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Trailing Edge Optimization Investigations on A320-Wing Sections.
Köster, H. (1994) Trailing Edge Optimization Investigations on A320-Wing Sections. DLR-Interner Bericht. 129-9428, 26 S.
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Abstract
After preliminary theoretical and experimental studies on several Airbus airfoils with and without optimized trailing edge it was decided to investigate a clean A320 wing with a modified trailing edge. As a first step optimized trailing edges for three airfoils of different span stations of the A320-wing have been developed. This report contains the results of 2D analysis calculations at DLR for these airfoils which show a reduction of the drag for the prescribed lift coefficients for the optimized airfoils can be obtained.
| Document Type: | Monograph (DLR-Interner Bericht) | ||||
|---|---|---|---|---|---|
| Additional Information: | LIDO-Berichtsjahr=1995, | ||||
| Title: | Trailing Edge Optimization Investigations on A320-Wing Sections. | ||||
| Authors: |
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| Date: | 1994 | ||||
| Number of Pages: | 26 | ||||
| Status: | Published | ||||
| Keywords: | Supercritical airfoil, Trailing edge optimization, Divergent trailing edge | ||||
| HGF - Research field: | UNSPECIFIED | ||||
| HGF - Program: | Aeronautics | ||||
| HGF - Program Themes: | L - no assignement | ||||
| DLR - Research area: | UNSPECIFIED | ||||
| DLR - Program: | L ST - Starrflüglertechnologien | ||||
| DLR - Research theme (Project): | L - Concepts & Integration | ||||
| Location: | Köln-Porz , Braunschweig , Göttingen | ||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik | ||||
| Deposited By: | elib DLR-Beauftragter | ||||
| Deposited On: | 03 Apr 2006 | ||||
| Last Modified: | 27 Apr 2009 10:05 |
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