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Fluid-Structure Coupled Loads Analysis of DLR’s F6 Wing-Body Configuration

Keye, Stefan and Sitzmann, Martin and Brodersen, Olaf and Heinrich, Ralf (2008) Fluid-Structure Coupled Loads Analysis of DLR’s F6 Wing-Body Configuration. In: 46th AIAA Aerospace Sciences Meeting, 2008. 46th AIAA Aerospace Sciences Meeting, 2008, 7.1.2008-10.1.2008, Reno, NV (USA).

Full text not available from this repository.

Official URL: http://www.aiaa.org

Abstract

The activities associated with the preparation of the DLR-F6 wind tunnel model for testing in NASA Langley’s National Transonic Facility (NTF) in September 2007 are described. The purpose of this test was to provide validation-quality experimental data for comparison to existing results from the third AIAA Computational Fluid Dynamics (CFD) Drag Prediction Workshop (DPW-3) held in 2006. As the aerodynamic forces associated with the required flow conditions exceed the model’s design load limits various model modifications were implemented and comprehensive fluid-structure coupled analyses were performed for the desired flow conditions in order to meet NTF safety requirements.

Item URL in elib:https://elib.dlr.de/54089/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Fluid-Structure Coupled Loads Analysis of DLR’s F6 Wing-Body Configuration
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Keye, StefanUNSPECIFIEDUNSPECIFIED
Sitzmann, MartinUNSPECIFIEDUNSPECIFIED
Brodersen, OlafUNSPECIFIEDUNSPECIFIED
Heinrich, RalfUNSPECIFIEDUNSPECIFIED
Date:January 2008
Journal or Publication Title:46th AIAA Aerospace Sciences Meeting, 2008
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
Status:Published
Keywords:DLR-F6, NTF, Drag Prediction Workshop, fluid-structure coupling
Event Title:46th AIAA Aerospace Sciences Meeting, 2008
Event Location:Reno, NV (USA)
Event Type:international Conference
Event Dates:7.1.2008-10.1.2008
Organizer:AIAA
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: Keye, Dr.(PH.D.) Stefan
Deposited On:15 May 2008
Last Modified:09 Feb 2017 19:17

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