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A Second Turbulent Regime When a Fully Developed Axial Turbulent Flow Enters a Rotating Pipe

Cloos, Ferdinand-J. ; Zimmermann, Anna-L. ; Pelz, Peter F. (2022)
A Second Turbulent Regime When a Fully Developed Axial Turbulent Flow Enters a Rotating Pipe.
ASME Turbo Expo 2016 - Turbomachinery Technical Conference and Exposition GT2016. Seoul, South Korea (13.06.2016-17.06.2016)
doi: 10.26083/tuprints-00021469
Konferenzveröffentlichung, Zweitveröffentlichung, Postprint

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Kurzbeschreibung (Abstract)

When a fluid enters a rotating circular pipe a swirl boundary layer with thickness of δ̃s appears at the wall and interacts with the axial momentum boundary layer with thickness of δ̃. We investigate a turbulent flow applying Laser-Doppler-Anemometry to measure the circumferential velocity profile at the inlet of the rotating pipe. The measured swirl boundary layer thickness follows a power law taking Reynolds number and flow number into account. A combination of high Reynolds number, high flow number and axial position causes a transition of the swirl boundary layer development in the turbulent regime. At this combination, the swirl boundary layer thickness as well as the turbulence intensity increase and the latter yields a self-similarity. The circumferential velocity profile changes to a new presented self-similarity as well. We define the transition inlet length, where the transition appears and a stability map for the two regimes is given for the case of a fully developed axial turbulent flow enters the rotating pipe.

Typ des Eintrags: Konferenzveröffentlichung
Erschienen: 2022
Autor(en): Cloos, Ferdinand-J. ; Zimmermann, Anna-L. ; Pelz, Peter F.
Art des Eintrags: Zweitveröffentlichung
Titel: A Second Turbulent Regime When a Fully Developed Axial Turbulent Flow Enters a Rotating Pipe
Sprache: Englisch
Publikationsjahr: 2022
Ort: Darmstadt
Publikationsdatum der Erstveröffentlichung: 2016
Verlag: ASME
Buchtitel: Proceedings of ASME Turbo Expo 2016 - Turbomachinery Technical Conference and Exposition GT2016 June 13-17, 2016, Seoul, South Korea. Volume 2B: Turbomachinery
Reihe: Proceedings of ASME Turbo Expo 2016 - Turbomachinery Technical Conference and Exposition GT2016
Band einer Reihe: 2B
Kollation: 9 Seiten
Veranstaltungstitel: ASME Turbo Expo 2016 - Turbomachinery Technical Conference and Exposition GT2016
Veranstaltungsort: Seoul, South Korea
Veranstaltungsdatum: 13.06.2016-17.06.2016
DOI: 10.26083/tuprints-00021469
URL / URN: https://tuprints.ulb.tu-darmstadt.de/21469
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Herkunft: Zweitveröffentlichungsservice
Kurzbeschreibung (Abstract):

When a fluid enters a rotating circular pipe a swirl boundary layer with thickness of δ̃s appears at the wall and interacts with the axial momentum boundary layer with thickness of δ̃. We investigate a turbulent flow applying Laser-Doppler-Anemometry to measure the circumferential velocity profile at the inlet of the rotating pipe. The measured swirl boundary layer thickness follows a power law taking Reynolds number and flow number into account. A combination of high Reynolds number, high flow number and axial position causes a transition of the swirl boundary layer development in the turbulent regime. At this combination, the swirl boundary layer thickness as well as the turbulence intensity increase and the latter yields a self-similarity. The circumferential velocity profile changes to a new presented self-similarity as well. We define the transition inlet length, where the transition appears and a stability map for the two regimes is given for the case of a fully developed axial turbulent flow enters the rotating pipe.

Status: Postprint
URN: urn:nbn:de:tuda-tuprints-214695
Sachgruppe der Dewey Dezimalklassifikatin (DDC): 600 Technik, Medizin, angewandte Wissenschaften > 620 Ingenieurwissenschaften und Maschinenbau
Fachbereich(e)/-gebiet(e): 16 Fachbereich Maschinenbau
16 Fachbereich Maschinenbau > Institut für Fluidsystemtechnik (FST) (seit 01.10.2006)
Hinterlegungsdatum: 07 Jun 2022 13:37
Letzte Änderung: 08 Jun 2022 06:23
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