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Wake Vortex Alleviation by Differential and Oscillating Flap Setting: A flight test

Voss, Guido and Gerz, Thomas and Baumann, Robert and Stumpf, Eike and Press, Michael (2009) Wake Vortex Alleviation by Differential and Oscillating Flap Setting: A flight test. 27th Applied Aerodynamics Conference, 22-25 Jun 2009, San Antonio, Texas.

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Item URL in elib:https://elib.dlr.de/61531/
Document Type:Conference or Workshop Item (Paper)
Title:Wake Vortex Alleviation by Differential and Oscillating Flap Setting: A flight test
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Voss, GuidoDLRUNSPECIFIED
Gerz, ThomasDLRUNSPECIFIED
Baumann, RobertDLRUNSPECIFIED
Stumpf, EikeDLRUNSPECIFIED
Press, MichaelDLRUNSPECIFIED
Date:June 2009
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Keywords:Wake Vortex Differential Flap Setting Oscillating Flap Setting ATTAS LIDAR
Event Title:27th Applied Aerodynamics Conference
Event Location:San Antonio, Texas
Event Type:international Conference
Event Dates:22-25 Jun 2009
Organizer:AIAA
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:L VU - Air Traffic and Environment (old)
DLR - Research area:Aeronautics
DLR - Program:L VU - Air Traffic and Environment
DLR - Research theme (Project):L - Wake Vortices (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Voß, Guido
Deposited On:15 Dec 2009 13:31
Last Modified:31 Jul 2019 19:26

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