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High speed static experimental investigations to estimate control device effectiveness and S&C capabilities

Rein, Martin and Irving, Jonathan and Rigby, Glyn and Birch, Trevor J. (2014) High speed static experimental investigations to estimate control device effectiveness and S&C capabilities. American Institute of Aeronautics and Astronautics. AIAA Aviation and Aeronautics Forum and Exposition (AVIATION 2014), 16. – 20. June 2014, Atlanta, GA, USA.

Full text not available from this repository.

Official URL: http://arc.aiaa.org | DOI: 10.2514/6.2014-2004

Abstract

The high speed experimental investigations of a generic UCAV configuration with control surfaces are presented. The current paper covers the design of the model, layout of the control surfaces and the static wind tunnel tests. The tests were performed in both the DNW and BAE Systems High Speed Tunnel facilities and included conditions up to a Mach number of M = 0.9. The experimental results are used to establish a common high speed CFD test matrix for the NATO Task Group STO/AVT-201 for computer code validation and to assess the capability to predict the complex vortical flow and aerodynamic S&C characteristics of moderately leading edge swept configurations.

Item URL in elib:https://elib.dlr.de/89341/
Document Type:Conference or Workshop Item (Speech)
Additional Information:AIAA 2014-2004, 32nd AIAA Applied Aerodynamics Conference, DOI: 10.2514/6.2014-2004
Title:High speed static experimental investigations to estimate control device effectiveness and S&C capabilities
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Rein, Martinmartin.rein (at) dlr.deUNSPECIFIED
Irving, JonathanBAE-Systems, Military Air Solutions, Flight Dynamics R&T, UKUNSPECIFIED
Rigby, GlynBAE-Systems, Military Air Solutions, Flight Dynamics R&T, UKUNSPECIFIED
Birch, Trevor J.DSTL, Portsmouth, UKUNSPECIFIED
Date:2014
Refereed publication:Yes
Open Access:No
In DOAJ:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-16
Publisher:American Institute of Aeronautics and Astronautics
Series Name:Conference Proceedings online
Status:Published
Keywords:high speed CFD, experimental investigations, UCAV configuration, High Speed Tunnel, control device effectiveness
Event Title:AIAA Aviation and Aeronautics Forum and Exposition (AVIATION 2014)
Event Location:Atlanta, GA, USA
Event Type:international Conference
Event Dates:16. – 20. June 2014
Organizer:American Institute of Aeronautics and Astronautics
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: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > High Speed Configurations
Deposited By: Micknaus, Ilka
Deposited On:18 Jul 2014 10:21
Last Modified:21 Oct 2014 13:55

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