Please use this identifier to cite or link to this item:
https://open.uns.ac.rs/handle/123456789/10817| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | Kosec G. | en |
| dc.contributor.author | Kovačlč G. | en |
| dc.contributor.author | Hodolič J. | en |
| dc.contributor.author | Kosec B. | en |
| dc.date.accessioned | 2020-03-03T14:41:24Z | - |
| dc.date.available | 2020-03-03T14:41:24Z | - |
| dc.date.issued | 2010-10-01 | en |
| dc.identifier.issn | 05435846 | en |
| dc.identifier.uri | https://open.uns.ac.rs/handle/123456789/10817 | - |
| dc.description.abstract | Generally failures of different aircraft components and parts are revealed and examined by the use of non-destructive examination methods. In further detailed explanation and interpretation of failures optical and scanning electron microscopy are used. This paper deals with a problem of a crack on aircraft wheel rim made from aluminium alloy 2014-T6. The crack was observed during regular control by the maintenance unit for non-destructive examination of the Slovenian air carrier Adria Airways. The crack on the rim of an aircraft wheel investigated was a typical fatigue crack. At same time a numerous pits were found which served as stress concentrations on the rim surface. | en |
| dc.relation.ispartof | Metalurgija | en |
| dc.title | Cracking of an aircraft wheel rim made from al-alloy 2014-T6 | en |
| dc.type | Journal/Magazine Article | en |
| dc.identifier.scopus | 2-s2.0-77956054431 | en |
| dc.identifier.url | https://api.elsevier.com/content/abstract/scopus_id/77956054431 | en |
| dc.relation.lastpage | 360 | en |
| dc.relation.firstpage | 357 | en |
| dc.relation.issue | 4 | en |
| dc.relation.volume | 49 | en |
| item.grantfulltext | none | - |
| item.fulltext | No Fulltext | - |
| Appears in Collections: | FTN Publikacije/Publications | |
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