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Wind-tunnel tests of leading edge modifications for controlling delta wings

Rein, Martin (2016) Wind-tunnel tests of leading edge modifications for controlling delta wings. [Other]

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Item URL in elib:https://elib.dlr.de/110555/
Document Type:Other
Additional Information:Seminarvortrag in Pasadena, Ca, USA
Title:Wind-tunnel tests of leading edge modifications for controlling delta wings
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Rein, Martinmartin.rein (at) dlr.deUNSPECIFIED
Date:2016
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:vortex, flow separation, flow control, delta wing
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 16:28
Last Modified:12 Jan 2017 16:28

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