Ryan, Jacob und Jacobitz, Frank und Costantini, Marco und Lemarechal, Jonathan (2024) On the laminar flow over a cylindrical roughness element. In: 102nd Annual Meeting of the American Association for theAdvancement of Science – Pacific Division, Seite 1. 102nd Annual Meeting of the American Association for theAdvancement of Science – Pacific Division, 2024-06-17 - 2024-06-20, San Diego, CA, USA.
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Offizielle URL: https://www.aaaspd.org/Proceedings2024SanDiego.pdf
Kurzfassung
A direct comparison of experimental and simulation results of two flows, a laminar boundary layer developing on a flat heated plate and the interaction of a laminar boundary layer with a single cylindrical roughness element with a height of the same order of the boundary-layer displacement thickness, is presented. The experiments were performed in a water channel using temperature-sensitive paint (TSP) and the simulations used the Ansys Fluent computational fluid dynamics software. The numerical simulations supplement the experimental data, allowing for a direct comparison with the experiment, and they provide information not easily accessible from the experiment. In the case of the laminar boundary layer developing over a heated flat plate, experimental measurements and simulation results of the surface temperature show strong agreement and a correlation coefficient for the two temperature fields of 0.98 is obtained. In the case of a laminar boundary layer interacting with a low aspect ratio roughness element at a roughness Reynolds number Re = 355, a complex vortical structure is observed. Again good agreement between the experimental and simulation results is obtained with a correlation coefficient of 0.95 for the respective temperature fields.
elib-URL des Eintrags: | https://elib.dlr.de/205140/ | ||||||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||
Zusätzliche Informationen: | https://www.aaaspd.org/index.htm | ||||||||||||||||||||
Titel: | On the laminar flow over a cylindrical roughness element | ||||||||||||||||||||
Autoren: |
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Datum: | Juni 2024 | ||||||||||||||||||||
Erschienen in: | 102nd Annual Meeting of the American Association for theAdvancement of Science – Pacific Division | ||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||
Seitenbereich: | Seite 1 | ||||||||||||||||||||
Name der Reihe: | Proceedings of the American Association for theAdvancement of Science – Pacific Division | ||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||
Stichwörter: | Roughness; Flat Plate; Blasius Boundary Layer; Temperature-Sensitive Paint | ||||||||||||||||||||
Veranstaltungstitel: | 102nd Annual Meeting of the American Association for theAdvancement of Science – Pacific Division | ||||||||||||||||||||
Veranstaltungsort: | San Diego, CA, USA | ||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||
Veranstaltungsbeginn: | 17 Juni 2024 | ||||||||||||||||||||
Veranstaltungsende: | 20 Juni 2024 | ||||||||||||||||||||
Veranstalter : | American Association for theAdvancement of Science – Pacific Division | ||||||||||||||||||||
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: | Göttingen | ||||||||||||||||||||
Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > Experimentelle Verfahren, GO | ||||||||||||||||||||
Hinterlegt von: | Micknaus, Ilka | ||||||||||||||||||||
Hinterlegt am: | 11 Jul 2024 16:42 | ||||||||||||||||||||
Letzte Änderung: | 11 Jul 2024 16:42 |
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