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Multidisciplinary design and aerodynamic assessment of an agile and highly swept aircraft configuration

Liersch, Carsten M. and Huber, Kerstin Claudie and Schütte, Andreas and Zimper, Dirk and Siggel, Martin (2016) Multidisciplinary design and aerodynamic assessment of an agile and highly swept aircraft configuration. CEAS Aeronautical Journal, 7 (4), pp. 677-694. Springer. DOI: 10.1007/s13272-016-0213-4 ISSN 1869-5582

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Abstract

The characteristics of highly swept aircraft configurations have been studied in a series of consecutive research projects in DLR for more than 15 years. Currently, the investigations focus on the generic SACCON UCAV configuration, which was specified in a common effort together with the NATO STO/AVT-161 task group. This paper is the first one in a series of articles presenting the SACCON-related research work within DLR. First, the article describes the conceptual design studies being performed for this aircraft configuration. At this point the question is raised, whether the simple aerodynamic methods used within conceptual design can be applied to such type of aircraft configurations with sufficient accuracy. Thus, the second part of this article provides a comparison of the aerodynamic characteristics of the SACCON configuration predicted by low- and high-fidelity aerodynamic methods, as well as some results from wind tunnel experiments

Item URL in elib:https://elib.dlr.de/107268/
Document Type:Article
Title:Multidisciplinary design and aerodynamic assessment of an agile and highly swept aircraft configuration
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Liersch, Carsten M.carsten.liersch (at) dlr.deUNSPECIFIED
Huber, Kerstin ClaudieKerstin.Huber (at) dlr.deUNSPECIFIED
Schütte, Andreasandreas.schuette (at) dlr.deUNSPECIFIED
Zimper, Dirkdirk.zimper (at) dlr.deUNSPECIFIED
Siggel, Martinmartin.siggel (at) dlr.deUNSPECIFIED
Date:October 2016
Journal or Publication Title:CEAS Aeronautical Journal
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
Volume:7
DOI :10.1007/s13272-016-0213-4
Page Range:pp. 677-694
Publisher:Springer
ISSN:1869-5582
Status:Published
Keywords:Conceptual aircraft design, Multi-fidelity, Highly swept aircraft configurations, SACCON, UCAV aerodynamics
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 , Göttingen , Köln-Porz
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Transport Aircraft
Program Coordination Defence & Security Research
German-Dutch Windtunnels
Deposited By: Schütte, Andreas
Deposited On:02 Nov 2016 14:19
Last Modified:06 Sep 2019 15:24

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