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HIGH SPEED STATIC EXPERIMENTALINVESTIGATIONS TO ESTIMATE CONTROL DEVICEEFFECTIVENESS AND S&C CAPABILITIES (Chapter 5)

Rein, Martin and Irving, Jonathan and Rigby, Glyn and Birch, Trevor J. (2016) HIGH SPEED STATIC EXPERIMENTALINVESTIGATIONS TO ESTIMATE CONTROL DEVICEEFFECTIVENESS AND S&C CAPABILITIES (Chapter 5). Other. STO-TR-AVT-201, 18 S. NATO Science & Technology Organization.

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Official URL: https://www.sto.nato.int/publications/STO%20Technical%20Reports/Forms/DispForm.aspx?ID=3921&RootFolder=STO%20Technical%20Reports%2FSTO%2DTR%2DAVT%2D201&IsDlg=1

Abstract

Within the AVT-201 Task Group a comprehensive research program has been designed to assess the ability to accurately predict both static and dynamic stability characteristics of air vehicles using Computational Fluid Dynamics (CFD) methods which 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. The AVT-201 Task Group established an extended integrated experimental and numerical approach to assess the performance and accuracy of stability and control prediction methods as well as the ability to design and estimate the effectiveness of control devices for highly swept low observable UCAV configurations. The aim of the AVT-201 Task Group was 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/110179/
Document Type:Monograph (Other)
Title:HIGH SPEED STATIC EXPERIMENTALINVESTIGATIONS TO ESTIMATE CONTROL DEVICEEFFECTIVENESS AND S&C CAPABILITIES (Chapter 5)
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.tjbirch (at) dstl.gov.ukUNSPECIFIED
Date:11 November 2016
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:18
Publisher:NATO Science & Technology Organization
Series Name:Technical Report
ISBN:978-92-837-2079-9
Status:Published
Keywords:static and dynamic stability characteristics, control devices, highly swept wings
Institution:NATO Science & Technology Organization
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, L - Concepts and Integration, L - Flight Physics
Location: Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > High Speed Configurations, GO
Deposited By: Bachmann, Barbara
Deposited On:06 Jan 2017 13:54
Last Modified:20 Nov 2018 17:38

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