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Wokoeck, Ralf and Radespiel, Rolf and Ehlers, Hauke and 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), pp. 19-32. Inderscience Publishers. doi: 10.1504/IJESMS.2013.052370. ISSN 1755-9758.
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Official URL: http://www.inderscience.com/jhome.php?jcode=ijesms
Abstract
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.
| Item URL in elib: | https://elib.dlr.de/77807/ | ||||||||||||||||||||
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| Document Type: | Article | ||||||||||||||||||||
| Additional Information: | ISSN online: 1755-9766 | ||||||||||||||||||||
| Title: | Experimental and numerical investigations of pitch-plunging wing aerodynamics at low Reynolds number | ||||||||||||||||||||
| Authors: |
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| Date: | 2013 | ||||||||||||||||||||
| Journal or Publication Title: | International Journal of Engineering Systems Modelling and Simulation | ||||||||||||||||||||
| Refereed publication: | Yes | ||||||||||||||||||||
| Open Access: | No | ||||||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||||||
| In SCOPUS: | Yes | ||||||||||||||||||||
| In ISI Web of Science: | Yes | ||||||||||||||||||||
| Volume: | 5 | ||||||||||||||||||||
| DOI: | 10.1504/IJESMS.2013.052370 | ||||||||||||||||||||
| Page Range: | pp. 19-32 | ||||||||||||||||||||
| Editors: |
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| Publisher: | Inderscience Publishers | ||||||||||||||||||||
| ISSN: | 1755-9758 | ||||||||||||||||||||
| Status: | Published | ||||||||||||||||||||
| Keywords: | 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 - Research field: | Aeronautics, Space and Transport | ||||||||||||||||||||
| HGF - Program: | Aeronautics | ||||||||||||||||||||
| HGF - Program Themes: | Aircraft Research (old) | ||||||||||||||||||||
| DLR - Research area: | Aeronautics | ||||||||||||||||||||
| DLR - Program: | L AR - Aircraft Research | ||||||||||||||||||||
| DLR - Research theme (Project): | L - Simulation & Validation (old) | ||||||||||||||||||||
| Location: | Göttingen | ||||||||||||||||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > Experimental Methods | ||||||||||||||||||||
| Deposited By: | Micknaus, Ilka | ||||||||||||||||||||
| Deposited On: | 06 Sep 2013 09:47 | ||||||||||||||||||||
| Last Modified: | 23 Jun 2023 11:24 |
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