2005
DOI: 10.1080/15376490500259202
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An Efficient Continuum Damage Model and its Application to Shear Deformable Laminated Plates

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Cited by 22 publications
(21 citation statements)
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“…For a complete description of the damage model development and its numerical implementation, the reader is referred to Robbins et al [31].…”
Section: Materials Non-linearity-continuum Damage Mechanicsmentioning
confidence: 99%
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“…For a complete description of the damage model development and its numerical implementation, the reader is referred to Robbins et al [31].…”
Section: Materials Non-linearity-continuum Damage Mechanicsmentioning
confidence: 99%
“…Finally, J 11 , J 22 , J 33 , and 0 are material constants that control the damage resistance characteristics of the material. To facilitate their implementation into displacement-based finite element models, the damage evolution equations are expressed in strain-based form where increments in the damage eigenvalues are expressed in terms of imposed strain increments via invoking the principle of maximum dissipation [31]. The resulting damage evolution equations can be expressed in matrix form as follows:…”
Section: Materials Non-linearity-continuum Damage Mechanicsmentioning
confidence: 99%
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“…For completeness sake, the development of the 3-D damage model is fully described in this paper and shares many similarities with the developments found in Barbero and De Vivo (2001) and Lee et al (1985). The numerical implementation of this particular damage model is described in detail by Robbins et al (2005) and Robbins and Reddy (2006).…”
Section: Objectives and Methodsmentioning
confidence: 99%
“…Lonetti et al (2003) used the triaxial damage model in conjunction with 3-D finite elements that each span the entire thickness of the laminate thus encompassing all of the material layers in a single element. Robbins et al (2005) discussed the numerical treatment of 3-D continuum damage mechanics within the context of a macroscopic finite element model based on the first order shear deformation theory of laminates. The authors studied the effect of various modeling parameters on predicted damage evolution and global failure.…”
Section: Introductionmentioning
confidence: 99%