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Ground-Based Simulation of Complex Maneuvers of a Delta-Wing Aircraft

Rein, Martin and Höhler, Gebhard and Schütte, Andreas and Bergmann, Andreas and Löser, Thomas (2008) Ground-Based Simulation of Complex Maneuvers of a Delta-Wing Aircraft. Journal of Aircraft, 45 (1), pp. 286-291. DOI: 10.2514/1.30033

Full text not available from this repository.

Abstract

Ground-based simulations of complex maneuvers of a model of the X-31 aircraft have been performed in the lowspeed wind tunnel of the German–Dutch Wind Tunnels. In the wind-tunnel tests a novel test rig with 6 degrees of freedom was used for the first time for moving the model. Furthermore, the model was equipped with eight remotely controlled control surfaces. In this manner, maneuvers in which both the model and its control surfaces were moved simultaneously have been performed. Both the specific technical equipment of the model and the novel 6 degree of freedom test rig will be reviewed. Thereafter, experimental results obtained will be discussed.

Item URL in elib:https://elib.dlr.de/53630/
Document Type:Article
Title:Ground-Based Simulation of Complex Maneuvers of a Delta-Wing Aircraft
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Rein, MartinUNSPECIFIEDUNSPECIFIED
Höhler, GebhardUNSPECIFIEDUNSPECIFIED
Schütte, AndreasUNSPECIFIEDUNSPECIFIED
Bergmann, AndreasDNW-NWBUNSPECIFIED
Löser, ThomasDNW-NWBUNSPECIFIED
Date:2008
Journal or Publication Title:Journal of Aircraft
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
Volume:45
DOI :10.2514/1.30033
Page Range:pp. 286-291
Status:Published
Keywords:ground-based testing, hexapod, X-31, maneuver
HGF - Research field:Aeronautics, Space and Transport (old)
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 , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Transport Aircraft
Institute of Aerodynamics and Flow Technology > High Speed Configurations
Deposited By: Rein, Prof.Dr. Martin
Deposited On:07 Apr 2008
Last Modified:27 Apr 2009 14:49

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