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Aero-Elastic Simulation of DLR’s F6 Transport Aircraft Configuration and Comparison to Experimental Data

Keye, Stefan and Rudnik, Ralf (2009) Aero-Elastic Simulation of DLR’s F6 Transport Aircraft Configuration and Comparison to Experimental Data. In: 48th AIAA Aerospace Sciences Meeting. 48th AIAA Aerospace Sciences Meeting, 2009-01-05 - 2009-01-08, Orlando, FL (USA).

Full text not available from this repository.

Abstract

The accuracy of a numerical aero-elastic simulation approach is assessed by comparing results from a fluid-structure-coupled analysis to experimental data. The German Aerospace Research Center’s (DLR) F6 wind tunnel model, a transonic wing-body design with optional flow-through nacelles, was used as a base configuration for this study. Coupled analyses were performed using an in-house simulation procedure built around DLR’s Reynolds-averaged Navier-Stokes flow solver TAU and the commercial finite-element structural analysis code ANSYS® Mechanical. Experimental data were available from a recent test campaign performed at NASA’s National Transonic Facility (NTF). Numerical predictions are evaluated using both aerodynamic and structural data.

Item URL in elib:https://elib.dlr.de/58120/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Aero-Elastic Simulation of DLR’s F6 Transport Aircraft Configuration and Comparison to Experimental Data
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Keye, StefanUNSPECIFIEDUNSPECIFIED
Rudnik, RalfUNSPECIFIEDUNSPECIFIED
Date:January 2009
Journal or Publication Title:48th AIAA Aerospace Sciences Meeting
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
Status:Published
Keywords:fluid-structure-coupling, experimental data, TAU, ANSYS, National Transonic Facility
Event Title:48th AIAA Aerospace Sciences Meeting
Event Location:Orlando, FL (USA)
Event Type:international Conference
Event Dates:2009-01-05 - 2009-01-08
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:24 Feb 2009
Last Modified:09 Feb 2017 19:18

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