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Structural modelling, dimensioning and assessment of agile military aircraft

Voß, Arne and Klimmek, Thomas and Windel, Niklas (2018) Structural modelling, dimensioning and assessment of agile military aircraft. Annual Military Scientific Research, pp. 32-33. Federal Ministry of Defence.

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With great probability, the next generation military aircraft will be autonomous, highly agile unmanned combat air vehicles (UCAV) operating in a unit as a combat air system. The DLR is examining such a UCAV configuration in the form of an unmanned, highly swept flying wing configuration. Key aspects include control concepts, aerodynamics, aeroelasticity, as well as exploration of a structural layout using numerical methods.

Item URL in elib:https://elib.dlr.de/119316/
Document Type:Article
Title:Structural modelling, dimensioning and assessment of agile military aircraft
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Voß, ArneArne.Voss (at) dlr.dehttps://orcid.org/0000-0003-2266-7853
Klimmek, Thomasthomas.klimmek (at) dlr.deUNSPECIFIED
Journal or Publication Title:Annual Military Scientific Research
Refereed publication:No
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Page Range:pp. 32-33
Publisher:Federal Ministry of Defence
Keywords:aeroelasticity, loads, UCAV, structural optimization
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 - Flight Physics (old)
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design
Deposited By: Voß, Arne
Deposited On:22 May 2018 10:31
Last Modified:22 May 2018 10:31

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