DGLR-Publikationsdatenbank - Detailansicht
Titel:
Flutter Simulation of a T-Tail by using Non Linear Aerodynamics
Autor(en):
H. Arizono, H.R. Kheirandish, J. Nakamichi
Zusammenfassung:
Numerical flutter simulation of the T-tail plane in transonic region is presented. A code for aeroelasticity simulations based on Multi-block and Overset grid concept was developed and has been applied to T-tail configuration. Flutter simulations are performed at Mach numbers 0.70 - 0.95, and those results are well accorded with the experimental results. The effects of the angle of attack for the flutter boundary are also presented.
Veranstaltung:
International Forum on Aeroelasticity and Structural Dynamics, 2005, München
Medientyp:
Conference Paper
Sprache:
englisch
Format:
21,0 x 29,7 cm, 8 Seiten
Veröffentlicht:
DGLR-Bericht, 2005, 2005-04, International Forum on Aeroelasticity and Structural Dynamics 2005; S.1-8; 2005; Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn
Preis:
NA
ISBN:
ISSN:
Kommentar:
in getr. Zählung;
Klassifikation:
Stichworte zum Inhalt:
aerodynamics, flutter
Verfügbarkeit:
Bibliothek
Veröffentlicht:
2005
Dieses Dokument ist Teil einer übergeordneten Publikation:
International Forum on Aeroelasticity and Structural Dynamics 2005