Fatigue life prediction of composite structures based on online stiffness monitoring

Author:

Zong Junda1,Yao Weixing12

Affiliation:

1. Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle, Nanjing University of Aeronautics and Astronautics, Nanjing, Jiangsu, China

2. State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing, Jiangsu, China

Abstract

This article presents an online statistical life prediction method based on both historical and local residual-stiffness information to reduce the effect of dispersive mechanical properties of fiber-reinforced plastic structures. Normalized residual-stiffness curves obtained from the laboratory are used as a benchmark, and the model parameters are assumed to be independent random variables. According to Bayesian statistical theory, the prior distribution of fatigue life is updated by the residual-stiffness sample information of the in-service structure through online monitoring; then, a more accurate life estimation is obtained. This method precisely captures the essence of stiffness degradation of a composite structure. The individual dispersion effect is largely eliminated through using the local stiffness data. In general, a more accurate life estimation can be obtained if more sample information is available. The test results of glass-fiber-reinforced plastic and carbon-fiber-reinforced plastic laminates show that the fatigue life can be accurately predicted with only the first 20% residual-stiffness data known.

Funder

Cheung Kong Scholars and Innovation Team Development Plan

National Natural Science Foundation of China

Publisher

SAGE Publications

Subject

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

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