Energy Absorption of Graphite/Epoxy Plates Using Hopkinson Bar Impact

Abstract

This work summarizes the analytical and experimental study on the energy absorption of quasi-isotropic graphite/ epoxy composite plates due to the impacting hemispherical penetrator in a Hopkinson bar apparatus. The mechanics of stress wave propagation through the bar and the composite laminate plate are discussed to predict the phenomenological process involved. The experimental data provided the results in terms of force, velocity, and energy of impact at all times during the penetration process occurring in microseconds. It has been been concluded that loss of contact occurs frequently during the penetration process due to the stress wave reflections back and forth in the thickness direction. The damage process seemed to be both velocity and temperature dependent. Below a certain transition velocity the laminate absorbs less energy at low temperature than at high temperature. The reverse is true above this transition velocity. The mechanism of failure tends to change with impact velocity in such a way that progressively less energy is absorbed at higher velocities.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1991
Accession Number
ADA244256

Entities

People

  • David Hui
  • Magna R. Altamirano
  • Piyush K. Dutta

Organizations

  • Cold Regions Research and Engineering Laboratory

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Absorption
  • Air Force
  • Cold Regions
  • Composite Materials
  • Engineering
  • Epoxy Composites
  • Failure Mode And Effect Analysis
  • Graphitic Materials
  • Laminates
  • Low Temperature
  • Materials
  • Materials Science
  • Mechanics
  • Micromechanics
  • Modulus Of Elasticity
  • Wave Propagation
  • Waves

Fields of Study

  • Materials science

Readers

  • Explosive Engineering.
  • Mechanical Engineering/Mechanics of Materials.
  • Structural Health Monitoring of Composite Structures.