4.7 Article

Interlaminar failure behavior of GLARE laminates under short-beam three-point-bending load

期刊

COMPOSITES PART B-ENGINEERING
卷 97, 期 -, 页码 361-367

出版社

ELSEVIER SCI LTD
DOI: 10.1016/j.compositesb.2016.05.003

关键词

Hybrid; Laminates; Debonding; Mechanical testing

资金

  1. National Engineering and Research Center for Commercial Aircraft Manufacturing [SAMC 13-JS-15-032]
  2. Jiangsu Innovation Program for Graduate Education [KYLX_0259]
  3. Fundamental Research Funds for the Central Universities
  4. Opening Project of Jiangsu Key Laboratory of Advanced Structural Materials and Application Technology [ASMA201401]
  5. Priority Academic Program Development of Jiangsu Higher Education Institutions

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In this paper, interlaminar failure behavior of GLARE-3/2-0.3 laminates under short-beam three-point-bending load were investigated with various span length-to-specimen thickness ratios (L/h). Failure modes and damage characteristics at different loading stages were observed by Scanning Electron Microscopy (SEM) to assess the failure behavior. It was found that failure modes changed accordingly with varying L/h ratios. A valid shear dominant failure mode was obtained at the L/h ratio of 8. Moreover, there were significant differences in failure modes and damage characteristics among three GLARE variants. The results also showed that lay-up configuration of glass/epoxy layer strongly affected load-deflection response, especially the failure load, and corresponding failure mode. (C) 2016 Elsevier Ltd. All rights reserved.

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