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 | |