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Wokoeck, Ralf und Radespiel, Rolf und Ehlers, Hauke und Konrath, Robert (2013) Experimental and numerical investigations of pitch-plunging wing aerodynamics at low Reynolds number. International Journal of Engineering Systems Modelling and Simulation, 5 (1-3), Seiten 19-32. Inderscience Publishers. doi: 10.1504/IJESMS.2013.052370. ISSN 1755-9758.
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Offizielle URL: http://www.inderscience.com/jhome.php?jcode=ijesms
Kurzfassung
In the present paper, the first results of a broad study of static and moving flat plate wings for Micro Air Vehicles, MAVs are presented. Wind tunnel experiments with force measurements and Particle Image Velocimetry, PIV were performed in a specially designed wind tunnel environment for low Reynolds number investigations. Corresponding numerical flow simulations were also carried out. Effects of the wing shape (elliptical and rectangular), the Reynolds number (18000, 36000 and 108000) and the kinematics using different motion forms of pure plunge and combined pitch/plunge with a reduced frequency of k=0.2 are discussed.
| elib-URL des Eintrags: | https://elib.dlr.de/77807/ | ||||||||||||||||||||
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| Dokumentart: | Zeitschriftenbeitrag | ||||||||||||||||||||
| Zusätzliche Informationen: | ISSN online: 1755-9766 | ||||||||||||||||||||
| Titel: | Experimental and numerical investigations of pitch-plunging wing aerodynamics at low Reynolds number | ||||||||||||||||||||
| Autoren: |
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| Datum: | 2013 | ||||||||||||||||||||
| Erschienen in: | International Journal of Engineering Systems Modelling and Simulation | ||||||||||||||||||||
| Referierte Publikation: | Ja | ||||||||||||||||||||
| Open Access: | Nein | ||||||||||||||||||||
| Gold Open Access: | Nein | ||||||||||||||||||||
| In SCOPUS: | Ja | ||||||||||||||||||||
| In ISI Web of Science: | Ja | ||||||||||||||||||||
| Band: | 5 | ||||||||||||||||||||
| DOI: | 10.1504/IJESMS.2013.052370 | ||||||||||||||||||||
| Seitenbereich: | Seiten 19-32 | ||||||||||||||||||||
| Herausgeber: |
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| Verlag: | Inderscience Publishers | ||||||||||||||||||||
| ISSN: | 1755-9758 | ||||||||||||||||||||
| Status: | veröffentlicht | ||||||||||||||||||||
| Stichwörter: | Micro Air Vehicle; MAV; Flapping Wing Kinematics; Low Reynolds Number; Reynolds Number Effect; Low Aspect Ratio; Aspect Ratio Effect; Wing Plan Shape; Vortical Flow Structures; Vortex Interaction; MAV Design; Dynamic Model Support | ||||||||||||||||||||
| HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||
| HGF - Programm: | Luftfahrt | ||||||||||||||||||||
| HGF - Programmthema: | Starrflügler (alt) | ||||||||||||||||||||
| DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||
| DLR - Forschungsgebiet: | L AR - Starrflüglerforschung | ||||||||||||||||||||
| DLR - Teilgebiet (Projekt, Vorhaben): | L - Simulation & Validierung (alt) | ||||||||||||||||||||
| Standort: | Göttingen | ||||||||||||||||||||
| Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > Experimentelle Verfahren | ||||||||||||||||||||
| Hinterlegt von: | Micknaus, Ilka | ||||||||||||||||||||
| Hinterlegt am: | 06 Sep 2013 09:47 | ||||||||||||||||||||
| Letzte Änderung: | 23 Jun 2023 11:24 |
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