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Computational Analysis of a Three-dimensional Flapping Wing

Buchmann, Nadine and Radespiel, Rolf and Heinrich, Ralf (2014) Computational Analysis of a Three-dimensional Flapping Wing. In: New Results in Numerical and Experimental Fluid Mechanics IX Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 124. Springer Verlag. pp. 651-659. ISBN 978-3-319-03157-6. ISSN 1612-2909

Full text not available from this repository.

Abstract

Unsteady Reynolds-averaged Navier-Stokes simulations are presented in which two-dimensional airfoil motion parameters have been extended to three-dimensional wing motion. The motion parameters have been redefined including induced angles of attack which have been identified using a panel method based on Prandtl's wing theory. The numerical simulation approach includes a mesh deformation tool to perform the wing's movement. The resulting thrust and propulsive efficiency on wing sections are compared to equivalent two-dimensional simulations.

Item URL in elib:https://elib.dlr.de/91152/
Document Type:Contribution to a Collection
Title:Computational Analysis of a Three-dimensional Flapping Wing
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Buchmann, NadineTU BraunschweigUNSPECIFIED
Radespiel, RolfTU BraunschweigUNSPECIFIED
Heinrich, Ralfralf.heinrich (at) dlr.deUNSPECIFIED
Date:2014
Journal or Publication Title:New Results in Numerical and Experimental Fluid Mechanics IX
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:124
Page Range:pp. 651-659
Editors:
EditorsEmail
Dillmann, AndreasDLR Göttingen
Heller, GerdAirbus Deutschland
Krämer, EwaldUniversität Stuttgart
Kreplin, Hans-PeterDLR Göttingen
Nitsche, WolfgangTU Berlin
Rist, UlrichUniverstität Stuttgart
Publisher:Springer Verlag
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ISSN:1612-2909
ISBN:978-3-319-03157-6
Status:Published
Keywords:Flapping wing, Unsteady simulation, RANS
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation and Validation
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > C²A²S²E - Center for Computer Applications in AeroSpace Science and Engineering
Deposited By: Seyfried, Beate
Deposited On:20 Oct 2014 11:54
Last Modified:27 Feb 2015 10:29

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