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      Thin fiber metal laminates comprising functionally graded ballistic-grade fabrics subjected to mechanical and damping characterization

      , , ,
      Thin-Walled Structures
      Elsevier BV

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          Production and mechanical properties of Al2O3 particle-reinforced 2024 aluminium alloy composites

          M. Kok (2005)
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            A review on the development and properties of continuous fiber/epoxy/aluminum hybrid composites for aircraft structures

            Weight reduction and improved damage tolerance characteristics were the prime drivers to develop new family of materials for the aerospace/aeronautical industry. Aiming this objective, a new lightweight Fiber/Metal Laminate (FML) has been developed. The combination of metal and polymer composite laminates can create a synergistic effect on many properties. The mechanical properties of FML shows improvements over the properties of both aluminum alloys and composite materials individually. Due to their excellent properties, FML are being used as fuselage skin structures of the next generation commercial aircrafts. One of the advantages of FML when compared with conventional carbon fiber/epoxy composites is the low moisture absorption. The moisture absorption in FML composites is slower when compared with polymer composites, even under the relatively harsh conditions, due to the barrier of the aluminum outer layers. Due to this favorable atmosphere, recently big companies such as EMBRAER, Aerospatiale, Boing, Airbus, and so one, starting to work with this kind of materials as an alternative to save money and to guarantee the security of their aircrafts.
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              Effects of various aluminum surface treatments on the basalt fiber metal laminates interlaminar adhesion

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                Author and article information

                Contributors
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                Journal
                Thin-Walled Structures
                Thin-Walled Structures
                Elsevier BV
                02638231
                April 2023
                April 2023
                : 185
                : 110628
                Article
                10.1016/j.tws.2023.110628
                123f930e-5dd9-4412-aba2-580a4ec2a0d5
                © 2023

                https://www.elsevier.com/tdm/userlicense/1.0/

                https://doi.org/10.15223/policy-017

                https://doi.org/10.15223/policy-037

                https://doi.org/10.15223/policy-012

                https://doi.org/10.15223/policy-029

                https://doi.org/10.15223/policy-004

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