Richter, K. (2002) Adaptive Elements on Transonic Airfoils. 15th Liepmann-Ludwieg-Seminar, California Institute of Technolgy, Pasadena, CA, USA, Juni 18, 2002.
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Abstract
Performance improvement due to multi point airfoil design including adaptive elements. Combined application of adaptive shock control bump and trailing edge flap for VC-Opt airfoil gains large drag reductions; definition of simple control laws. Large, complex TE-flap can be replaced with very small and less complex mini trailing edge device (MiniTED). MiniTEDs achieve considerable performance enhancements for VC-Opt airfoil. Divergent trailing edge is better MiniTED at transonic speeds, and suitable for application as adaptive element.
| Item URL in elib: | https://elib.dlr.de/13823/ | ||||||||
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| Document Type: | Conference or Workshop Item (Speech) | ||||||||
| Additional Information: | LIDO-Berichtsjahr=2002, | ||||||||
| Title: | Adaptive Elements on Transonic Airfoils | ||||||||
| Authors: |
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| Date: | 2002 | ||||||||
| Open Access: | No | ||||||||
| Gold Open Access: | No | ||||||||
| In SCOPUS: | No | ||||||||
| In ISI Web of Science: | No | ||||||||
| Status: | Published | ||||||||
| Keywords: | multi point airfoil design, adaptive wing, variable camber, airfoil | ||||||||
| Event Title: | 15th Liepmann-Ludwieg-Seminar, California Institute of Technolgy, Pasadena, CA, USA, Juni 18, 2002 | ||||||||
| HGF - Research field: | Aeronautics, Space and Transport (old) | ||||||||
| HGF - Program: | Aeronautics | ||||||||
| HGF - Program Themes: | other | ||||||||
| DLR - Research area: | Aeronautics | ||||||||
| DLR - Program: | L ST - Starrflüglertechnologien | ||||||||
| DLR - Research theme (Project): | UNSPECIFIED | ||||||||
| Location: | Köln-Porz , Braunschweig , Göttingen | ||||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > Institut für Strömungsmechanik | ||||||||
| Deposited By: | DLR-Beauftragter, elib | ||||||||
| Deposited On: | 16 Sep 2005 | ||||||||
| Last Modified: | 14 Jan 2010 21:01 |
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