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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.

Full text not available from this repository.

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)
Additional Information: institution=AIAA, LIDO-Berichtsjahr=1995, pages=10,
Title:A Design Method for Supersonic Transport Wings
Authors:
AuthorsInstitution or Email of Authors
Li, P.(1)UNSPECIFIED
Sobieczky, H.UNSPECIFIED
Seebass, R.(1)UNSPECIFIED
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:other
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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