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Static and Forced-Oscillation Tests of a Generic Unmanned Combat Air Vehicle

Vicroy, Dan D. and Loeser, Thomas D. and Schütte, Andreas (2012) Static and Forced-Oscillation Tests of a Generic Unmanned Combat Air Vehicle. Journal of Aircraft, 49 (6), pp. 1558-1583. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.C031501 ISSN 0021-8669

Full text not available from this repository.

Abstract

A series of three wind-tunnel static and forced-oscillation tests were conducted on a model of a generic unmanned combat air vehicle. These tests are part of an international research effort to assess the state of the art of computational fluid dynamics methods to predict the static and dynamic stability and control characteristics. The experimental data set includes not only force and moment time histories, but also surface pressure and offbody particle image velocimetry measurements. The extent of the data precludes a full examination within the scope of this paper. This paper provides a general description and selected examples of the available static and dynamic data, as well as some of the observed trends.

Item URL in elib:https://elib.dlr.de/80507/
Document Type:Article
Title:Static and Forced-Oscillation Tests of a Generic Unmanned Combat Air Vehicle
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Vicroy, Dan D.dan.d.vicroy (at) nasa.govUNSPECIFIED
Loeser, Thomas D.thomas.loeser (at) dlr.deUNSPECIFIED
Schütte, Andreasandreas.schuette (at) dlr.deUNSPECIFIED
Date:November 2012
Journal or Publication Title:Journal of Aircraft
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:49
DOI :10.2514/1.C031501
Page Range:pp. 1558-1583
Publisher:American Institute of Aeronautics and Astronautics (AIAA)
ISSN:0021-8669
Status:Published
Keywords:Delta Wing; UCAV; Stability and Control; Wind Tunnel Experiment; Dynamic Testinmg; PIV; DNW-NWB; MPM; SACCON; RTO; AVT
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 - Military Technologies (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Schütte, Andreas
Deposited On:11 Jan 2013 10:25
Last Modified:08 Mar 2018 18:41

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