Fatigue delamination growth of carbon and glass reinforced fiber metal laminates in fracture mode II
Source abstract
Abstract
Abstract Fatigue delamination growth (FDG) rate was investigated in composite laminates with aluminium and carbon/glass fibers. An End Notch Flexure test was used to determine compliance-calibration as well as fatigue and quasi-static interlaminar fracture. Experimental tests results suggest, that fatigue delamination threshold in a metal-composite interface is governed by the epoxy matrix, while the FDG rate is governed by the fibers/matrix cohesion. Deceleration of delamination growth was observed when delamination reached a central point of the specimen. Generally, laminates reinforced by glass fibers are more resistant for delamination growth than reinforced by carbon fibers.
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Research context
OpenAlex topics: Mechanical Behavior of Composites · Fatigue and fracture mechanics · Ultrasonics and Acoustic Wave Propagation
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
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