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

Alrutz, T. and Rütten, M. (2005) Investigation of Vortex Breakdown over a Generic Pitching Delta Wing applying the DLR TAU-Code with Full Automatic Grid Adaptation. 36th AIAA Fluid Dynamics Conference and Exhibit, 2005-06-06 - 2005-09-06, Toronto, Canada.

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Item URL in elib:https://elib.dlr.de/54027/
Document Type:Conference or Workshop Item (Paper)
Title:Investigation of Vortex Breakdown over a Generic Pitching Delta Wing applying the DLR TAU-Code with Full Automatic Grid Adaptation
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Alrutz, T.UNSPECIFIEDUNSPECIFIED
Rütten, M.UNSPECIFIEDUNSPECIFIED
Date:June 2005
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Vortex Breakdown, Pitching Delta Wing, TAU-Code
Event Title:36th AIAA Fluid Dynamics Conference and Exhibit
Event Location:Toronto, Canada
Event Type:international Conference
Event Dates:2005-06-06 - 2005-09-06
Organizer:American Institute of Aeronautics and Astronautics
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 > Helicopters
Deposited By: Rütten, Dr.-Ing. Markus
Deposited On:15 May 2008
Last Modified:27 Apr 2009 14:55

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