2021
DOI: 10.3390/aerospace9010017
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Stress Intensity Factors for a Non-Circular Hole with Inclusion Layer Embedded in a Cracked Matrix

Abstract: The failure analysis of a non-circular hole with an inclusion layer embedded in an infinite cracked matrix under a remote in-plane uniform load is presented. In this study, a series solution of stress functions for both the matrix and inclusion layer is obtained using the complex variable theory in conjunction with the method of conformal mapping. The stress intensity factor (SIF) can then be determined numerically by solving the singular integral equation (SIE) for the interaction among different crack sites,… Show more

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Cited by 3 publications
(1 citation statement)
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“…In the theoretical model limitation, an "equiangular polygon" is investigated for realizing irregularly shaped inclusion. This composite system, including irregular holes, coating layers, and matrix has been discussed under different conditions [29][30][31][32][33]. However, the previous [21,22], and (d) macrostructure of the hole, iron oxide, and steel matrix [28].…”
Section: Introductionmentioning
confidence: 99%
“…In the theoretical model limitation, an "equiangular polygon" is investigated for realizing irregularly shaped inclusion. This composite system, including irregular holes, coating layers, and matrix has been discussed under different conditions [29][30][31][32][33]. However, the previous [21,22], and (d) macrostructure of the hole, iron oxide, and steel matrix [28].…”
Section: Introductionmentioning
confidence: 99%