Compressive strength of unidirectional composites: Measurement and prediction

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

The present work examines the effect of resin ductility (varied as a function of temperature) on the compressive strength of unidirectional T800/924C carbon fibre-epoxy laminates. Tests are conducted in a screw-driven machine between room temperature and 100°C. Untabbed straight-sided specimens are used in a modified Celanese test rig; conventional serrated grip faces of the Celanese jig are replaced by spark-eroded inserts to eliminate adhesively bonded tabs on the specimen ends and minimize gripping region failures. Test results show that at approximately 80°C the failure mode switches from in-plane to out-of-plane fibre microbuckling. As the test temperature increases, the shear strength/stiffness of the resin is considerably reduced; this decreases the amount of side support for the fibres and reduces the strain level at which fibre buckling occurs. Recent fracture models are used to predict the compressive strength of the T800/924C system; agreement between theory and experiment is acceptable.
Original languageEnglish
Title of host publicationComposite Materials
Subtitle of host publicationTesting and Design, Thirteenth Volume
EditorsSteven J. Hooper
Place of PublicationWest Conshohocken
PublisherASTM International
Pages168-176
Number of pages9
Volume13
ISBN (Print)9780803124783
DOIs
Publication statusPublished - 1 Jan 1997

Publication series

NameASTM Special Technical Publication
PublisherASTM
Volume1242

Keywords

  • Carbon fibre composite
  • Compressive strength
  • Failure analysis
  • Fibre microbuckling
  • Fibre misalignment
  • Shear properties
  • Temperature effects

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