Test and Analysis of Composite Hat Stringer Pull-off Test Specimens

Abstract

Hat stringer pull-off tests were performed to evaluate the delamination failure mechanisms in the flange region for a rod-reinforced hat stringer section. A special test fixture was used to pull the hat off the stringer while reacting the pull-off load through roller supports at both stringer flanges. Microscopic examinations of the failed specimens revealed that failure occurred at the ply termination in the flange area where the flange of the stiffener is built up by adding 45/-45 tape plies on the top surface. Test results indicated that the as-manufactured microstructure in the flange region has a strong influence on the delamination initiation and the associated pull-off loads. Finite element models were created for each specimen with a detailed mesh based on micrographs of the critical location. A fracture mechanics approach and a mixed mode delamination criterion were used to predict the onset of delamination and the pull-off load. By modeling the critical local details of each specimen from micrographs, the model was able to accurately predict the hat stringer pull-off loads and replicate the variability in the test results.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1996
Accession Number
AD1043129

Entities

People

  • Carl Q. Rousseau
  • Jian Li
  • T. K. O'brien

Organizations

  • United States Army Research Laboratory

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Composite Materials
  • Composite Structures
  • Delamination
  • Engineering
  • Epoxy Composites
  • Equations
  • Failure Mode And Effect Analysis
  • Finite Element Analysis
  • Fracture (Mechanics)
  • Geometry
  • Graphitic Materials
  • Materials
  • Mechanics
  • Micromechanics
  • Microstructure
  • Military Research
  • Test Fixtures

Readers

  • Structural Dynamics.
  • Structural Health Monitoring of Composite Structures.
  • Surface Coatings Technology.