DGLR-Publikationsdatenbank - Detailansicht
Titel:
Fatigue Tolerant Design in Airframes and the Influence of Vibration Suppression on Crack Growth in Helicopters
Autor(en):
H. Perrett, J.P. Dawkins
Zusammenfassung:
A study is presented of flaw tolerant design methodology in rotary and fixed wing aircraft. Flaw tolerant design is compared to safe life design with reference to the requirements of FAR29 and the influence of load spectrum content is used to illustrate fundamental differences between rotary and fixed wing applications. Crack growth prediction is used to show how the Active Control of Structural Response in helicopter airframes can modify the loading environment so as to restore the ability to apply flaw tolerant design.
Veranstaltung:
23rd ICAF Symposium of the international Committee on Aeronautical Fatique, 2005, Hamburg
Medientyp:
Conference Paper
Sprache:
englisch
Format:
A5, 12 Seiten
Veröffentlicht:
DGLR-Bericht, 2005, 2005-03, 23rd ICAF Symposium of the international Committee on Aeronautical Fatique - Proceedings; S.341-352; 2005; Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn
Preis:
NA
ISBN:
ISSN:
Kommentar:
Klassifikation:
Stichworte zum Inhalt:
helicopters, vibrations, fatigue
Verfügbarkeit:
Bestellbar
Veröffentlicht:
2005
Dieses Dokument ist Teil einer übergeordneten Publikation:
23rd ICAF Symposium of the international Committee on Aeronautical Fatique - Proceedings