A reliable progressive fatigue damage model for life prediction of composite laminates incorporating an adaptive cyclic jump algorithm

Journal Article (2022)
Author(s)

T. Zheng (TU Delft - Structural Integrity & Composites, Harbin Institute of Technology)

Licheng Guo (Harbin Institute of Technology)

Zhenxin Wang (AECC Commercial Aircraft Engine Co., Ltd)

Benedictus Benedictus (TU Delft - Structural Integrity & Composites)

John- Alan Pascoe (TU Delft - Structural Integrity & Composites)

Research Group
Structural Integrity & Composites
Copyright
© 2022 T. Zheng, Licheng Guo, Zhenxin Wang, R. Benedictus, J.A. Pascoe
DOI related publication
https://doi.org/10.1016/j.compscitech.2022.109587
More Info
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Publication Year
2022
Language
English
Copyright
© 2022 T. Zheng, Licheng Guo, Zhenxin Wang, R. Benedictus, J.A. Pascoe
Research Group
Structural Integrity & Composites
Bibliographical Note
Green Open Access added to TU Delft Institutional Repository 'You share, we take care!' - Taverne project https://www.openaccess.nl/en/you-share-we-take-care Otherwise as indicated in the copyright section: the publisher is the copyright holder of this work and the author uses the Dutch legislation to make this work public.@en
Volume number
227
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Abstract

In this paper, a reliable progressive fatigue damage model (PFDM) for predicting the fatigue life of composite laminates is proposed by combining the normalized fatigue life model, nonlinear residual degradation models and fatigue-improved Puck criterion. To balance the accuracy of life predictions and computational efficiency, an adaptive cyclic jump algorithm is developed and implemented within the PFDM. The sensitivity of life prediction to cyclic jump parameter has been greatly reduced by correlating the cyclic jump with the increment time and viscous coefficient. Therefore, the cyclic jump parameter can be arbitrarily selected within a relatively large range to obtain convergent results. When incorporating the adaptive cyclic jump algorithm, there is no need to define a standard for determining the material failure in numerical calculations, which effectively eliminates an artificially induced uncertainty in life predictions. Two sets of experiments are conducted to validate the proposed PFDM. The numerical predictions including static failure strength and fatigue life correlate reasonably well with the available experimental data.

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