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

Integrated Experimental and Numerical Resaerch on the Aerodynamics of Unsteady Aircraft

Bergmann, Andreas und Hübner, Andreas-René (2007) Integrated Experimental and Numerical Resaerch on the Aerodynamics of Unsteady Aircraft. 3rd International Symosium on Integrating CFD and Experiments in Aerodynamics, 2007-06-20 - 2007-06-21, ASAFA, Colorado.

Dieses Archiv kann nicht den gesamten Text zur Verfügung stellen.

Kurzfassung

Abstract For the experimental determination of the dynamic wind tunnel data a new combined motion test capability was developed at the German-Dutch Wind Tunnels DNW for their 3m Low Speed Wind Tunnel NWB in Braunschweig, Germany, using a unique six degree-of-freedom test rig called ‘Model Positioning Mechanism’ (MPM) as an improved successor to the older systems. With that cutting-edge device several transport aircraft configurations including a blended wing body configuration were tested in different modes of oscillatory motions roll, pitch and yaw as well as delta wing geometries like X-31 equipped with remote controlled rudders and flaps to be able to simulate realistic flight maneuvers, e.g. a Dutch Roll. This paper describes the motivation behind these tests and the test setup and in addition gives a short introduction into time accurate maneuver testing capabilities incorporating models with remote controlled control surfaces. Furthermore, the adaptation of numerical methods for the prediction of dynamic derivatives is described and some examples with the DLR-F12 configuration will be given. The calculations are based on RANS-solution using the finite volume parallel solution algorithm with an unstructured discretization concept (DLR TAU-code).

Dokumentart:Konferenzbeitrag (Vortrag, Paper)
Titel:Integrated Experimental and Numerical Resaerch on the Aerodynamics of Unsteady Aircraft
Autoren:
AutorenInstitution oder E-Mail-Adresse der Autoren
Bergmann, AndreasDNW-NWB
Hübner, Andreas-RenéNICHT SPEZIFIZIERT
Datum:Juni 2007
Referierte Publikation:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:unsteady aerodynamics, dynamic wind tunnel experiments, maneuvering aircraft, dynamic derivatives, EULER/RANS-solution, model positioning mechanism, movement device
Veranstaltungstitel:3rd International Symosium on Integrating CFD and Experiments in Aerodynamics
Veranstaltungsort:ASAFA, Colorado
Veranstaltungsart:internationale Konferenz
Veranstaltungsdatum:2007-06-20 - 2007-06-21
Veranstalter :ASAFA, Colorado
HGF - Forschungsbereich:Verkehr und Weltraum (alt)
HGF - Programm:Luftfahrt
HGF - Programmthema:keine Zuordnung
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L - keine Zuordnung
DLR - Teilgebiet (Projekt, Vorhaben):L -- keine Zuordnung
Standort: Köln-Porz , Braunschweig , Göttingen
Institute & Einrichtungen:Institut für Aerodynamik und Strömungstechnik
Institut für Aerodynamik und Strömungstechnik > Konfigurativer Entwurf
Hinterlegt von: Andreas-Rene Hübner
Hinterlegt am:31 Jan 2008
Letzte Änderung:27 Apr 2009 14:42

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.