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<rdf:RDF xmlns:rdf="http://www.w3.org/1999/02/22-rdf-syntax-ns#" xmlns:dc="http://purl.org/dc/elements/1.1/"><rdf:Description rdf:about="https://repozitorij.uni-lj.si/IzpisGradiva.php?id=185935"><dc:title>Fatigue life and failure mechanisms of cord-reinforced rubber composites: influence of fiber orientation, layer architecture, and matrix thickness</dc:title><dc:creator>Głowacka,	Karolina	(Avtor)
	</dc:creator><dc:creator>Małecka,	J.	(Avtor)
	</dc:creator><dc:creator>Pawliczek,	Roland	(Avtor)
	</dc:creator><dc:creator>Kurek,	A.	(Avtor)
	</dc:creator><dc:creator>Nagode,	Marko	(Avtor)
	</dc:creator><dc:creator>Klemenc,	Jernej	(Avtor)
	</dc:creator><dc:creator>Łagoda,	Tadeusz	(Avtor)
	</dc:creator><dc:subject>composite</dc:subject><dc:subject>rubber</dc:subject><dc:subject>fatigue</dc:subject><dc:subject>uniaxial loading</dc:subject><dc:subject>mean value</dc:subject><dc:description>This study investigates the fatigue life of cord-reinforced rubber composites subjected to fully reversed three-point bending. Although nominally a bending test, the high displacement amplitudes and low specimen stiffness lead to a tension-dominated loading state due to geometric nonlinearity. The research focuses on the influence of fiber orientation (0/90° vs. ±45°) and the number of reinforcement layers on fatigue durability. It was demonstrated that traditional parameters, such as strain amplitude or maximum strain, are insufficient to describe fatigue life under non-zero-mean-strain conditions. Instead, the Smith- Watson-Topper (SWT) and Walker models were successfully employed to unify the results. The findings reveal that ±45° configurations exhibit superior fatigue life compared to 0/90° layups under strain-controlled conditions, primarily due to fiber reorientation and lower internal stress levels. Analysis using the Walker model showed that single-layer composites are more sensitive to maximum strain (γ = 0.3), whereas double-layer systems are dominated by strain amplitude (γ = 0.7) due to interlaminar shear and internal friction. Furthermore, a critical relationship between matrix thickness and reinforcement ratio was identified: increasing rubber thickness improves durability in single-layer systems but deteriorates it in double-layer composites due to weakened crack-bridging mechanisms. SEM analysis confirmed these findings, highlighting the role of fiber pull-out and interlaminar degradation. Finally, the study highlights a lack of correlation between static tensile strength and fatigue performance, underscoring the need to account for viscoelastic effects in the design of cord-rubber structures.</dc:description><dc:date>2026</dc:date><dc:date>2026-08-24 09:45:58</dc:date><dc:type>Članek v reviji</dc:type><dc:identifier>185935</dc:identifier><dc:language>sl</dc:language></rdf:Description></rdf:RDF>
