論文

2021年4月

Mechanical properties and failure mode of thin-ply fiber metal laminates under out-of-plane loading

Composites Part A: Applied Science and Manufacturing
  • Kohei Yamada
  • ,
  • Benedikt Kötter
  • ,
  • Masaaki Nishikawa
  • ,
  • Shuto Fukudome
  • ,
  • Naoki Matsuda
  • ,
  • Kazumasa Kawabe
  • ,
  • Bodo Fiedler
  • ,
  • Masaki Hojo

143
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研究論文(学術雑誌)
DOI
10.1016/j.compositesa.2020.106267

© 2020 In this study, fiber metal laminates (FMLs), which consisted of thin-ply prepreg and stainless steel layers with a ply thickness of 0.04 mm, were fabricated with the aim of suppressing the fiber breakage that decreases the compression-after-impact (CAI) strength. Then, static flexural tests of FMLs were conducted to investigate the effects of the number of metal layers on the failure mode and mechanical properties during static out-of-plane loading, and the results were compared with those of our previous impact and CAI tests. The results confirmed that the plastic deformation of metal layers improved the energy dissipation and thus failure occurred in a limited range of locations. Furthermore, the investigation of the in situ stress during flexural tests by finite element method (FEM) analysis revealed that a hybrid material that both suppresses ply failure and has a high modulus of the metal can be realized owing to the constraining effect of thin-ply laminates.

リンク情報
DOI
https://doi.org/10.1016/j.compositesa.2020.106267
Scopus
https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=85101033817&origin=inward
Scopus Citedby
https://www.scopus.com/inward/citedby.uri?partnerID=HzOxMe3b&scp=85101033817&origin=inward
ID情報
  • DOI : 10.1016/j.compositesa.2020.106267
  • ISSN : 1359-835X
  • SCOPUS ID : 85101033817

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