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Generic lambda wing configuration with classical and novel control surfaces and highly integrated intakes

Rein, Martin (2016) Generic lambda wing configuration with classical and novel control surfaces and highly integrated intakes. [Other]

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Item URL in elib:https://elib.dlr.de/110506/
Document Type:Other
Additional Information:Seminar in Davis, CA, USA; Eingeladener Vortrag
Title:Generic lambda wing configuration with classical and novel control surfaces and highly integrated intakes
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Rein, Martinmartin.rein (at) dlr.deUNSPECIFIED
Date:2016
Refereed publication:No
Open Access:No
In DOAJ:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:vortex, flow separation, flow control, delta wing, intake
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Military Technologies
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > High Speed Configurations
Deposited By: Bachmann, Barbara
Deposited On:12 Jan 2017 16:18
Last Modified:12 Jan 2017 16:18

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