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.
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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/ | ||||||||||||||||||||||||||||
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Document Type: | Contribution to a Collection | ||||||||||||||||||||||||||||
Title: | Computational Analysis of a Three-dimensional Flapping Wing | ||||||||||||||||||||||||||||
Authors: |
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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: |
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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 (old) | ||||||||||||||||||||||||||||
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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