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SACCON STATIC WIND TUNNEL TESTS AT DNW-NWB AND 14ft × 22ft NASA LARC

Löser, Thomas and Vicroy, Dan D. and Schütte, Andreas (2009) SACCON STATIC WIND TUNNEL TESTS AT DNW-NWB AND 14ft × 22ft NASA LARC. 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

Static force and pressure measurement results obtained from three test campaigns in two different wind tunnels are presented. The model investigated was the generic UCAF configuration SACCON. Model design, manufacture, as well as three wind tunnel entries have been performed within the NATO/RTO AVT-161 Task Group “Assessment of Stability and Control Prediction Methods for NATO Air and Sea Vehicles”. The model has undergone static as well as dynamic tests as an international co-operation; the tests have been accompanied by corresponding numerical investigations. This chapter covers the static part of the wind tunnel experiments. Model and instrumentation are described in detail and, focussing on the force measurement results, the effects of the different parameters are explained.

Item URL in elib:https://elib.dlr.de/110896/
Document Type:Other
Title:SACCON STATIC WIND TUNNEL TESTS AT DNW-NWB AND 14ft × 22ft NASA LARC
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Löser, Thomasthomas.loeser (at) dnw.aeroUNSPECIFIED
Vicroy, Dan D.dan.d.vicroy (at) nasa.govUNSPECIFIED
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:22
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 10:05
Last Modified:30 Jan 2017 10:05

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