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Evaluation of damage accumulation zone in the vicinity of the crack tip: FEM analysis via UMAT procedure
Nowadays the damage and failure of the material are of critical interest to designers of engineering structures, especially in aircraft and spacecraft industry. As there is a lack of methods for accurate failure prediction and damage analysis. Especially for early stages of the design process, a qui...
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Published in: | Journal of physics. Conference series 2018-12, Vol.1096 (1), p.12157 |
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Main Authors: | , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
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Summary: | Nowadays the damage and failure of the material are of critical interest to designers of engineering structures, especially in aircraft and spacecraft industry. As there is a lack of methods for accurate failure prediction and damage analysis. Especially for early stages of the design process, a quick way of estimating material behavior is needed. There is a need for a material model coupled with a damage evolution law. In the paper a damage model, based on continuum damage mechanics, is presented. The material law is implemented computationally as a user defined subroutine (UMAT) in a commercially available FEM package Simulia Abaqus. The active damage accumulation zones in the vicinity of the crack tip for a wide class of cracked specimens are analyzed. Distribution of each damage component is given. |
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ISSN: | 1742-6588 1742-6596 |
DOI: | 10.1088/1742-6596/1096/1/012157 |