Damage development during flexural fatigue of carbon fibre-reinforced PEEK

G. Dillon, M. Buggy

Research output: Contribution to journalArticlepeer-review

17 Scopus citations

Abstract

Fatigue damage growth mechanisms in [0]16 and [0, 90]4s laminates of APC-2 subjected to three-point flexure were studied using scanning electron microscopy. Building on an understanding gained from the study of statically tested samples, specific fatigue mechanisms were identified. For each laminate geometry a coherent progression of damage build-up is proposed.

Original languageEnglish (US)
Pages (from-to)355-370
Number of pages16
JournalComposites
Volume26
Issue number5
DOIs
StatePublished - May 1995

All Science Journal Classification (ASJC) codes

  • Materials Science(all)

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