1973
DOI: 10.1007/bf00035958
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An augmented double cantilever beam model for studying crack propagation and arrest

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Cited by 785 publications
(133 citation statements)
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“…Figure 19 shows the load-displacement curve at the end of one of the two arms of the specimen. The global response until the complete failure of the specimen agrees with the theoretical solution calculated for a beam on an elastic foundation [16] using linear fracture mechanics theory for the propagation [3]. The difference in slope which can be observed before the softening part of the curve is due to the fact that the damage law used in the calculation enables damage to take place progressively before the rupture of a point.…”
Section: Cohesive Interfacessupporting
confidence: 71%
“…Figure 19 shows the load-displacement curve at the end of one of the two arms of the specimen. The global response until the complete failure of the specimen agrees with the theoretical solution calculated for a beam on an elastic foundation [16] using linear fracture mechanics theory for the propagation [3]. The difference in slope which can be observed before the softening part of the curve is due to the fact that the damage law used in the calculation enables damage to take place progressively before the rupture of a point.…”
Section: Cohesive Interfacessupporting
confidence: 71%
“…The adhesion energy of the coating on PMMA was quantified using the asymmetric double cantilever beam (ADCB) test. The asymmetric specimen configuration was specially chosen to confine the debond occurring at the interface of soft polymer substrate and hard coating. The specimens (Figure ) were prepared by bonding an uncoated thinner substrate onto a coated thicker substrate using epoxy adhesive [E-20HP Hysol High Strength Epoxy Structural Adhesive, Henkel AG & Company, Düsseldorf, Germany]. The in-plane dimensions of the specimen were 9 mm × 70 mm.…”
Section: Experimental Methodsmentioning
confidence: 99%
“…The specimens were loaded with a displacement rate of 5 μm/s in tension to produce controlled coating debonding, followed by unloading. The load was measured simultaneously, and the adhesion energy, G c (J/m 2 ), was calculated from the critical value of the strain energy release rate. …”
Section: Experimental Methodsmentioning
confidence: 99%
“…An interface stiffness of the same order as the beam material's Young's modulus can be regarded as a rigid interface [18], but there is no unanimous agreement on the exact value in the literature (see, for example, Refs. [19,20,21]). For application to composite DCBs, the interfacial stiffness can be determined by 3 0…”
Section: Rigid Interfacementioning
confidence: 99%