, Portugal
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:29 Juni 2026
Veranstaltungsende:2 Juli 2026
Veranstalter :Instituto Superior Técnico, Universidade de Lisboa, Portugal
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Effizientes Luftfahrzeug
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L EV - Effizientes Luftfahrzeug
DLR - Teilgebiet (Projekt, Vorhaben):L - Virtuelles Flugzeug und Validierung
Standort: Köln-Porz
Institute & Einrichtungen:Institut für Antriebstechnik > Triebwerksmesstechnik
Hinterlegt von: Klinner, Dr.-Ing. Joachim
Hinterlegt am:15 Sep 2026 15:16
Letzte Änderung:15 Sep 2026 15:17

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