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Mechanics of Composite Materials
Erschienen in: Mechanics of Composite Materials 5/2023

31.10.2023

Interlaminar Shear Strength Behavior of Carbon Fiber Reinforced Aluminum Alloy Laminate

verfasst von: Zijing Qu, Yibo Li, Minghui Huang, Lei Dong

Erschienen in: Mechanics of Composite Materials | Ausgabe 5/2023

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Abstract

The interlayer bonding ability is a crucial indicator of thermoplastic fiber metal laminates (FMLs). Using different preparation strategies and adhesive thicknesses, a series of fiber metal laminates were prepared from 2024-T3 Al alloy, unidirectional carbon fiber prepreg tapes, and films of polyether ether ketone. The span-thickness ratio for this type of laminates was examined and characterized to identify the most suitable span-thickness ratio. The effects of adhesive layer thickness on the interlaminar properties of FMLs were investigated, and the failure processes were analyzed by microscopic observation. The results show that lower span-thickness ratios have better applicability in thermoplastic carbon fiber aluminum alloy laminates. The adhesive layer presence significantly affects interlaminar properties independent of its thickness, and the FMLs with unidirectional alignment and anodized treatment possess stronger shear resistance.
Vorheriger Artikel Shear Buckling Mode and Failure of Flat Fiber-Reinforced Specimens Under Axial Compression 1. Refined Nonlinear Mathematical Deformation Model
Nächster Artikel The Continual Mechanics of Frontally Growing Objects. Theory

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Metadaten
Titel
Interlaminar Shear Strength Behavior of Carbon Fiber Reinforced Aluminum Alloy Laminate
verfasst von
Zijing Qu
Yibo Li
Minghui Huang
Lei Dong
Publikationsdatum
31.10.2023
Verlag
Springer US
Erschienen in
Mechanics of Composite Materials / Ausgabe 5/2023
Print ISSN: 0191-5665
Elektronische ISSN: 1573-8922
DOI
https://doi.org/10.1007/s11029-023-10141-7

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