2020
DOI: 10.3390/met10050699
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Interfacial Fracture Toughness Assessment of a New Titanium–CFRP Adhesive Joint: An Experimental Comparative Study

Abstract: Adhesive joints between dissimilar layers of metals and composites are increasingly used by different industries, as they promise significant weight savings and, consequently, a reduction in energy consumption and pollutant emissions. In the present work, the interfacial fracture behavior of a new titanium–carbon fiber reinforced plastic (CFRP) adhesive joint is experimentally investigated using the double cantilever beam (DCB) and end-notched flexure (ENF) test configurations. A potential application of this … Show more

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Cited by 21 publications
(8 citation statements)
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“…Due to the mismatch between the materials on both sides of the interface, mixed-mode states produce inherently in the crack tip. The stress intensity factors in the interface crack tip calculated for the modified Arcan sample are simply the real and imaginary parts of a complex tress intensity factor K = K1 + iK2 (Choupani, 2008b;Mirsayar et al, 2014;Tsokanas et al, 2020). For an interfacial crack between two dissimilar isotropic materials with Young's moduli E1 and E2, Poisson's ratios v1 and v2, shear moduli µ1 and µ2, and biomaterial constant β, the strain energy release rate for plane strain condition can be calculated as:…”
Section: Cohesive Interfacial and Interlaminar Fracture Mechanicsmentioning
confidence: 99%
“…Due to the mismatch between the materials on both sides of the interface, mixed-mode states produce inherently in the crack tip. The stress intensity factors in the interface crack tip calculated for the modified Arcan sample are simply the real and imaginary parts of a complex tress intensity factor K = K1 + iK2 (Choupani, 2008b;Mirsayar et al, 2014;Tsokanas et al, 2020). For an interfacial crack between two dissimilar isotropic materials with Young's moduli E1 and E2, Poisson's ratios v1 and v2, shear moduli µ1 and µ2, and biomaterial constant β, the strain energy release rate for plane strain condition can be calculated as:…”
Section: Cohesive Interfacial and Interlaminar Fracture Mechanicsmentioning
confidence: 99%
“…In recent years the connection of different materials has become more and more popular due to the development, in particular, of composite materials and bonding techniques. The number of such solutions has increased drastically in many industries, particularly in the automotive or aviation industry and others and is reflected by the growing year-to-year number of papers [30][31][32][33][34][35][36][37][38][39][40][41].…”
Section: Introductionmentioning
confidence: 99%
“…[43][44][45]. The main failure forms of the adhesive joints are adhesive failure, cohesive failure, thin-layer cohesive failure, stock-break failure, fiber-tear and light-fiber-tear failure and adherend failure outside the joint [38,44,45]. The significant influence on the joint strength has a suitable selection of the adhesive material.…”
Section: Introductionmentioning
confidence: 99%
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“…The most common reinforcements are glass, aramid, and carbon fibers. The production of carbon fibers has enabled the development of new composite materials with high strengths and low densities [3]. These materials are widely preferred in various applications, due to their high specific strength and modulus [4].…”
Section: Introductionmentioning
confidence: 99%