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Conceptual Design and Aerodynamic Analyses of a Generic UCAV Configuration

Liersch, Carsten M. and Huber, Kerstin Claudie (2014) Conceptual Design and Aerodynamic Analyses of a Generic UCAV Configuration. In: 32nd AIAA Applied Aerodynamics Conference (2001). 32nd AIAA Applied Aerodynamics Conference, Atlanta, GA, USA, 16.-20. Juni 2014, Atlanta, GA, USA.

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Abstract

Applying DLR's conceptual aircraft design system to military ying wing configurations, the design of a generic UCAV configuration is presented. For its outer shape, the SACCON geometry specified by NATO STO/AVT-161 Task Group was taken. For mission analysis and structural sizing, aerodynamic data from fast and robust conceptual design methods (i.e. potential ow theory) were used. In order to assess the validity of these simple methods for such configurations, a comparison with results from RANS aerodynamics and wind tunnel measurements was performed. The results of this design task were included into the stability and control investigations performed within the AVT-201 task group

Item URL in elib:https://elib.dlr.de/90264/
Document Type:Conference or Workshop Item (Speech)
Title:Conceptual Design and Aerodynamic Analyses of a Generic UCAV Configuration
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Liersch, Carsten M.carsten.liersch (at) dlr.deUNSPECIFIED
Huber, Kerstin Claudiekerstin.huber (at) dlr.deUNSPECIFIED
Date:June 2014
Journal or Publication Title:32nd AIAA Applied Aerodynamics Conference
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:UCAV, Design, Aerodynamic design, multi disciplinary, vortical flow, CFD, engineering methods, Stability and Control, control, devices
Event Title:32nd AIAA Applied Aerodynamics Conference, Atlanta, GA, USA
Event Location:Atlanta, GA, USA
Event Type:international Conference
Event Dates:16.-20. Juni 2014
Organizer:AIAA
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: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Schütte, Andreas
Deposited On:03 Sep 2014 14:26
Last Modified:31 Jul 2019 19:47

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