The Fatigue Response’s Fingerprint of Composite Materials Subjected to Constant and Variable Amplitude Loadings

Author:

D’Amore Alberto1ORCID,Grassia Luigi1

Affiliation:

1. Department of Engineering, Università della Campania “Luigi Vanvitelli”, Via Roma 19, 81031 Aversa, Italy

Abstract

This paper discusses the theoretical and experimental correlations between fatigue and static strength statistical distributions. We use a two-parameter residual strength model that obeys the qualitative strength-life equal rank assumption (SLERA) for guidance. The modeling approach consists of recovering the model’s parameters by best fitting the constant amplitude (CA) fatigue data at a given stress ratio, R, and the experimental Weibull parameters of the static strength distribution function. An extensive set of fatigue life and residual strength data for AS4 carbon/epoxy 3k/E7K8 Plain Weave Fabric with [45/−45/90/45/−45/45/−45/0/45/−45]S layups, obtained at different stress ratios, R, have been analyzed. The modeling approach consists of recovering the model’s parameters from pure tension or compression fatigue data at R = 0.1 and R = 5, respectively. Once the parameters are fixed, the model’s capabilities, potential, and limits are discussed by comparing its predictions with residual strength and fatigue life data obtained at stress ratios with mixed tension/compression loadings, namely R = −0,2 and R = −1. Moreover, from a preliminary analysis, the theoretical extension of the model’s capabilities to variable amplitude loadings is conceptualized. The application of Miner’s rule is also discussed and compared with a new damage rule to analyze the fatigue responses under variable amplitude loadings.

Publisher

MDPI AG

Subject

Engineering (miscellaneous),Ceramics and Composites

Reference20 articles.

1. (2023, April 01). DOT/FAA/AR-10/6. Determining the Fatigue Life of Composites Aircraft Structures Using Life and Load-Enhancement Factors, Available online: http://www.tc.faa.gov/its/worldpac/techrpt/ar10-6.pdf.

2. Numerical evaluation of structural relaxation-induced stresses in amorphous polymers;Caputo;Compos. Part A Appl. Sci. Manuf.,2006

3. The Critical Element Model: A modeling philosophy;Reifsnider;Eng. Fract. Mech.,1986

4. Reifsneider, K.L. (1990). Fatigue of Composite Materials, Elsevier Publishing.

5. Progressive fatigue damage modelling of composite materials. Part I: Modeling;Shokrieh;J. Compos. Mater.,2000

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