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Mechanics of Composite Materials
Erschienen in: Mechanics of Composite Materials 5/2016

10.11.2016

Hybrid Laminates for Application in North Conditions

verfasst von: V. V. Antipov, E. I. Oreshko, V. S. Erasov, N. Yu. Serebrennikova

Erschienen in: Mechanics of Composite Materials | Ausgabe 5/2016

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Abstract

A hybrid aluminum-lithium alloy/SIAL laminate as a possible material for application in structures operated in North conditions is considered. The finite-element method is used for a buckling stability analysis of hybrid panels, bars, and plates. A technique allowing one to compare the buckling stability of multilayered hybrid plates is offered. Compression tests were run on a hybrid laminate wing panel as a prototype of the top panel of TU-204SM airplane made from a high-strength B95T2 aluminum alloy. It turned out that the lighter composite panel had a higher load-carrying capacity than the aluminum one. Results of investigation into the properties the hybrid aluminum-lithium alloy/SIAL laminate and an analysis of scientific-technical data on this subject showed that this composite material could be used in the elements of airframes, including those operated in north conditions.
Vorheriger Artikel Effect of surface and interface energies on the nonlinear bending behaviour of nanoscale laminated thin plates
Nächster Artikel Incremental Carcass Theory of Polycrystalline Media at Large Elastic and Plastic Deformations

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Metadaten
Titel
Hybrid Laminates for Application in North Conditions
verfasst von
V. V. Antipov
E. I. Oreshko
V. S. Erasov
N. Yu. Serebrennikova
Publikationsdatum
10.11.2016
Verlag
Springer US
Erschienen in
Mechanics of Composite Materials / Ausgabe 5/2016
Print ISSN: 0191-5665
Elektronische ISSN: 1573-8922
DOI
https://doi.org/10.1007/s11029-016-9617-9

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