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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 | ||||||||||||||
| 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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