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Tests of the effectiveness of elevons and split flaps for the DLR-F17E model in high-speed flows

Rein, Martin (2013) Tests of the effectiveness of elevons and split flaps for the DLR-F17E model in high-speed flows. DLR-Interner Bericht. DLR-IB 917-2013 A 85, 48 S.

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Item URL in elib:https://elib.dlr.de/84013/
Document Type:Monograph (DLR-Interner Bericht)
Title:Tests of the effectiveness of elevons and split flaps for the DLR-F17E model in high-speed flows
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Rein, Martinmartin.rein (at) dlr.deUNSPECIFIED
Date:2013
Refereed publication:No
Open Access:No
In DOAJ:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:48
Status:Published
Keywords:DLR-F17E, SACCON, vortical flow, transonic flow, lambda wing, control surfaces
Institution:DLR
Department:Hochgeschwindigkeitskonfigurationen
HGF - Research field:Aeronautics, Space and Transport
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 > High Speed Configurations
Deposited By: Danzer, Kristina
Deposited On:24 Sep 2013 15:30
Last Modified:29 Oct 2013 09:59

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