Mechanism Based Failure Laws for Graphite/Epoxy Composites

Abstract

A significant progress has been made towards achieving the overall goal of developing mechanism-based failure laws for graphite/epoxy laminate under biaxial compression. Microstructural-level mechanisms have been largely uncovered using examination of load-interrupted specimens, including the strength data under different materials axes orientations and in-plane biaxiality ratios. Mechanism-based failure laws for uniaxial compression have also been developed, including a fracture mechanics-based predictive crack density model. New and unusual size effects related to modulus were uncovered, and so were the observations that seem to indicate fiver microbuckling mechanism to be simply end loading related.

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Document Details

Document Type
Technical Report
Publication Date
Jul 31, 1998
Accession Number
ADA397678

Entities

People

  • Vijay Gupta

Organizations

  • University of California, Los Angeles

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aspect Ratio
  • Composite Materials
  • Compression
  • Delamination
  • Epoxy Composites
  • Epoxy Laminates
  • Failure Mode And Effect Analysis
  • Fracture (Mechanics)
  • Graphitic Materials
  • Laminates
  • Law
  • Materials
  • Materials Science
  • Mechanical Working
  • Mechanics
  • Micromechanics
  • Orientation (Direction)

Readers

  • Reinforced Composite Materials
  • Structural Health Monitoring of Composite Structures.