Mode I fatigue cracking in a fiber reinforced metal matrix composite
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2012, Composites Part A: Applied Science and ManufacturingCitation Excerpt :A literature review revealed that the behavior of composite laminates is strongly affected by the stress ratio, in a consistent way however, which allows the derivation of universal formulations that can simulate this effect independently of the examined material [7]. Extensive research efforts were also devoted to the investigation of the fatigue crack growth under Mode I [8–11], Mode II [12,13] and mixed-Mode fracture [14,15] of composite joints under fatigue loading. Instead of the S–N curves, fatigue crack growth (FCG) curves are used to represent the fatigue behavior and also provide information concerning the developed damage in terms of crack or cracks that propagate during fatigue loading.
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