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Investigation of Vortex Breakdown over a Pitching Delta Wing applying the DLR TAU-Code with Full, Automatic Grid Adaptation

Alrutz, Thomas and Ruetten, Markus (2005) Investigation of Vortex Breakdown over a Pitching Delta Wing applying the DLR TAU-Code with Full, Automatic Grid Adaptation. AIAA. 35th AIAA Fluid Dynamics, 6-9 June 2005, Toronto, Canada.

Full text not available from this repository.

Abstract

This paper covers a description of the complete process chain used to investigate the vortex breakdown over a pitching delta wing. Special attention is given to the dynamic adaptation strategies used to capture the main flow structures as well as the analysis of vortex breakdown and the formation of primary and secondary vortices. The demonstrated approach with hybrid grids and a standard URANS flow solver shows extraordinary good results for this type of application.

Item URL in elib:https://elib.dlr.de/21725/
Document Type:Conference or Workshop Item (Paper)
Title:Investigation of Vortex Breakdown over a Pitching Delta Wing applying the DLR TAU-Code with Full, Automatic Grid Adaptation
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Alrutz, ThomasUNSPECIFIEDUNSPECIFIED
Ruetten, MarkusUNSPECIFIEDUNSPECIFIED
Date:9 June 2005
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Publisher:AIAA
Status:Accepted
Keywords:grid adaptation, vortex breakdown, TAU-Code, delta wing
Event Title:35th AIAA Fluid Dynamics
Event Location:Toronto, Canada
Event Type:international Conference
Event Dates:6-9 June 2005
Organizer:AIAA
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > CASE
Deposited By: Alrutz, Thomas
Deposited On:24 Jan 2006
Last Modified:27 Apr 2009 04:56

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