Analysis of Local Stress Ratio for Delamination in Composites Under Fatigue Loads

Journal Article (2020)
Author(s)

A. Raimondo (TU Delft - Aerospace Structures & Computational Mechanics)

C. Bisagni (TU Delft - Aerospace Structures & Computational Mechanics)

Research Group
Aerospace Structures & Computational Mechanics
Copyright
© 2020 A. Raimondo, C. Bisagni
DOI related publication
https://doi.org/10.2514/1.J058465
More Info
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Publication Year
2020
Language
English
Copyright
© 2020 A. Raimondo, C. Bisagni
Research Group
Aerospace Structures & Computational Mechanics
Issue number
1
Volume number
58
Pages (from-to)
455-463
Reuse Rights

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Abstract

An approach based on the cohesive zone model for analyzing delamination in composite laminates under cyclic fatigue loading is presented. The proposed technique, called “min-max load approach,” is able to dynamically capture the local stress ratio during the progression of delamination. The possibility to know the local stress ratio is relevant in all the situations where its value is different from the applied load ratio and cannot be determined a priori. The methodology analyzes in a single finite element analysis two identical models with two different constant loads, the minimum and the maximum load of the fatigue cycle. The two models interact with each other, exchanging information to calculate the crack growth rate. At first, the approach has been validated in simulations of mode I and mixed-mode propagation using double cantilever beam and mixed-mode bending tests. Then, to prove the effectiveness of the developed methodology, a modified version of the mixed-mode bending test has been analyzed. Mode I and mode II components of the load are decoupled and applied independently, resulting in a local stress ratio different from the applied load ratio. The results obtained from the simulations, compared with the analytical model obtained using the corrected beam theory, show that the proposed approach is able to predict the local stress ratio and thereby to correctly evaluate the crack growth rate during the propagation of the damage.

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