A progessive damage fatigue model for unidirectional laminated composites based on finite element analysis

The simulation of the fatigue damage of laminated composites under multi-axial and variable amplitude loadings has to deal with several new challenges and several methods of damage modelling. In this paper we present how to account for the complex loading by using the damage hysteresis operator app...

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Main Authors: Michael Hack, D. Carrella-Payan, B. Magneville, T. Naito, Y. Urushiyama, W. Yamazaki, T. Yokozeki, W. Van Paepegem
Format: Article
Language:English
Published: Gruppo Italiano Frattura 2018-09-01
Series:Frattura ed Integrità Strutturale
Subjects:
Online Access:https://www.fracturae.com/index.php/fis/article/view/2017
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spelling doaj-39d2981a5ed84ae4809525e60751bb632021-01-27T17:14:39ZengGruppo Italiano FratturaFrattura ed Integrità Strutturale1971-89932018-09-011246A progessive damage fatigue model for unidirectional laminated composites based on finite element analysisMichael Hack0D. Carrella-Payan1B. Magneville2T. Naito3Y. Urushiyama4W. Yamazaki5T. Yokozeki6W. Van Paepegem7Siemens PLM SoftwareSiemens PLM Software, GermanySiemens PLM Software, GermanyHonda R&D Co Ltd, Tochigi, JapanHonda R&D Co Ltd, Tochigi, JapanUniversity of Tokyo, JapanUniversity of Tokyo, JapanGhent University, Belgium The simulation of the fatigue damage of laminated composites under multi-axial and variable amplitude loadings has to deal with several new challenges and several methods of damage modelling. In this paper we present how to account for the complex loading by using the damage hysteresis operator approach for fatigue. It is applied to a fatigue model for intra-laminar damage based on stiffness degradation laws from Van Paepegem and has been extended to deal with unidirectional carbon fibres. The parameter identification method is presented here and parameter sensitivities are discussed. The initial static damage of the material is accounted for by using the Ladevèze damage model and the permanent shear strain accumulation based on Van Paepegem’s formulation. This approach has been implemented into commercial software. The intra-laminar fatigue damage model combines efficient methods with a low number of tests to identify the parameters of the stiffness degradation law, this overall procedure for fatigue life prediction is demonstrated to be cost efficient at industrial level. https://www.fracturae.com/index.php/fis/article/view/2017CompositeFatigueVariable AmplitudeStiffness degradation
collection DOAJ
language English
format Article
sources DOAJ
author Michael Hack
D. Carrella-Payan
B. Magneville
T. Naito
Y. Urushiyama
W. Yamazaki
T. Yokozeki
W. Van Paepegem
spellingShingle Michael Hack
D. Carrella-Payan
B. Magneville
T. Naito
Y. Urushiyama
W. Yamazaki
T. Yokozeki
W. Van Paepegem
A progessive damage fatigue model for unidirectional laminated composites based on finite element analysis
Frattura ed Integrità Strutturale
Composite
Fatigue
Variable Amplitude
Stiffness degradation
author_facet Michael Hack
D. Carrella-Payan
B. Magneville
T. Naito
Y. Urushiyama
W. Yamazaki
T. Yokozeki
W. Van Paepegem
author_sort Michael Hack
title A progessive damage fatigue model for unidirectional laminated composites based on finite element analysis
title_short A progessive damage fatigue model for unidirectional laminated composites based on finite element analysis
title_full A progessive damage fatigue model for unidirectional laminated composites based on finite element analysis
title_fullStr A progessive damage fatigue model for unidirectional laminated composites based on finite element analysis
title_full_unstemmed A progessive damage fatigue model for unidirectional laminated composites based on finite element analysis
title_sort progessive damage fatigue model for unidirectional laminated composites based on finite element analysis
publisher Gruppo Italiano Frattura
series Frattura ed Integrità Strutturale
issn 1971-8993
publishDate 2018-09-01
description The simulation of the fatigue damage of laminated composites under multi-axial and variable amplitude loadings has to deal with several new challenges and several methods of damage modelling. In this paper we present how to account for the complex loading by using the damage hysteresis operator approach for fatigue. It is applied to a fatigue model for intra-laminar damage based on stiffness degradation laws from Van Paepegem and has been extended to deal with unidirectional carbon fibres. The parameter identification method is presented here and parameter sensitivities are discussed. The initial static damage of the material is accounted for by using the Ladevèze damage model and the permanent shear strain accumulation based on Van Paepegem’s formulation. This approach has been implemented into commercial software. The intra-laminar fatigue damage model combines efficient methods with a low number of tests to identify the parameters of the stiffness degradation law, this overall procedure for fatigue life prediction is demonstrated to be cost efficient at industrial level.
topic Composite
Fatigue
Variable Amplitude
Stiffness degradation
url https://www.fracturae.com/index.php/fis/article/view/2017
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