DGLR-Publikationsdatenbank - Detailansicht
Titel:
Active Control of Three Surface Wind Tunnel Aeroelastic Demonstrator: Modelling and Correlation
Autor(en):
A. Scotti, G. Quaranta, S. Ricci
Zusammenfassung:
This article describes the methodology adopted to implement an ILAF control system on a three surface aeroelastic demonstrator with the aim of shaping fuselage modal dynamics. General concepts used, hypotheses formulated and numerical results are provided to show that a numerical simulation involving reduced order models for aeroelastic models is suitable, even at a very early design stage, especially when a control system is developed starting from scratch. Correlations with experimental wind tunnel testing show a remarkable correlation between numerical and experimental dynamic
Veranstaltung:
International Forum on Aeroelasticity and Structural Dynamics, 2005, München
Medientyp:
Conference Paper
Sprache:
englisch
Format:
21,0 x 29,7 cm, 14 Seiten
Veröffentlicht:
DGLR-Bericht, 2005, 2005-04, International Forum on Aeroelasticity and Structural Dynamics 2005; S.1-14; 2005; Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn
Preis:
NA
ISBN:
ISSN:
Kommentar:
in getr. Zählung;
Klassifikation:
Stichworte zum Inhalt:
active controls, wind tunnel models, reduced order modeling
Verfügbarkeit:
Bibliothek
Veröffentlicht:
2005
Dieses Dokument ist Teil einer übergeordneten Publikation:
International Forum on Aeroelasticity and Structural Dynamics 2005