elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Impressum | Kontakt | English
Schriftgröße: [-] Text [+]

Integrated Computational/Experimental Approach to UCAV and Delta-Canard Configurations Regarding Stability & Control

Schütte, Andreas und Cummings, Russel M. und Loeser, Thomas und Vicroy, Dan D. (2009) Integrated Computational/Experimental Approach to UCAV and Delta-Canard Configurations Regarding Stability & Control. 4th Symposium on Integrating CFD and Experiments in Aerodynamics, 14-16 Sept. 2009, Brüssel, Belgien.

Dieses Archiv kann nicht den gesamten Text zur Verfügung stellen.

Kurzfassung

In the past computational fluid dynamics (CFD) was often relegated to the position of following experimental investigations of aerodynamic vehicles. As CFD has matured and developed, the place of CFD in the vehicle development process has improved substantially, however a true integration of CFD with experiments has been slow to develop. This paper outlines the integrated approach to simulating static and dynamic stability characteristics for a generic UCAV and the X-31 configuration, as being performed by NATO RTO Task Group AVT-161. The UCAV, named SACCON (Stability And Control CONfiguration), and the X-31 are the subject of an intensive computational and experimental study. The stability characteristics of the vehicles are being evaluated via a highly integrated approach, where CFD and experimental results are being used in a parallel and collaborative fashion. The purpose of the paper is to show how these investigations have been performed in a truly integrated fashion, which has noticeably improved the knowledge gained from the program.

Dokumentart:Konferenzbeitrag (Paper)
Titel:Integrated Computational/Experimental Approach to UCAV and Delta-Canard Configurations Regarding Stability & Control
Autoren:
AutorenInstitution oder E-Mail-Adresse der Autoren
Schütte, AndreasDLR-AS-TF
Cummings, Russel M.US Air Force Academy
Loeser, ThomasDNW-NWB
Vicroy, Dan D.NASA LaRC
Datum:14 September 2009
Stichwörter:CFD, Experiment, UCAV, RTO, AVT, AVT-161, Integration, vortex flow, delta wing
Veranstaltungstitel:4th Symposium on Integrating CFD and Experiments in Aerodynamics
Veranstaltungsort:Brüssel, Belgien
Veranstaltungsart:internationale Konferenz
Veranstaltungsdatum:14-16 Sept. 2009
HGF - Forschungsbereich:keine Zuordnung
HGF - Programm:Luftfahrt
HGF - Programmthema:Starrflügler
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L AR - Starrflüglerforschung
DLR - Teilgebiet (Projekt, Vorhaben):L - Militärische Technologien
Standort: Braunschweig
Institute & Einrichtungen:Institut für Aerodynamik und Strömungstechnik
Hinterlegt von: Andreas Schütte
Hinterlegt am:15 Dez 2009 13:34
Letzte Änderung:15 Dez 2009 13:34

Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags

Blättern
Suchen
Hilfe & Kontakt
Informationen
electronic library verwendet EPrints 3.3.12
Copyright © 2008-2013 Deutsches Zentrum für Luft- und Raumfahrt (DLR). Alle Rechte vorbehalten.