Baza Publikacji Pracowników Politechniki Lubelskiej

Status:
Autorzy:	Dadej Konrad, Bieniaś Jarosław, Surowska Barbara
Dyscypliny:
	Aby zobaczyć szczegóły należy się zalogować.
Rok wydania:	2017
Wersja dokumentu:	Drukowana \| Elektroniczna
Język:	angielski
Numer czasopisma:	Pt 1
Wolumen/Tom:	100
Strony:	94 - 104
Impact Factor:	3,132
Web of Science® Times Cited:	46
Scopus® Cytowania:	55
Bazy:	Web of Science \| Scopus
Efekt badań statutowych	NIE
Materiał konferencyjny:	NIE
Publikacja OA:	NIE
Abstrakty:	angielski
	The life cycle of fiber metal laminates subjected to mechanical fatigue is commonly divided into three stages: crack initiation, crack propagation, and final failure. However for some configurations of fiber metal laminates, the composite component may keep its fatigue load carrying capabilities, even after through the thickness metal failure, whereas normally the structure was expected to fail entirely. The aim of this article was to identify and analyse the mechanisms which are the key for appearance of residual fatigue life phase of fiber metal lamiantes. The results show that the shape of the stress-cycles curve, as well as the static tensile strength of particular fiber metal laminate components are crucial for the presence of residual fatigue life. The study also presents a general methodology for stress-cycle curve prediction for any type of FML laminates.

Residual fatigue life of carbon fibre aluminium laminates