2015
DOI: 10.1007/s11012-015-0214-0
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Damage initialization techniques for non-sequential FE propagation analysis of delaminations in composite aerospace structures

Abstract: The experimental effort required to develop, damage tolerant, aerospace composite structures could be significantly reduced if reliable numerical simulations were used to perform engineering studies of complex damaged structures. Finite element (FE) simulations of impact damaged structures typically follow a sequential approach that require large computational resources to reproduce complex damage scenarios. A numerical tool capable to reconstruct such scenarios using data from previous impact simulations or N… Show more

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Cited by 9 publications
(5 citation statements)
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“…A viscosity parameter improves the stability of a model during progressive delamination, but an inappropriate value may significantly change the results and cause them to differ from reality. Its value in the paper was selected based on several recent publications, including Panettieri et al [49], Abdulla et al [50], Zoghbi [51] and Demir et al [52]. In the cited works, the coefficient was assumed in a wide range χ = 0.00001÷0.002.…”
Section: Principles For Fe Modelling Of Adhesively Bonded Jointsmentioning
confidence: 99%
“…A viscosity parameter improves the stability of a model during progressive delamination, but an inappropriate value may significantly change the results and cause them to differ from reality. Its value in the paper was selected based on several recent publications, including Panettieri et al [49], Abdulla et al [50], Zoghbi [51] and Demir et al [52]. In the cited works, the coefficient was assumed in a wide range χ = 0.00001÷0.002.…”
Section: Principles For Fe Modelling Of Adhesively Bonded Jointsmentioning
confidence: 99%
“…The presence of defects into the fiber-matrix inter-phase is introduce into the models using an ad hoc technique developed by the authors [17]. The proposed method is based on the ABAQUS subroutine SDVINI, which can be invoked before the first increment of the simulations in order to define the initial values of internal state variables (STATEV) present into the user defined material subroutines (UMAT).…”
Section: Inter-phase Damage Injection Techniquementioning
confidence: 99%
“…If one want to address the influence of fiber-matrix interphase defects on the mechanical properties of an unidirectional Carbon/Epoxy material, the last point is critical and has not yet been addressed in the literature. The paper presents a possible approach based on user tailored cohesive elements, that model the fiber-matrix interface, whose damage can be initialized through an original technique developed by the authors for meso-scale analyses [17].…”
Section: Introductionmentioning
confidence: 99%
“…Cohesive elements have been proved to be an excellent approach in computational fracture mechanics. Nevertheless, massively parallel computations are required to capture damage patterns and evolution meticulously in composites [17]. The concept of CZM is to show the material separation between crack faces as a fracture [18].…”
Section: Introductionmentioning
confidence: 99%