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THE NATO STO TASK GROUP AVT-201

Cummings, Russel M. and Schütte, Andreas (2016) THE NATO STO TASK GROUP AVT-201. NATO STO - Science and Technology Organisation. [Other]

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

Abstract

The ability to accurately predict both static and dynamic stability characteristics of air vehicles using Computational Fluid Dynamics (CFD) methods could revolutionize the air vehicle design process, especially for military air vehicles. A validated CFD capability would significantly reduce the number of ground tests required to verify vehicle concepts and, in general, could eliminate costly vehicle ‘repair’ campaigns required to fix performance anomalies that were not adequately predicted prior to full-scale vehicle development. This chapter outlines the extended integrated experimental and numerical approach to assess the of stability and control prediction method capabilities as well as the design and estimation the control device effectiveness for highly swept low observable UCAV configurations. The aim of the AVT-201 Task Group is to provide an assessment of the CFD capabilities using model-scale experiments and transferring this knowledge to real-scale applications

Item URL in elib:https://elib.dlr.de/110901/
Document Type:Other
Title:THE NATO STO TASK GROUP AVT-201
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Cummings, Russel M.russ.cummings (at) usafa.eduUNSPECIFIED
Schütte, AndreasAndreas.Schuette (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:20
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, cfd, NATO, AVT, STO, prediction methods
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
Deposited By: Schütte, Andreas
Deposited On:02 Feb 2017 09:45
Last Modified:02 Feb 2017 09:45

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