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INTRODUCTION TO THE AVT-161 AIR FACET: AN INTEGRATED COMPUTATIONAL/EXPERIMENTAL APPROACH TO UCAV STABILITY AND CONTROL ESTIMATION

Cummings, Russel M. and Schütte, Andreas (2009) INTRODUCTION TO THE AVT-161 AIR FACET: AN INTEGRATED COMPUTATIONAL/EXPERIMENTAL APPROACH TO UCAV STABILITY AND CONTROL ESTIMATION. NATO RTO - Research and Technology Organisation. [Other]

Full text not available from this repository.

Official URL: https://www.sto.nato.int/publications/STO%20Technical%20Reports/RTO-TR-AVT-161/$$TR-AVT-161-ALL.pdf

Abstract

Within the AVT-161 Task Group a comprehensive research program designed to investigate the ability of computational methods to predict stability and control characteristics of a generic unmanned combat air vehicle and the X-31 experimental aircraft has been undertaken. The integrated approach to simulating static and dynamic stability characteristics was performed by the NATO RTO Task Group AVT-161. The UCAV, named SACCON (Stability and Control Configuration), and the X-31 configuration was the subject of an intensive computational and experimental study. The stability characteristics of the vehicles were evaluated via a highly integrated approach, where CFD and experimental results were used in a parallel and collaborative fashion. The results show that computational methods have made great strides in predicting static and dynamic stability characteristics, but several key issues need to be resolved before efficient, affordable, and reliable predictions are available.

Item URL in elib:https://elib.dlr.de/110895/
Document Type:Other
Title:INTRODUCTION TO THE AVT-161 AIR FACET: AN INTEGRATED COMPUTATIONAL/EXPERIMENTAL APPROACH TO UCAV STABILITY AND CONTROL ESTIMATION
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Cummings, Russel M.russ.cummings (at) usafa.eduUNSPECIFIED
Schütte, AndreasAndreas.Schuette (at) dlr.deUNSPECIFIED
Date:4 September 2009
Journal or Publication Title:NATO RTO Technical Report, RTO-AVT-TR-161 on "Assessment of Stability and Control Prediction Methods for NATO Air and Sea Vehicles"
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.14339/RTO-TR-AVT-161
Number of Pages:28
Publisher:NATO RTO - Research and Technology Organisation
Status:Published
Keywords:UCAV, Delta wing, vortical flow, stability and control, validation, Experiment, cfd, NATO, AVT, RTO
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
Deposited By: Schütte, Andreas
Deposited On:30 Jan 2017 10:04
Last Modified:30 Jan 2017 10:04

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