Effect of Matrix Resin on the Impact Fracture Characteristics of Graphite-Epoxy Laminates.

Abstract

This report presents the results of an investigation into the effect of resin chemistry on basic impact-energy-absorbent mechanisms exhibited by graphite-epoxy composites. Impact fracture modes and microscopic resin deformation characteristics were examined for 26 NASA-impacted graphite-epoxy laminates with different resin chemistries. Discrete specimen fracture modes were identified through cross-sectional examination after impact and subsequently compared with measured glass transition temperatures, cure cycles, and residual impact capabilities. Details of microscopic resin deformation mechanisms and their overall relationship to impact loading conditions, voids, and resin content also were characterized through detailed scanning electron microscopic examination of separated fracture surfaces. (MM)

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1982
Accession Number
ADA305801

Entities

People

  • A. G. Miller
  • B. W. Smith
  • P. E. Hertzberg

Organizations

  • Boeing

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircraft Industry
  • Aircrafts
  • Chemistry
  • Commercial Aircraft
  • Composite Materials
  • Crack Propagation
  • Epoxy Composites
  • Epoxy Laminates
  • Failure Mode And Effect Analysis
  • Glass Transition Temperature
  • Laminates
  • Materials
  • Materials Processing
  • Materials Science
  • Plastic Flow
  • Resins
  • Transition Temperature

Fields of Study

  • Materials science

Readers

  • Materials Science and Engineering.
  • Reinforced Composite Materials

Technology Areas

  • Microelectronics