Peridynamics for fatigue life and residual strength prediction of composite laminates

Y. L. Hu, Erdogan Madenci

Research output: Contribution to journalArticle

21 Citations (Scopus)

Abstract

This study presents an application of peridynamics to predict damage initiation and growth in fiber reinforced composites under cyclic loading. The fatigue model utilizes standard S-N fatigue data for a lamina along with the critical energy release rate values. The fidelity of this model is established by simulating the tests conducted by the Air Force Research Laboratory under the Tech Scout Project. As part of this project, the AFRL tested open-hole composite laminates made of IM7/977-3 for three different layups under cyclic loads for strength and failure progression. The peridynamic predictions agree with the reduction in stiffness and strength as a function of number of load cycles. Also, the progressive damage predictions capture the general characteristics of the experimentally observed damage patterns.

Original languageEnglish (US)
Pages (from-to)169-184
Number of pages16
JournalComposite Structures
Volume160
DOIs
StatePublished - Jan 15 2017

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Laminates
Fatigue of materials
Cyclic loads
Energy release rate
Composite materials
Research laboratories
Stiffness
Fibers
Air

Keywords

  • Composites
  • Failure
  • Fatigue
  • Peridynamics
  • Progressive

ASJC Scopus subject areas

  • Ceramics and Composites
  • Civil and Structural Engineering

Cite this

Peridynamics for fatigue life and residual strength prediction of composite laminates. / Hu, Y. L.; Madenci, Erdogan.

In: Composite Structures, Vol. 160, 15.01.2017, p. 169-184.

Research output: Contribution to journalArticle

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