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A proposal for similitude in characterizing fatigue delamination behavior with fibre bridging of carbon-fibre reinforced polymer composites

  • Liaojun Yao*
  • , Mingyue Chuai
  • , Zhangming Lyu
  • , Xiangming Chen
  • , Licheng Guo
  • , R. C. Alderliesten
  • *Corresponding author for this work
  • Aircraft Strength Research Institute
  • Harbin Institute of Technology
  • Delft University of Technology

Research output: Contribution to journalArticlepeer-review

Abstract

Methods based on fracture mechanics have been widely used in fatigue delamination growth (FDG) characterization of composite laminates. These methods are based on the similitude hypothesis. It is therefore important to have appropriate parameters to well represent the similitude, which is useful for fatigue delamination test standard development aimed by Technical Committee 4 of the European Structural Integrity Society (ESIS TC4) and the ISO/TC61/SC13. In the present study, discussions on similitude parameters for fibre-bridged fatigue delamination interpretation have been conducted via fatigue data with fibre bridging at different R-ratios. The results clearly demonstrate that the strain energy release rate (SERR) indeed applied around the crack front, rather than the total applied SERR, should be employed to represent the similitude for FDG interpretation with large-scale fibre bridging. Particularly, the use of Δ√Gtip can well determine fibre-bridged delamination behavior of a given R-ratio, but it is not valid for FDG at different R-ratios in accordance with the similitude principles. A new similitude parameter, in terms of both Δ√Gtip and the maximum SERR Gmax_tip, was therefore proposed to appropriately represent FDG behavior with fibre bridging at different R-ratios. This study can not only provide database, but also give important insights for the development of mode I fatigue delamination test standard of composite laminates.

Original languageEnglish
Article number109756
JournalEngineering Fracture Mechanics
Volume295
DOIs
StatePublished - 23 Jan 2024

Keywords

  • Composite laminates
  • Fatigue delamination
  • Fibre bridging
  • Similitude
  • Stress ratio

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