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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. Seminar in Davis, USA, 2016-11-28, Davis, CA, USA.

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Item URL in elib:https://elib.dlr.de/110740/
Document Type:Conference or Workshop Item (Speech)
Title:Generic lambda wing configuration with classical and novel control surfaces and highly integrated intakes
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Rein, MartinUNSPECIFIEDhttps://orcid.org/0000-0002-2670-2815UNSPECIFIED
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, intake
Event Title:Seminar in Davis, USA
Event Location:Davis, CA, USA
Event Type:Other
Event Date:28 November 2016
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 (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > High Speed Configurations
Deposited By: Bachmann, Barbara
Deposited On:17 Jan 2017 11:37
Last Modified:24 Apr 2024 20:15

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