2006
DOI: 10.1016/j.commatsci.2005.09.004
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Fatigue modeling of short fiber reinforced composites with ductile matrix under cyclic loading

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Cited by 24 publications
(12 citation statements)
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“…m w is the shape parameter and controls the brittleness of the material and a d is the scale parameter (Weibull modulus). The Weibull damage model has been applied to model debonding effects in fiber reinforced composites (Kabir et al, 2006;Kim and Lee, 2011;Lee, 2001). Despite the fact that shale can be viewed as a geomaterial with a clay rich matrix and brittle bonds inclusion as a result of diagenetic processes, in the present work the damage model is introduced as purely phenomenological and no connection between microstructure and the damage evolution function is asserted.…”
Section: Coupled Plastic-damage Modelmentioning
confidence: 99%
“…m w is the shape parameter and controls the brittleness of the material and a d is the scale parameter (Weibull modulus). The Weibull damage model has been applied to model debonding effects in fiber reinforced composites (Kabir et al, 2006;Kim and Lee, 2011;Lee, 2001). Despite the fact that shale can be viewed as a geomaterial with a clay rich matrix and brittle bonds inclusion as a result of diagenetic processes, in the present work the damage model is introduced as purely phenomenological and no connection between microstructure and the damage evolution function is asserted.…”
Section: Coupled Plastic-damage Modelmentioning
confidence: 99%
“…Which ratio of fibers are aligned along or transverse to the main direction, is described by means of the eigenvalues of the three-dimensional orientation tensor . (6) Kabir et al [10] have shown that at 0° and 90° load there are two failure mechanisms: fiber fracture and failure of the matrix-fiber composite. At 0° load, there is mainly fiber fracture, whereas at 90° load, the failure is primarily a separation of the fibers from the matrix.…”
Section: -2mentioning
confidence: 99%
“…Different from the phenomenological approaches based upon the macroscopic level, the progressive model is needed to consider local damage mechanisms, such as fiber breakage, matrix deformation, interfacial debonding, etc (Kabir et al, 2006) and predict the dominant failure modes. This method seems to be more accurate but computationally complicated because it accounts for many failure mechanisms and is also related to damage accumulation correlated with material properties degradation.…”
Section: Introductionmentioning
confidence: 99%