Fracture Graphite Fiber Reinforced Composites.

Abstract

The fracture of thin, prenotched graphite/ epoxy laminates is studied analytically and experimentally. The analytical portion of the study is concentrated on a three- dimensional finite element analysis of the crack problem in anisotropic laminates featuring a two-stage solution employing a hybrid model multilayered element. The case of a four ply (45 degree/-45 degree/-45 degree/45) laminate is analyzed, and results are presented for the distribution of in- plane stresses and interlaminar shear stresses about a sharp crack tip. A two- dimensional analysis is also employed to provide K-calibrations for fracture specimens used in the experimental program. Experiments are performed to investigate the applicability of classical fracture mechanics, the characteristics of crack tip damage during loading, and the final modes of crack propagation for representative ply configurations of graphite/epoxy laminates. The development of the subcritical zone into a final catastrophic fracture mode is also described. (Author, modified-PL)

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1973
Accession Number
AD0775729

Entities

People

  • Frederick J. Mcgarry
  • John F. Mandell
  • Su-su Wang

Organizations

  • Massachusetts Institute of Technology

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Composite Materials
  • Crack Propagation
  • Crack Tips
  • Cracks
  • Epoxy Laminates
  • Fiber Reinforced Composites
  • Finite Element Analysis
  • Fracture (Mechanics)
  • Graphitic Materials
  • Laminates
  • Mechanics
  • Micromechanics
  • Shear Stresses
  • Three Dimensional
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Materials Science (Mechanical Engineering).
  • Structural Dynamics.