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FLOW PHYSICS ANALYSES ON THE UCAV SACCON CONFIGURATION USING AN INTEGRATED COMPUTATIONAL AND EXPERIMENTAL APPROACH

Schütte, Andreas and Hummel, Dietrich and Hitzel, Stephan M. (2009) FLOW PHYSICS ANALYSES ON THE UCAV SACCON CONFIGURATION USING AN INTEGRATED COMPUTATIONAL AND EXPERIMENTAL APPROACH. 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 understanding of the vortical flow in connection with the non-linear aerodynamic behavior of the UCAV SACCON “Stability And Control CONfiguration” configuration is the subject of this paper. For this purpose, an integrated approach is used taking experimental data and numerical results into account to establish an entire picture of the flow physics and induced aerodynamic behavior in symmetrical flow.

Item URL in elib:https://elib.dlr.de/110898/
Document Type:Other
Title:FLOW PHYSICS ANALYSES ON THE UCAV SACCON CONFIGURATION USING AN INTEGRATED COMPUTATIONAL AND EXPERIMENTAL APPROACH
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schütte, AndreasAndreas.Schuette (at) dlr.deUNSPECIFIED
Hummel, Dietrichdietrich.hummel (at) tu-braunschweig.deUNSPECIFIED
Hitzel, Stephan M.stephan.hitzel (at) airbus.comUNSPECIFIED
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:40
Publisher:NATO RTO - Research and Technology Organisation
Status:Published
Keywords:UCAV, Delta wing, vortical flow, stability and control, validation, Experiment, cfd, NATO, AVT, RTO, SACCON, DLR TAU
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 10:25
Last Modified:30 Jan 2017 10:25

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