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Aerodynamic Optimization of Supersonic Configurations.

Orlowski, M. and Herrmann, U. (1996) Aerodynamic Optimization of Supersonic Configurations. In: Proc. 20th Congress of the ICAS, 8-13 September 1996. 20th Congress of the International Council of the Aeronautical Sciences, 8.-13. September 1996, Sorrento, Italy.

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Abstract

In the present paper first steps towards aerodynamic optimization of supersonic civil trasport configurations are described. The DLR optimization tool MODeM is introduced. Optimization capabilities are demonstrated using an unconventional waverider- like generic SCT configuration. Furthermore sensitivities of the lift to drag ratio with respect to five fuselage design variables of conventional wing/body configurations are studied.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1996, pages=7,
Title:Aerodynamic Optimization of Supersonic Configurations.
Authors:
AuthorsInstitution or Email of Authors
Orlowski, M.UNSPECIFIED
Herrmann, U.UNSPECIFIED
Date:1996
Journal or Publication Title:Proc. 20th Congress of the ICAS, 8-13 September 1996
Status:Published
Keywords:Aerodynamic optimization, supersonic commercial transport, wing/body configurations, sensitivities
Event Title:20th Congress of the International Council of the Aeronautical Sciences, 8.-13. September 1996, Sorrento, Italy
HGF - Research field:UNSPECIFIED
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):W - Zukünftige Raumtransporter - Entwurf und Simulationsmethoden für Raumtransporter (old)
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 10:06

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