Use of modern numerical methods for fatigue life predictions

dc.creator	Grbović, Aleksandar
dc.creator	Rašuo, Boško
dc.date.accessioned	2022-09-19T17:30:23Z
dc.date.available	2022-09-19T17:30:23Z
dc.date.issued	2014
dc.identifier.uri	https://machinery.mas.bg.ac.rs/handle/123456789/1978
dc.description.abstract	In this chapter, FEM is used for fatigue crack growth predictions on 2D model of the spar, whereas XFEM is used for fatigue crack growth predictions and fatigue life estimation of corresponding 3D model. The values of stress intensity factors (SIFs) are extracted from FRANC2D software and MorfeoCrack for Abaqus add-on. The results obtained corresponded well with the experimental values, which proves that numerical methods can be successfully used in the determination of proper inspection intervals for the purpose of preventing the catastrophic failure of structural components under variable amplitude loading.	en
dc.publisher	Nova Science Publishers, Inc.
dc.rights	restrictedAccess
dc.source	Recent Trends in Fatigue Design
dc.subject	XFEM	en
dc.subject	FEM	en
dc.subject	Fatigue	en
dc.subject	Failure	en
dc.subject	Crack	en
dc.subject	Aircraft	en
dc.title	Use of modern numerical methods for fatigue life predictions	en
dc.type	bookPart
dc.rights.license	ARR
dc.citation.epage	73
dc.citation.other	: 31-73
dc.citation.spage	31
dc.identifier.rcub	https://hdl.handle.net/21.15107/rcub_machinery_1978
dc.identifier.scopus	2-s2.0-84955154715
dc.type.version	publishedVersion

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