2012
DOI: 10.1016/j.ijimpeng.2012.03.009
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Modelling of dynamic damage and failure in aluminium alloys

Abstract: a b s t r a c tA physically based damage and failure model, applicable to orthotropic metals is proposed in this paper. To account for the physical mechanisms of failure, the concept of thermally activated damage initially proposed by Klepaczko [1], has been adopted as the basis for the model. This assumption makes the proposed damage/failure model compatible with the Mechanical Threshold Strength (MTS) model [2e6], which was used within the overall constitutive model to describe material behaviour in the plas… Show more

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Cited by 19 publications
(10 citation statements)
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“…The Taylor impact test was applied to study the behavior of low-density open-cell aluminum foam at higher strain-rates [21,22]. A foam specimen was accelerated to the desired velocity by a gas gun and then impacted into a rigid wall.…”
Section: Methodsmentioning
confidence: 99%
“…The Taylor impact test was applied to study the behavior of low-density open-cell aluminum foam at higher strain-rates [21,22]. A foam specimen was accelerated to the desired velocity by a gas gun and then impacted into a rigid wall.…”
Section: Methodsmentioning
confidence: 99%
“…The damage effects are represented on the overall elastic and plastic mechanical behavior of the material by using a scalar or tensorial damage variables to depict the ductile defects initiation and growth and their consequences on the other mechanical fields. Various engineering problems have been conducted using this model (Betten, 1986; Brünig and Gerke, 2011; Brünig and Ricci, 2005; Chaboche, 1992, 1993; Kachanov, 1980; Lemaitre et al., 2000; Liu et al., 2017; Vignjevic et al., 2012a, 2012b; Voyiadjis et al., 2009 ).…”
Section: Coupled Elastoplastic Model With Damage Modelmentioning
confidence: 99%
“…To study the failure mechanisms of textile composites, the damage development and material properties of constituents must be better understood at the microscopic level of RUC. Therefore, a majority of damage models and failure analysis methods have been provided by many scholars in recent years (Campbell et al, 2006;Desrumaux et al, 2001;Huang, 2005;Okabe et al, 2001;Panov et al, 2006;Vignjevic et al, 2012a;Vignjevic et al, 2012b). When 3D textile composites are subjected to the external loading, damage and failure of constituents of tow and matrix within the composites may be happened.…”
Section: Critical Damage Area (Cda) Failure Theorymentioning
confidence: 99%