Fiber Reinforced Plastics/Composites ›› 2016, Vol. 0 ›› Issue (9): 5-11.

• BASIC STUDY •     Next Articles

EXPERIMENTAL STUDY ON DEFORMATION AND FAILURE OF COMPOSITE MATERIAL BONDING INTERFACE UNDER CYCLIC LOADING

YANG Zhi, LU Bo-yuan, LV Zhi-hui, LI Zhi-yuan*   

  1. Non-destructive Testing Laboratory, Hebei University, Baoding 071002, China
  • Received:2016-04-01 Online:2016-09-28 Published:2016-09-28

Abstract: Researches on damage deformation and evolution behavior of adhesively bonded composite joints in real-time are of great importance for structural safety and its reliability assessment in service. In this paper, we use of Digital Image Correlation (DIC) and Acoustic Emission (AE) as complementary techniques for studying interfacial damage, deformation and failure behavior of adhesive-bonded composite single-lap joints under cyclic tension. On the basis of the average tensile failure load value, cyclic tensile tests were conducted with 70% and 80% of quasi-static failure loading, respectively. According to the damage deformation field, strain field information, and AE signals originated from damage of adhesive-bonded composite single-lap joints at different stages, the relationships between the mechanical failure mechanism of composite single-lap joints and the corresponding real-time deformation and AE signals were analyzed. The results show that the real-time micro-displacement field, AE relative energy, cumulative hits and amplitude spectra obtained from damage and failure of adhesive-bonded composite single-lap joints are connected with the initiation and propagation behavior of microcracks at adhesive interfaces. As the stress levels increase, the number of loading cycles that the joints can sustain before failure decreases.

Key words: cyclic loading, composite adhesive joints, acoustic emission, digital image correlation, damage evolution

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