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DLR-F4 Wing-Body Configuration.

Redeker, G. (1994) DLR-F4 Wing-Body Configuration. In: AGARD-AR-303, II., II.-. AGARD, 7 rue Ancelle, 92200 Neuilly-sur-Seine France.

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Abstract

These tests have been carried out under the auspices of GARTEUR in order to provide an experimental data base for a modern commercial transport type aircraft against which results of various computational methods may be checked. The tests were carried out in three major European wind tunnels (NLR-HST, ONERA-S2MA, DRA-8ftx8ft DRA Bedford) in order to compare the results of the same model in different wind tunnels. For the purpose of these tests the available geometry of the DLR-F4 model of a wing body configuration, which was developed as a research configuration of a modern transport type aircraft, was selected by the GARTEUR Action Group AD (AG01) "Wing body aerodynamics at transonic speeds.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1994, pages=AGARD-AR-303,
Title:DLR-F4 Wing-Body Configuration.
Authors:
AuthorsInstitution or Email of Authors
Redeker, G.UNSPECIFIED
Date:1994
Journal or Publication Title:AGARD-AR-303
Volume:II.
Page Range:II.-
Publisher:AGARD, 7 rue Ancelle, 92200 Neuilly-sur-Seine France
Series Name:AGARD-AR-303
Status:Published
Keywords:Wind tunnel tests, transport aircraft, transonic wing
HGF - Research field:UNSPECIFIED
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
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: elib DLR-Beauftragter
Deposited On:03 Apr 2006
Last Modified:27 Apr 2009 10:05

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