The behavior of cracked cross-ply composite laminates under shear loading

C. L. Tsai*, I. M. Daniel

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

46 Scopus citations

Abstract

An interlaminar-shear-stress analysis developed earlier by Tsai et al. (1990, Micro-cracking-Induced Damage in Composites) for a [φmn], bi-directional composite laminate is used to solve the case of a cross-ply [0m/90n]x laminate with the 90° layer only or both layers cracked under pure shear loading. Strains, forces and laminate shear modulus reduction due to matrix cracking were obtained. Experimental results for shear modulus as a function of crack densities were obtained by a simple shear test and they agree very well with the theoretical prediction.

Original languageEnglish (US)
Pages (from-to)3251-3267
Number of pages17
JournalInternational Journal of Solids and Structures
Volume29
Issue number24
DOIs
StatePublished - 1992

ASJC Scopus subject areas

  • Modeling and Simulation
  • Materials Science(all)
  • Condensed Matter Physics
  • Mechanics of Materials
  • Mechanical Engineering
  • Applied Mathematics

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