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UCAV model design and static experimental investigations to estimate control device effectiveness and Stability and Control capabilities

Huber, Kerstin Claudie and Vicroy, Dan D. and Schütte, Andreas and Hübner, Andreas-René (2014) UCAV model design and static experimental investigations to estimate control device effectiveness and Stability and Control capabilities. In: 32nd AIAA Applied Aerodynamics Conference (2002), pp. 1-21. 32nd AIAA Applied Aerodynamics Conference, Atlanta, GA, USA, 16.-20. Juni 2014, Atlanta, GA, USA.

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Abstract

The experimental investigations of two generic UCAV configurations with control surfaces are presented. The current paper is covering the design of the model, layout of the control surfaces as well as the static wind tunnel tests. The low speed static wind tunnel tests have been undertaken to evaluate the effectiveness of different control surfaces and control surface settings. Finally, the experimental results are used to establish a common CFD test matrix for the NATO STO Task Group AVT-201 for computer code validation and to assess the capability to predict the complex vortical flow and aerodynamic Stability and Control (S&C) characteristics of configurations with highly swept leading edges and vortex dominated flow field

Item URL in elib:https://elib.dlr.de/90261/
Document Type:Conference or Workshop Item (Speech)
Additional Information:DOI: 10.2514/6.2014-2002
Title:UCAV model design and static experimental investigations to estimate control device effectiveness and Stability and Control capabilities
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Huber, Kerstin Claudiekerstin.huber (at) dlr.deUNSPECIFIED
Vicroy, Dan D.dan.d.vicroy (at) nasa.govUNSPECIFIED
Schütte, Andreasandreas.schuette (at) dlr.deUNSPECIFIED
Hübner, Andreas-RenéAndreas.Huebner (at) dlr.deUNSPECIFIED
Date:June 2014
Journal or Publication Title:32nd AIAA Applied Aerodynamics Conference
Refereed publication:Yes
Open Access:No
In DOAJ:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-21
Status:Published
Keywords:UCAV, vortical flow, control devices, delta wing, Experiment, Stability and Control, static, 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
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
German-Dutch Windtunnels
Deposited By: Schütte, Andreas
Deposited On:03 Sep 2014 15:13
Last Modified:17 Oct 2014 14:00

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