Delamination Growth Behavior in Cross-Ply Laminated Composites Due to Transverse Concentrated Loading

Abstract

An analytical model was developed to study the delamination growth behavior of graphite/epoxy cross-ply laminated composites resulting from quasi- static transverse concentrated loads. The objective of the study was to fundamentally understand the interaction between the initial matrix cracking and the delamination initiation and growth in laminated composites due to transverse concentrated loads. During this period of the investigation, attention is given to the growth of the surface matrix crack-induced delamination in cross-ply composites and the interaction between the matrix cracking and the delimination initiation and propagation inside the laminates. Based on the study, it shows that delamination growth in laminated composites due to transverse loads is strongly affected by the initial matrix cracks. Delamination induced by a bending crack (surface) would grow into a slender shape with its major axis parallel to the direction of the surface cracks. Mode I fracture toughness dominates the initiation and growth of the delamination induced by the bending cracks. Also, bending crack-induced delamination is stable in laminated composites.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1992
Accession Number
ADA255974

Entities

People

  • Fu-Kuo Chang
  • Sheng Liu

Organizations

  • Stanford University

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aeronautics
  • Applied Mechanics
  • Astronautics
  • Composite Materials
  • Delamination
  • Engineering
  • Epoxy Laminates
  • Failure Mode And Effect Analysis
  • Fiber Reinforced Composites
  • Finite Element Analysis
  • Graphitic Materials
  • Laminates
  • Materials
  • Mechanics
  • Three Dimensional
  • Toughness
  • Universities

Fields of Study

  • Materials science

Readers

  • Structural Health Monitoring of Composite Structures.