Fatigue Life Prediction under Variable Cyclic Loading Based on Statistical Linear Cumulative Damage Rule for CFRP Laminates-Reference-Cited by-同舟云学术

Fatigue Life Prediction under Variable Cyclic Loading Based on Statistical Linear Cumulative Damage Rule for CFRP Laminates

Published:2007-05 Issue:7 Volume:26 Page:665-680
ISSN:0731-6844
Container-title:Journal of Reinforced Plastics and Composites
language:en
Short-container-title:Journal of Reinforced Plastics and Composites

Author:

Noda Junji¹,Nakada Masayuki²,Miyano Yasushi²

Affiliation:

1. Materials System Research Laboratory Kanazawa Institute of Technology 3-1 Yatsukaho, Hakusan, Ishikawa, 924-0838, Japan, -it.ac.jp

2. Materials System Research Laboratory Kanazawa Institute of Technology 3-1 Yatsukaho, Hakusan, Ishikawa, 924-0838, Japan

Abstract

This paper is concerned with the applicability of the statistical linear cumulative damage (SLCD) rule for predicting the fatigue life under variable cyclic loading for CFRP laminates. The three-point bending fatigue tests for plain-woven and quasi-isotropic CFRP laminates were carried out under various cyclic loadings with constant and variable load amplitude and frequency. As a result, the applicability of SLCD rule to the flexural fatigue life of these CFRP laminates was confirmed for the cases of variable frequency as well as variable amplitude from the viewpoint of statistics.

Publisher

SAGE Publications

Subject

Materials Chemistry,Polymers and Plastics,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Link

http://journals.sagepub.com/doi/pdf/10.1177/0731684407075577

Reference19 articles.

1. Analysis of viscoelastic laminated composite plates

2. Loading Rate and Temperature Dependence on Flexural Fatigue Behavior of a Satin Woven CFRP Laminate

3. Role of matrix resin on the flexural static behavior of unidirectional pitch-based carbon fiber laminates

4. Influence of Stress Ratio on Fatigue Behavior in the Transverse Direction of Unidirectional CFRPS

5. Prediction of Flexural Fatigue Strength of CRFP Composites under Arbitrary Frequency, Stress Ratio and Temperature

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