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Application of Advanced CFD Tools for High Reynolds Number Testing.

Melber-Wilkending, Stefan and Wichmann, Georg (2008) Application of Advanced CFD Tools for High Reynolds Number Testing. 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition, 2009-01-05 - 2009-01-08, Orlando, Florida.

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Abstract

Numerical simulations of the DLR F11 high lift half model in landing configuration in the test section of the ETW wind tunnel have been carried out with the unstructured CFD code DLR TAU. The numerical results are compared to measurements of the cryogenic wind tunnel ETW performed within the EU project FLIRET. The tests have been conducted with three different peniche heights of the F11 model to determine the influence of the so called half model mounting effects on the aerodynamic characteristics of model flow. Based on the numerical simulation of the half model tests the peniche effects and the wind tunnel flow itself are analyzed. The capability of the used CFD code for high Reynolds number testing is demonstrated.

Item URL in elib:https://elib.dlr.de/57153/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Application of Advanced CFD Tools for High Reynolds Number Testing.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Melber-Wilkending, StefanUNSPECIFIEDUNSPECIFIED
Wichmann, GeorgUNSPECIFIEDUNSPECIFIED
Date:December 2008
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Accepted
Keywords:FLIRET, ETW, HighLift, Peniche, Half-model, Numerical Wind Tunnel
Event Title:47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition
Event Location:Orlando, Florida
Event Type:international Conference
Event Dates:2009-01-05 - 2009-01-08
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: Melber-Wilkending, Stefan
Deposited On:07 Jan 2009
Last Modified:31 Jul 2019 19:23

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