DGLR-Publikationsdatenbank - Detailansicht
Titel:
Buckling Behaviour of Composite Shells under Combined Loading
Autor(en):
V. Giavotto, C. Poggi
Zusammenfassung:
The research project presented in this paper aims at improving the knowledge of the buckling behaviour of composite shell structures through an extensive experimental analytical and numerical investigation. Comparison of the numerical and analytical results with the experiments will allow validation of the numerical tools that can be used in further wide parametric studies. The main objective is to produce strength design criteria for composite cylinders under combined loading. The current status of the project is presented and the first experimental and numerical results discussed. Furthermore, a theoretical investigation, performed to analyse the effects of the lamination geometries on the buckling and post-buckling behaviour of imperfect composite cylindrical shells is presented.
Veranstaltung:
17th European Rotorcraft Forum 1991, Berlin
Medientyp:
Conference Paper
Sprache:
englisch
Format:
21,0 x 29,7 cm, 13 Seiten
Veröffentlicht:
DGLR-Bericht, 1991, 1991-08, 17th European Rotorcraft Forum Proceedings; 1991; Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn
Preis:
NA
ISBN:
ISSN:
Kommentar:
Dieser Aufsatz ist nicht Teil der Veröffentlichung!
Klassifikation:
Stichworte zum Inhalt:
composite materials, helicopters, structural dynamic analysis, buckling
Verfügbarkeit:
Bestellbar
Veröffentlicht:
1991
Dieses Dokument ist Teil einer übergeordneten Publikation:
17th European Rotorcraft Forum Proceedings