Detachment of an Elastic Matrix from a Rigid Spherical Inclusion.

Abstract

An approximate theoretical treatment is given for detachment of an elastomer from a rigid spherical inclusion by a tensile stress applied to the elastomeric matrix. The inclusion is assumed to have an initially-debonded patch on its surface and the conditions for growth of the patch are derived from fracture energy considerations. Catastrophic debonding is predicted to occur at a critical applied stress when the initial debond is small. The strain energy dissipated as result of this detachment, and hence the mechanical hysteresis, are also evaluated. When a reasonable value is adopted for Young's modulus (E) of the elastomeric matrix, it is found that detachment from small inclusions, of less than abut 0.1 mm in diameter, will not occur, even when the level of adhesion is relatively low. Instead, rupture of the matrix near the inclusion becomes the preferred mode of failure at an applied stress given approximately by E/2. For still smaller inclusions, of less than about 1 micrometer in diameter, rupture of the matrix becomes increasingly difficult, due to the increasing importance of a surface energy term. These considerations account for the general features of reinforcement of elastomers.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1980
Accession Number
ADA087414

Entities

People

  • Alan Neville Gent

Organizations

  • University of Akron

Tags

Communities of Interest

  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Atmospheric Sciences
  • Civil Engineering
  • Composite Materials
  • Engineering
  • Materials
  • Mechanics
  • Military Research
  • Modulus Of Elasticity
  • Particle Size
  • Particles
  • Space Sciences
  • Surface Energy
  • Tensile Stress
  • United States
  • Weapons

Readers

  • Fluid Dynamics.
  • Materials Science (Mechanical Engineering).
  • Surface Coatings Technology.