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Validation of the TAU-code for fuselage-rotorhead applications with moving meshes

Wendisch, Jan-Hendrik (2011) Validation of the TAU-code for fuselage-rotorhead applications with moving meshes. DLR-Interner Bericht. 124-2011/914. Deutsches Zentrum für Luft- und Raumfahrt e.V.. 16 S.

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In the SHANEL-L project in 2009 a simulation of the Eurocopter EC145 fuselage with a model rotorhead was performed with the block-structured solver FLOWer and the unstructured solver TAU 2007 by Eurocopter Deutschland. The results were compared to experimental data from a wind tunnel campaign at the university of Munich. While the results of FLOWer were comparable to the experiment, TAU suffered from an issue in the motion module. Since the solver was considerable improved in the last years, the simulation was repeated in order to demonstrate its applicability for fuselage-rotorhead simulations with moving meshes. The obtained results with the TAU 2011.1.0 release are validated against the experimental data and the FLOWer results.

Item URL in elib:https://elib.dlr.de/72572/
Document Type:Monograph (DLR-Interner Bericht)
Title:Validation of the TAU-code for fuselage-rotorhead applications with moving meshes
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Wendisch, Jan-HendrikJan-Hendrik.Wendisch (at) dlr.deUNSPECIFIED
Date:September 2011
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Number of Pages:16
Keywords:TAU, EC145, fuselage, rotorhead, validation, SHANEL-L, CFD
Institution:Deutsches Zentrum für Luft- und Raumfahrt e.V.
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Rotorcraft (old)
DLR - Research area:Aeronautics
DLR - Program:L RR - Rotorcraft Research
DLR - Research theme (Project):L - The Virtual Aerodynamic Rotorcraft (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Helicopters
Deposited By: Wendisch, Jan-Hendrik
Deposited On:14 Dec 2011 09:49
Last Modified:12 Dec 2013 21:28

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