Flexural fatigue of carbon fibre-reinforced PEEK laminates

M. Buggy, G. Dillon

Research output: Contribution to journalArticle

13 Scopus citations

Abstract

Stress/number of cycles to failure relations were established for unidirectional, cross-plied and angle-plied laminates of APC-2 using three-point bend flexure tests. Results for constant stress ratio fatigue tests were modelled using both Weibull and fatigue modulus degradation analyses. Behaviour was compared with that of an established carbon/epoxy system.

Original languageEnglish (US)
Pages (from-to)191-198
Number of pages8
JournalComposites
Volume22
Issue number3
DOIs
StatePublished - May 1991

All Science Journal Classification (ASJC) codes

  • Materials Science(all)

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