Buckling strength of FML profiles of ‘classic’ versus thin-ply design

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dc.contributor.authorMania, Radosław
dc.contributor.authorYork, Christopher
dc.date.accessioned2024-04-23T08:51:00Z
dc.date.available2024-04-23T08:51:00Z
dc.date.issued2016
dc.description.abstractThe past few decades have seen the introduction of fiber metal laminates (FMLs), especially GLARE, into primary structure applications such as the fuselage of the largest civil transport aircraft in current production: the Airbus A380. GLARE material properties, as well as FMLs in general, exhibit partly metallic and partly composite behaviour. The hybrid nature of FML has several advantages when compared with monolithic aluminium application to fuselage skins, i.e. lower density and crack arresting capability of the fiber layers in presence of a fatigue cracks, which are a major concern in the design of monolithic aluminium . The possibility to tailor the material to meet specific structural or mechanical requirements, by appropriate orientation of the fibers layers, is especially important. These features allow to some extent the concerns about `flying with undetectable fatigue damage´, which influences inspection intervals and the economics of airframe maintenanceen_EN
dc.identifier.citationMania R., York C., Buckling strength of FML profiles of ‘classic’ versus thin-ply design. W: Statics, Dynamics and Stability of Structures. Vol. 6 Research Advances in Applied Mechanics, Mania R. (Ed.), A Series of Monographs; No 2180, Wydawnictwo Politechniki Łódzkiej, Łódź 2016, s. 88-110, ISBN 978-83-7283-768-4
dc.identifier.isbnISBN 978-83-7283-768-4
dc.identifier.urihttp://hdl.handle.net/11652/5271
dc.language.isoeng
dc.page.numbers. 88-110
dc.publisherWydawnictwo Politechniki Łódzkiejpl_PL
dc.publisherLodz University of Technology Pressen_EN
dc.relation.ispartofMania R. (Ed.), Statics, Dynamics and Stability of Structures. Vol. 6 Research Advances in Applied Mechanics, A Series of Monographs; No 2180, Wydawnictwo Politechniki Łódzkiej, Łódź 2016, ISBN 978-83-7283-768-4, DOI 10.34658/9788372837684
dc.rightsDla wszystkich w zakresie dozwolonego użytkupl_PL
dc.rightsFair use conditionen_EN
dc.rights.licenseLicencja PŁpl_PL
dc.rights.licenseLUT Licenseen_EN
dc.subjectstructural stabilityen_EN
dc.subjectconstruction dynamicsen_EN
dc.subjectapplied mechanicsen_EN
dc.subjectstabilność konstrukcjipl_PL
dc.subjectdynamika konstrukcjipl_PL
dc.subjectmechanika stosowanapl_PL
dc.titleBuckling strength of FML profiles of ‘classic’ versus thin-ply design
dc.typeRozdział - monografiapl_PL
dc.typeChapter - monographpl_PL

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