Cracked components under anti-plane loading: recent outcomes and future developments

The existence of three-dimensional effects at cracks has been known for many years, but understanding has been limited, and for some situations still is. Understanding improved when the existence of corner point singularities and their implications became known. Increasingly powerful computers made...

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Main Author: F. Berto
Format: Article
Language:English
Published: Gruppo Italiano Frattura 2017-07-01
Series:Fracture and Structural Integrity
Subjects:
Online Access:http://www.gruppofrattura.it/pdf/rivista/numero41/numero_41_art_59.pdf
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author F. Berto
author_facet F. Berto
author_sort F. Berto
collection DOAJ
description The existence of three-dimensional effects at cracks has been known for many years, but understanding has been limited, and for some situations still is. Understanding improved when the existence of corner point singularities and their implications became known. Increasingly powerful computers made it possible to investigate three-dimensional effects numerically in detail. Despite increased understanding, three-dimensional effects are sometimes ignored in situations where they may be important. The purpose of the present investigation is to study by means of accurate 3D finite element (FE) models a coupled fracture mode generated by anti-plane loading of a straight through-the-thickness crack in linear elastic plates. An extended version of the present work has recently been published in the literature. The results obtained from the highly accurate finite element analyses have improved understanding of the behaviour of through cracked components under anti-plane loading. The influence of plate bending is increasingly important as the thickness decreases. It appears that a new field parameter, probably a singularity, is needed to describe the stresses at the free surfaces. Discussion on whether KIII tends to zero or infinity as a corner point is approached is futile because KIII is meaningless at a corner point. The intensity of the local stress and strain state through the thickness of the cracked components has been evaluated by using the strain energy density (SED) averaged over a control volume embracing the crack tip. The SED has been considered as a parameter able to control fracture in some previous contributions and can easily take into account also coupled three-dimensional effects. Calculation of the SED shows that the position of the maximum SED is independent of plate thickness. Both for thin plates and for thick ones the maximum SED is close to the lateral surface, where the maximum intensity of the coupled mode II takes place.
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1971-8993
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publishDate 2017-07-01
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spelling doaj-art-b87a0fe09f82482fa56bab18c5c7984a2025-02-03T00:45:47ZengGruppo Italiano FratturaFracture and Structural Integrity1971-89931971-89932017-07-01114147548310.3221/IGF-ESIS.41.59Cracked components under anti-plane loading: recent outcomes and future developmentsF. Berto0 University of Science and Technology, NorwayThe existence of three-dimensional effects at cracks has been known for many years, but understanding has been limited, and for some situations still is. Understanding improved when the existence of corner point singularities and their implications became known. Increasingly powerful computers made it possible to investigate three-dimensional effects numerically in detail. Despite increased understanding, three-dimensional effects are sometimes ignored in situations where they may be important. The purpose of the present investigation is to study by means of accurate 3D finite element (FE) models a coupled fracture mode generated by anti-plane loading of a straight through-the-thickness crack in linear elastic plates. An extended version of the present work has recently been published in the literature. The results obtained from the highly accurate finite element analyses have improved understanding of the behaviour of through cracked components under anti-plane loading. The influence of plate bending is increasingly important as the thickness decreases. It appears that a new field parameter, probably a singularity, is needed to describe the stresses at the free surfaces. Discussion on whether KIII tends to zero or infinity as a corner point is approached is futile because KIII is meaningless at a corner point. The intensity of the local stress and strain state through the thickness of the cracked components has been evaluated by using the strain energy density (SED) averaged over a control volume embracing the crack tip. The SED has been considered as a parameter able to control fracture in some previous contributions and can easily take into account also coupled three-dimensional effects. Calculation of the SED shows that the position of the maximum SED is independent of plate thickness. Both for thin plates and for thick ones the maximum SED is close to the lateral surface, where the maximum intensity of the coupled mode II takes place.http://www.gruppofrattura.it/pdf/rivista/numero41/numero_41_art_59.pdfFracture mechanicsFinite element analysisAnti-plane loadingStress intensity factorCorner point effects
spellingShingle F. Berto
Cracked components under anti-plane loading: recent outcomes and future developments
Fracture and Structural Integrity
Fracture mechanics
Finite element analysis
Anti-plane loading
Stress intensity factor
Corner point effects
title Cracked components under anti-plane loading: recent outcomes and future developments
title_full Cracked components under anti-plane loading: recent outcomes and future developments
title_fullStr Cracked components under anti-plane loading: recent outcomes and future developments
title_full_unstemmed Cracked components under anti-plane loading: recent outcomes and future developments
title_short Cracked components under anti-plane loading: recent outcomes and future developments
title_sort cracked components under anti plane loading recent outcomes and future developments
topic Fracture mechanics
Finite element analysis
Anti-plane loading
Stress intensity factor
Corner point effects
url http://www.gruppofrattura.it/pdf/rivista/numero41/numero_41_art_59.pdf
work_keys_str_mv AT fberto crackedcomponentsunderantiplaneloadingrecentoutcomesandfuturedevelopments