DLR-F4 Wing-Body Configuration.

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

Full text not available from this repository.

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:

Authors	Institution or Email of Authors
Redeker, G.

Date:

1994

Journal or Publication Title:

AGARD-AR-303

Volume:

II.

Page Range:

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:

L - no assignement

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

Repository Staff Only: item control page