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SACCON UCAV FORCED OSCILLATION TESTS AT DNW-NWB AND NASA LANGLEY 14ft × 22ft TUNNEL

Vicroy, Dan D. and Löser, Thomas and Schütte, Andreas (2009) SACCON UCAV FORCED OSCILLATION TESTS AT DNW-NWB AND NASA LANGLEY 14ft × 22ft TUNNEL. 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

The role of Computational Fluid Dynamics (CFD) methods in the design process of both air and sea vehicles continues to grow. However, the ability of CFD to accurately predict the static and dynamic stability characteristics of these vehicles has yet to be validated. An Applied Vehicle Technology Task Group (AVT-161) was established by the NATO Research and Technology Organization (RTO) to assess the state-of-the-art in CFD methods for the prediction of static and dynamic stability and control characteristics of military vehicles in the air and sea domains. Two highly swept wing configurations were selected for the air vehicle experimental and numerical investigations. The primary configuration was a generic UCAV geometry called SACCON – “Stability And Control CONfiguration”. The SACCON model mounted in the Low-Speed Wind Tunnel Braunschweig (DNW-NWB) is shown in Figure 3-1. The other focus air vehicle of AVT-161 was the X-31. This paper presents the results of a series of forced oscillation tests of the SACCON model conducted in both the DNW-NWB low-speed wind tunnel and the NASA Langley 14′ × 22′ Subsonic Tunnel. A complementary set of static data were also collected during these tests and reported in reference.

Item URL in elib:https://elib.dlr.de/110897/
Document Type:Other
Title:SACCON UCAV FORCED OSCILLATION TESTS AT DNW-NWB AND NASA LANGLEY 14ft × 22ft TUNNEL
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Vicroy, Dan D.dan.d.vicroy (at) nasa.govUNSPECIFIED
Löser, Thomasdnw-nwbUNSPECIFIED
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
In DOAJ:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.14339/RTO-TR-AVT-161
Number of Pages:42
Publisher:NATO RTO - Research and Technology Organisation
Status:Published
Keywords:UCAV, Delta wing, vortical flow, stability and control, validation, Experiment, NATO, AVT, RTO, DNW-NWB, MPM, NASA. dynamic tests, maneuver
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
German-Dutch Windtunnels
Deposited By: Schütte, Andreas
Deposited On:30 Jan 2017 10:24
Last Modified:30 Jan 2017 10:24

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