Analysis of the Effect of Matrix Degradation on Fatigue Behavior of a Graphite/Epoxy Laminate.

Abstract

An analytical study of the effect of fatigue on a + OR - 45/90 SUB 2sub s graphite/epoxy laminate is conducted considering two levels of damage. The first one is microscopic damage, which is viewed as a matrix softening mechanism that is accounted for by the use of micromechanics. The second level of damage is delamination. An evaluation of lamination theory versus a finite element elasticity solution which accounts for free edge stresses is made first. Lamination theory is found to be inadequate due to its inability to account for large amounts of shear deformation as the matrix degrades. Experimental data are used to evaluate the matrix degradation as a function of fatigue cycles, and then a parametric study of the strain energy release rate as a function of delamination size at various degrees of matrix degradation is conducted. For a constant maximum stress fatigue test, the matrix degradation leads to an increase in strain energy which is predicted to eventually cause rapid delamination. Reasonably good agreement between theory and experimental data on the + OR - 45/9O sub 2sub s laminate is demonstrated. (MM)

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1982
Accession Number
ADA305263

Entities

People

  • Robert T. Arenburg

Organizations

  • Texas A&M University

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Aspect Ratio
  • Composite Materials
  • Elastic Materials
  • Engineering
  • Epoxy Laminates
  • Failure Mode And Effect Analysis
  • Finite Element Analysis
  • Geometry
  • Laminates
  • Materials
  • Mechanics
  • Micromechanics
  • Modulus Of Elasticity
  • Shear Modulus
  • Tensile Strength
  • Thermal Expansion

Fields of Study

  • Physics

Readers

  • Structural Health Monitoring of Composite Structures.