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Investigation on a Three-Surface Airplane Configuration

Wichmann, G. and Strohmeyer, D. and Streit, T. (1999) Investigation on a Three-Surface Airplane Configuration. In: Proceedings ODAS 1999. ONERA/DLR Symposium, Paris (fr), 21.06.-24.06.1999.

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Abstract

In this paper the activities of the Institute of Design Aerodynamics within the DLR project "Dreiflächen-Flugzeug (3FF)" - Three-Surface Aircraft, TSA - concerning the investigation of three-surface aircraft configurations are presented. First aircraft predesign results indicate a better performance for TSA configurations compared with conventional designs. Transonic canard designs demonstrate the aerodynamic feasibility of the canard concept in the complex three-dimensional forbody flow at the high Mach numbers of cruise, whereby forward swept canards show major advantages.

Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=1999,
Title:Investigation on a Three-Surface Airplane Configuration
Authors:
AuthorsInstitution or Email of Authors
Wichmann, G.UNSPECIFIED
Strohmeyer, D.UNSPECIFIED
Streit, T.UNSPECIFIED
Date:1999
Journal or Publication Title:Proceedings ODAS 1999
Status:Published
Keywords:three-surface aircraft, transonic canard design, predesign, canard optimization, fuselage-canard configuration, forward swept canard
Event Title:ONERA/DLR Symposium, Paris (fr), 21.06.-24.06.1999
Organizer:ONERA
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
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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