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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 Schütte, Andreas and Vicroy, Dan D. and Hübner, Andreas-René (2016) UCAV MODEL DESIGN AND STATIC EXPERIMENTAL INVESTIGATIONS TO ESTIMATE CONTROL DEVICE EFFECTIVENESS AND STABILITY AND CONTROL CAPABILITIES. NATO STO - Science and Technology Organisation. [Other]

Full text not available from this repository.

Official URL: https://www.sto.nato.int/publications/STO%20Technical%20Reports/STO-TR-AVT-201/$$TR-AVT-201-ALL.pdf

Abstract

The experimental investigations of two generic UCAV configurations with control surfaces are presented. The current chapter 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 flowfield.

Item URL in elib:https://elib.dlr.de/110903/
Document Type:Other
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
Schütte, AndreasAndreas.Schuette (at) dlr.deUNSPECIFIED
Vicroy, Dan D.dan.d.vicroy (at) nasa.govUNSPECIFIED
Hübner, Andreas-Renéandreas.huebner (at) dlr.deUNSPECIFIED
Date:15 November 2016
Journal or Publication Title:NATO STO Technical Report, RTO-AVT-TR-201 on "Extended Assessment of Stability and Control Prediction Methods for NATO Air Vehicles"
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.14339/STO-TR-AVT-201
Number of Pages:22
Publisher:NATO STO - Science and Technology Organisation
ISBN:978-92-837-2079-9
Status:Published
Keywords:UCAV, Delta wing, vortical flow, stability and control, control surfaces, SACCON, AVT-201, validation, experiment, NATO, AVT, STO, prediction methods, maneuver simulation
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 , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Transport Aircraft
German-Dutch Windtunnels
Deposited By: Schütte, Andreas
Deposited On:02 Feb 2017 09:48
Last Modified:02 Feb 2017 15:56

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