Analytical Modeling of Composite-to-Composite (Scarf) Joints in Tension and Compression

Abstract

Fracture mechanics-based multi-level computational modeling and simulation techniques were developed to predict failure strengths of composite scarf joints under tension or compression. Global, local, and element level models were used in the study to calculate the energy release rates at the scarf joints. The study showed that explicit modeling of the resin layer at the scarf joint, where cracks initiate, was important for accurate prediction of the joint failure strengths. In addition, the consideration of the joint interface slope in the fracture model was important especially for compressive joint failure strengths. In terms of the mixed failure criteria for crack propagation, the interactive biquadratic criterion was found to be useful for reliable prediction of joint failure strengths. The predicted strengths were in good agreement with experimental data, which were obtained for two different kinds of polymer composites: e-glass/epoxy and carbon/epoxy.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 2007
Accession Number
ADA470122

Entities

People

  • Todd R. Greene

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Air Force
  • Carbon Fibers
  • Composite Materials
  • Experimental Data
  • Failure Mode And Effect Analysis
  • Fracture (Mechanics)
  • Geometry
  • Laminates
  • Material Degradation Processes
  • Materials
  • Materials Laboratories
  • Materials Processing
  • Materials Science
  • Materials Testing
  • Mechanics
  • Polymer Matrix Composites
  • Reinforced Plastics

Readers

  • Structural Health Monitoring of Composite Structures.