DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Low-speed Dynamic Wind Tunnel Test Analysis of a Generic 53° Swept UCAV Configuration with Controls

Vicroy, Dan D. and Huber, Kerstin Claudie and Rohlf, Detlef and Löser, Thomas (2014) Low-speed Dynamic Wind Tunnel Test Analysis of a Generic 53° Swept UCAV Configuration with Controls. In: 32nd AIAA Applied Aerodynamics Conference (2003), pp. 1-24. 32nd AIAA Applied Aerodynamics Conference, Atlanta, GA, USA, 16.-20. Juni 2014, Atlanta, GA, USA.

Full text not available from this repository.

Official URL: http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2003


Several static and dynamic forced-motion wind tunnel tests have been conducted on a generic unmanned combat air vehicle (UCAV) configuration with a 53° swept leading edge. These tests are part of an international research effort to assess and advance the state-of-art of computational fluid dynamics (CFD) methods to predict the static and dynamic stability and control characteristics for this type of configuration. This paper describes the dynamic forced motion data collected from two different models of this UCAV configuration as well as analysis of the control surface deflections on the dynamic forces and moments

Item URL in elib:https://elib.dlr.de/90262/
Document Type:Conference or Workshop Item (Speech)
Additional Information:DOI: 10.2514/6.2014-2003
Title:Low-speed Dynamic Wind Tunnel Test Analysis of a Generic 53° Swept UCAV Configuration with Controls
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Vicroy, Dan D.dan.d.vicroy (at) nasa.govUNSPECIFIED
Huber, Kerstin Claudiekerstin.huber (at) dlr.deUNSPECIFIED
Rohlf, DetlefDetlef.Rohlf (at) dlr.deUNSPECIFIED
Date:June 2014
Journal or Publication Title:32nd AIAA Applied Aerodynamics Conference
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Page Range:pp. 1-24
Keywords:UCAV, vortical flow, control devices, delta wing, Experiment, Stability and Control, dynamic
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
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 15:03
Last Modified:17 Oct 2014 14:15

Repository Staff Only: item control page

Help & Contact
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.