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A Design Method for Supersonic Transport Wings
Li, P.(1) and Sobieczky, H. and Seebass, R.(1) (1995) A Design Method for Supersonic Transport Wings. In: 13th AIAA Applied Aerodynamics Conference, San Diego, CA. 19.-22. June 1995.
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Abstract
Es wird die Methode des fiktiven Gases auf Euler-Gleichungen angewandt und zur Auslegung eines supersonischen schraegfliegenden Tragfluegels verwendet.
| Document Type: | Conference or Workshop Item (Paper) | ||||||||
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| Additional Information: | institution=AIAA, LIDO-Berichtsjahr=1995, pages=10, | ||||||||
| Title: | A Design Method for Supersonic Transport Wings | ||||||||
| Authors: |
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| Date: | 1995 | ||||||||
| Journal or Publication Title: | 13th AIAA Applied Aerodynamics Conference, San Diego, CA. 19.-22. June 1995 | ||||||||
| Series Name: | AIAA 95 - 1819 | ||||||||
| Status: | Published | ||||||||
| Keywords: | Ueberschalltransport, Oblique Flying Wing (OFW), Entwurfsmethode | ||||||||
| 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): | UNSPECIFIED | ||||||||
| Location: | Köln-Porz , Braunschweig , Göttingen | ||||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > Institut für Strömungsmechanik > Institut für Experimentelle Strömungsmechanik | ||||||||
| Deposited By: | elib DLR-Beauftragter | ||||||||
| Deposited On: | 03 Apr 2006 | ||||||||
| Last Modified: | 27 Apr 2009 10:08 |
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