2015
DOI: 10.1016/j.compstruct.2015.06.007
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Effective anisotropic stiffness of inclusions with debonded interface for Eshelby-based models

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Cited by 40 publications
(26 citation statements)
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“…Each fiber is represented by an ellipsoidal inclusion with its own aspect ratio, orientation and volume. We have demonstrated that this algorithm correctly calculates the homogenized elastic properties of the composite and that the stresses in fibers [31] and on the fiber-matrix interface [32] are calculated with an acceptable accuracy. We also have proven that for typical random fiber composites the degree of asymmetry of the stiffness tensor predicted with Mori-Tanaka method is limited and simple symmetrisation of the stiffness tensor provides an acceptable correction [33].…”
Section: Micromechanical Modellingmentioning
confidence: 99%
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“…Each fiber is represented by an ellipsoidal inclusion with its own aspect ratio, orientation and volume. We have demonstrated that this algorithm correctly calculates the homogenized elastic properties of the composite and that the stresses in fibers [31] and on the fiber-matrix interface [32] are calculated with an acceptable accuracy. We also have proven that for typical random fiber composites the degree of asymmetry of the stiffness tensor predicted with Mori-Tanaka method is limited and simple symmetrisation of the stiffness tensor provides an acceptable correction [33].…”
Section: Micromechanical Modellingmentioning
confidence: 99%
“…While for the other types of loading, simple stress redistribution rules have been developed. Expressions for the stress distribution for an inclusion with debonded interface scheme are presented in table 1, detailed derivations and FE validation of the proposed "EqBI" can be found in [32].…”
Section: Micromechanical Modellingmentioning
confidence: 99%
“…Using a combination of the Mori-Tanaka formulation [16] and an algorithm for treating fiber matrix debonding [17], this method predicts the local SN curve with only one SN curve as input. The approach was named the Master SN curve approach, in short the MSNC approach.…”
Section: *Manuscript Click Here To View Linked Referencesmentioning
confidence: 99%
“…It is known that the first mode of damage in SFRCs is fiber matrix debonding. There are multiple methods to calculate the onset of debonding, for example the Modified Coulomb criteria [22]. It can be shown that the stress at which onset of debonding occurs is much lower than the expected stress to failure for a SFRCs after a million cycles of loading.…”
Section: Theory and Formulation Of The Master Sn Curve Approachmentioning
confidence: 99%
“…In the proposed MSNC approach, the first cycle of loading is modelled by using the full MT formulation, which is chosen based on its predictive abilities for stresses in individual inclusions [24] and the degree of asymmetry in the predicted stiffness tensor is also rather limited when the MT formulation is applied to SFRCs [25]. Non-linear stress strain behavior of SFRCs during the first cycle of loading is modelled by accounting for fiber-matrix debonding and matrix non-linearity, which is described below.…”
Section: Theory and Formulation Of The Master Sn Curve Approachmentioning
confidence: 99%