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Aerodynamics of the Wing/Fuselage Junction at an Transport Aircraft in High-lift Configuration.

Melber-Wilkending, Stefan (2008) Aerodynamics of the Wing/Fuselage Junction at an Transport Aircraft in High-lift Configuration. 16th AG STAB/DGLR Symposium, 2008-11-03 - 2008-11-04, Aachen.

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Abstract

This paper presents the numerical simulation (DLR TAU-code) and the analysis of viscous high-lift flow around a complex wing/body configuration (DLR ALVAST) in landing configuration. The investigations aim for a better understanding of the aerodynamics at the wing root and the lift breakdown for such a configuration.

Item URL in elib:https://elib.dlr.de/57152/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Aerodynamics of the Wing/Fuselage Junction at an Transport Aircraft in High-lift Configuration.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Melber-Wilkending, StefanUNSPECIFIEDUNSPECIFIED
Date:November 2008
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Accepted
Keywords:Highlift, maximum Lift, CFD, TAU-Code, ALVAST
Event Title:16th AG STAB/DGLR Symposium
Event Location:Aachen
Event Type:national Conference
Event Dates:2008-11-03 - 2008-11-04
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L - no assignment
DLR - Research theme (Project):L - no assignment (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Melber-Wilkending, Stefan
Deposited On:07 Jan 2009
Last Modified:31 Jul 2019 19:23

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