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Validation of the suction optimization on the A310 wing
Stock, H.W. (1999) Validation of the suction optimization on the A310 wing. DLR-Interner Bericht. 129-99/6.
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Abstract
The results concerning the suction optimization for the A310 wing, obtained by ONERA, are validated using the boundary layer code and the stability code. The suction is applied at the leading edge region between x/c = 0 and x/c = 0.19. Four flow cases on the upper surface of the wing are considered.
| Document Type: | Monograph (DLR-Interner Bericht) | ||||
|---|---|---|---|---|---|
| Additional Information: | LIDO-Berichtsjahr=1999, | ||||
| Title: | Validation of the suction optimization on the A310 wing | ||||
| Authors: |
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| Date: | 1999 | ||||
| Status: | Published | ||||
| Keywords: | Laminar Wing Flow, Suction Optimization | ||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||
| HGF - Program: | Aeronautics | ||||
| HGF - Program Themes: | L - no assignement | ||||
| DLR - Research area: | Aeronautics | ||||
| 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: | Claudia Grant | ||||
| Deposited On: | 16 Sep 2005 | ||||
| Last Modified: | 14 Jan 2010 20:01 |
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