Peridynamics for Failure and Residual Strength Prediction of Fiber-Reinforced Composites
Peridynamics is a reformulation of classical continuum mechanics that utilizes integral equations in place of partial differential equations to remove the difficulty in handling discontinuities, such as cracks or interfaces, within a body. Damage is included within the constitutive model; initiatio...
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ndltd-arizona.edu-oai-arizona.openrepository.com-10150-3113002015-10-23T05:29:36Z Peridynamics for Failure and Residual Strength Prediction of Fiber-Reinforced Composites Colavito, Kyle Wesley Madenci, Erdogan Madenci, Erdogan Guven, Ibrahim Missoum, Samy Wu, Xiaoyi Critical Stretch Fracture Peridynamics Mechanical Engineering Composites Peridynamics is a reformulation of classical continuum mechanics that utilizes integral equations in place of partial differential equations to remove the difficulty in handling discontinuities, such as cracks or interfaces, within a body. Damage is included within the constitutive model; initiation and propagation can occur without resorting to special crack growth criteria necessary in other commonly utilized approaches. Predicting damage and residual strengths of composite materials involves capturing complex, distinct and progressive failure modes. The peridynamic laminate theory correctly predicts the load redistribution in general laminate layups in the presence of complex failure modes through the use of multiple interaction types.This study presents two approaches to obtain the critical peridynamic failure parameters necessary to capture the residual strength of a composite structure. The validity of both approaches is first demonstrated by considering the residual strength of isotropic materials. The peridynamic theory is used to predict the crack growth and final failure load in both a diagonally loaded square plate with a center crack, as well as a four-point shear specimen subjected to asymmetric loading.This study also establishes the validity of each approach by considering composite laminate specimens in which each failure mode is isolated. Finally, the failure loads and final failure modes are predicted in a laminate with various hole diameters subjected to tensile and compressive loads. 2013 text Electronic Dissertation http://hdl.handle.net/10150/311300 en_US Copyright © is held by the author. Digital access to this material is made possible by the University Libraries, University of Arizona. Further transmission, reproduction or presentation (such as public display or performance) of protected items is prohibited except with permission of the author. The University of Arizona. |
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en_US |
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Critical Stretch Fracture Peridynamics Mechanical Engineering Composites |
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Critical Stretch Fracture Peridynamics Mechanical Engineering Composites Colavito, Kyle Wesley Peridynamics for Failure and Residual Strength Prediction of Fiber-Reinforced Composites |
description |
Peridynamics is a reformulation of classical continuum mechanics that utilizes integral equations in place of partial differential equations to remove the difficulty in handling discontinuities, such as cracks or interfaces, within a body. Damage is included within the constitutive model; initiation and propagation can occur without resorting to special crack growth criteria necessary in other commonly utilized approaches. Predicting damage and residual strengths of composite materials involves capturing complex, distinct and progressive failure modes. The peridynamic laminate theory correctly predicts the load redistribution in general laminate layups in the presence of complex failure modes through the use of multiple interaction types.This study presents two approaches to obtain the critical peridynamic failure parameters necessary to capture the residual strength of a composite structure. The validity of both approaches is first demonstrated by considering the residual strength of isotropic materials. The peridynamic theory is used to predict the crack growth and final failure load in both a diagonally loaded square plate with a center crack, as well as a four-point shear specimen subjected to asymmetric loading.This study also establishes the validity of each approach by considering composite laminate specimens in which each failure mode is isolated. Finally, the failure loads and final failure modes are predicted in a laminate with various hole diameters subjected to tensile and compressive loads. |
author2 |
Madenci, Erdogan |
author_facet |
Madenci, Erdogan Colavito, Kyle Wesley |
author |
Colavito, Kyle Wesley |
author_sort |
Colavito, Kyle Wesley |
title |
Peridynamics for Failure and Residual Strength Prediction of Fiber-Reinforced Composites |
title_short |
Peridynamics for Failure and Residual Strength Prediction of Fiber-Reinforced Composites |
title_full |
Peridynamics for Failure and Residual Strength Prediction of Fiber-Reinforced Composites |
title_fullStr |
Peridynamics for Failure and Residual Strength Prediction of Fiber-Reinforced Composites |
title_full_unstemmed |
Peridynamics for Failure and Residual Strength Prediction of Fiber-Reinforced Composites |
title_sort |
peridynamics for failure and residual strength prediction of fiber-reinforced composites |
publisher |
The University of Arizona. |
publishDate |
2013 |
url |
http://hdl.handle.net/10150/311300 |
work_keys_str_mv |
AT colavitokylewesley peridynamicsforfailureandresidualstrengthpredictionoffiberreinforcedcomposites |
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1718106411971379200 |