Lemarechal, Jonathan (2017) Transition Delay by Oblique Roughness Elements in a Blasius Boundary-Layer Flow. In: 56th AIAA Aerospace Sciences Meeting. Doktoranden Seminar des Instituts für Aerodynamik, 2017-12-19, Stuttgart, Deutschland. doi: 10.2514/6.2018-1057. ISBN 978-162410524-1.
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Kurzfassung
A passive device to delay the laminar-turbulent transition in a Blasius boundary-layer flow is tested at low Reynolds numbers in the laminar water channel. The passive device consists of oblique surface roughness elements lined up perpendicular to the flow. Each element has the shape of a cuboid, is oriented 45° to the direction of the oncoming flow, and generates a non-symmetric vortex system. These vortices generate high and low speed streaks inside of the boundary layer through the lift-up effect. The streaks alter the two-dimensional (2D) boundary layer into a three-dimensional (3D) one. For correctly placed and sized roughness elements the 2D Tollmien-Schlichting wave is altered into a 3D less amplified wave and the transition occurs further downstream. The flow is investigated by means of surface visualizations with the Temperature-Sensitive Paint (TSP) method and velocity measurements with hot-film anemometry. With the TSP method the laminar-turbulent transition was measured with high spatial and temporal resolution. The changes of transition location and changes of transition mechanism are weil captured.
elib-URL des Eintrags: | https://elib.dlr.de/118680/ | ||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||
Titel: | Transition Delay by Oblique Roughness Elements in a Blasius Boundary-Layer Flow | ||||||||
Autoren: |
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Datum: | 2017 | ||||||||
Erschienen in: | 56th AIAA Aerospace Sciences Meeting | ||||||||
Referierte Publikation: | Nein | ||||||||
Open Access: | Nein | ||||||||
Gold Open Access: | Nein | ||||||||
In SCOPUS: | Ja | ||||||||
In ISI Web of Science: | Nein | ||||||||
DOI: | 10.2514/6.2018-1057 | ||||||||
ISBN: | 978-162410524-1 | ||||||||
Status: | veröffentlicht | ||||||||
Stichwörter: | laminar-turbulent transition, Blasius boundary layer, k-type transition, passive transition delay, streaks, temperature-sensitive paint, TSP, hot-film anemometry, laminar water channel, Laminarwasserkanal, low Reynolds number experiment | ||||||||
Veranstaltungstitel: | Doktoranden Seminar des Instituts für Aerodynamik | ||||||||
Veranstaltungsort: | Stuttgart, Deutschland | ||||||||
Veranstaltungsart: | Andere | ||||||||
Veranstaltungsdatum: | 19 Dezember 2017 | ||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||
HGF - Programm: | Luftfahrt | ||||||||
HGF - Programmthema: | Flugzeuge | ||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||
DLR - Forschungsgebiet: | L AR - Aircraft Research | ||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Simulation und Validierung (alt) | ||||||||
Standort: | Göttingen | ||||||||
Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > Experimentelle Verfahren, GO | ||||||||
Hinterlegt von: | Bachmann, Barbara | ||||||||
Hinterlegt am: | 02 Feb 2018 14:38 | ||||||||
Letzte Änderung: | 24 Apr 2024 20:23 |
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