Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
4917861 | Composite Structures | 2017 | 9 Pages |
Abstract
A testing method is presented to determine the pull-out behavior of interleaving metallic z-reinforcements for carbon fiber reinforced polymer (CFRP) laminates and joints. Energy absorbing mechanisms are described with respect to the metallic materials and means of surface pretreatment applied. Mechanical, wet-chemical and physical pretreatments result in milli-, micro- and nanoscaled oxide morphologies of titanium and stainless steel surfaces. Both, a high macro roughness of the reinforcement surface and a low difference in thermal expansion with regard to the surrounding CFRP is clearly proven to feature the highest level of energy absorption during pull-out tests. Surface analyses through scanning electron microscopy (SEM) and X-ray photoelectron spectroscopy (XPS) indicate laser-induced nanostructure's scale and morphology to provide good adhesion properties but not to allow macroscopic friction between metal surface and epoxy resin.
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Authors
Michael Juergens, Manuel Tiago von Hafe Pérez Ferreira da Silva, Sebastian Heimbs, Holger Lang, Elisabeth Ladstaetter, Elke Hombergsmeier,