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Experimental and numerical investigations of pitch-plunging wing aerodynamics at low Reynolds number

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: 10.1054/IJESMS.2013.052370 ISSN 1755-9758

Full text not available from this repository.

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/
Document Type:Article
Additional Information:ISSN online: 1755-9766
Title:Experimental and numerical investigations of pitch-plunging wing aerodynamics at low Reynolds number
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Wokoeck, RalfTechnische Universität Braunschweig, Institut für StrömungsmechanikUNSPECIFIED
Radespiel, RolfTechnische Universität Braunschweig, Institut für StrömungsmechanikUNSPECIFIED
Ehlers, Haukehauke.ehlers (at) dlr.deUNSPECIFIED
Konrath, Robertrobert.konrath (at) dlr.deUNSPECIFIED
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 :10.1054/IJESMS.2013.052370
Page Range:pp. 19-32
Editors:
EditorsEmail
Yang, Xiaogang UNSPECIFIED
Zouaoui , ZoubirUNSPECIFIED
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:14 Dec 2019 04:20

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