Ballistic Damage of Graphite-Epoxy Plates.

Abstract

Thin eight-ply laminated graphite-epoxy plates of a representative lay-up (0/+ or - 45 deg/0)s were damaged ballistically. The extent of damage varied with impact velocity and impactor mass. Visual and microscopic inspection was augmented by x-ray inspection utilizing a radio-opaque dye, to evaluate the extent of damage area. Specimens were then tested in tension to failure, to evaluate the residual strength. Damage length (in the 0 degree direction) varied with impact velocity, the greatest damage resulting from the lower velocities. Damage width (in the 90 deg direction) was not greatly affected by velocity changes. Variation of impactor mass had little effect. Residual strength as measured by tensile tests in the 0 deg direction was insensitive to damage size effects. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1977
Accession Number
ADA042296

Entities

People

  • George Arthur Eaton

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Biocomposites
  • Composite Materials
  • Delamination
  • Graphitic Materials
  • Inspection
  • Laminates
  • Materials
  • Materials Laboratories
  • Materials Testing
  • Military Aircraft
  • Residuals
  • Sequences
  • Test Beds
  • United States
  • United States Naval Academy
  • X Rays

Readers

  • Mathematics or Statistics
  • Structural Health Monitoring of Composite Structures.