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Interlaminar fatigue growth under thermal cycles in composite laminate

  • Stony Brook University
  • Oklahoma State University

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

1 Scopus citations

Abstract

A fatigue growth of fiber-reinforced composite laminate was characterized under a combined experimental and computational investigation. Here, 24-ply composites with pre-existing delamination were subjected to thermal cycles. During two month long test period, the crack growths were regularly monitored under variable amplitude. The measured data was used to determine the relationship between the temperature and growth rate. After completion of the test, inspections of fractured surfaces showed uneven growth with greater propagations near free surfaces. Due to such a behavior, 3D finite element analyses were performed to obtain energy release rate and mixed-mode stress intensity factors. The variations of these parameters were consistent with the observed crack front. The measured crack growth rates were also correlated with energy release rate to show good fit with the Paris law. The results are useful in understanding delamination growth under thermal cycles and estimating the threshold temperature to drive the growth.

Original languageEnglish
Title of host publicationProceedings of the 16th International Conference on Composite Materials, ICCM-16 - "A Giant Step Towards Environmental Awareness
Subtitle of host publicationFrom Green Composites to Aerospace"
PublisherInternational Committee on Composite Materials
ISBN (Print)9784931136052
StatePublished - 2007

Publication series

NameICCM International Conferences on Composite Materials

Keywords

  • 3D FEM
  • Energy release rate
  • Interlaminar fatigue crack
  • Mixed-mode fracture

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