Reparation of Composites used in Naval Industry
Source abstract
Abstract
In this work the repairing process of a completely cured epoxy-glass laminate was simulated. Repairing plaques were joined to the original material at different curing temperatures. After reparation, delamination, lap-shear and impact tests were carried out. Fiber bridging was observed. The optimum temperature for delamination was 70°C. Strength and modulus increased with the curing temperature. In the case of impact test, higher temperature favored the patch failure against the failure of the base material.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Mechanical Behavior of Composites · Epoxy Resin Curing Processes · Structural Analysis of Composite Materials
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Affiliations
Research Institute of Material Science and Technology (INTEMA) National Research Council (CONICET)- Universidad Nacional de Mar del Plata Av. Juan B. Justo 4302, 7600 Mar del Plata. Argentina
Research Institute of Material Science and Technology (INTEMA) National Research Council (CONICET)- Universidad Nacional de Mar del Plata Av. Juan B. Justo 4302, 7600 Mar del Plata. Argentina,
References (8)
Show source-provided references
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