Combined Bearing and Bypass Loading on a Graphite/Epoxy Laminate.

Abstract

A combined experimental and analytical study was conducted to determine the behavior of a graphite/epoxy laminate subjected to combined bearing and bypass loading. Single-fastener quasi-isotropic specimens were loaded at various hearing-bypass ratios until damage was produced at the fastener hole. Damage-onset strengths and damage modes were then analyzed using local hole-boundary stresses calculated by a finite-element analysis. The tension data showed the expected linear interaction for combined bearing and bypass loading with damage developing in the net-section tension mode. However, the compression bearing-bypass strengths showed an unexpected interaction involving the bearing mode. Compressive bypass loads reduced the bearing strength by decreasing the bolt-hole contact arc and thus increasing the severity of the bearing loads. The bearing stresses at the hole boundary were not accurately estimated by superposition of the stress components for separate bearing and bypass loading. However, superposition produced reasonably accurate estimates for tangential stresses especially near the specimen net-section. (MM)

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1988
Accession Number
ADA301632

Entities

People

  • J. H. Crews Jr.
  • R. A. Naik

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Bearing Strength
  • Bolts
  • Composite Materials
  • Control Systems
  • Epoxy Composites
  • Epoxy Laminates
  • Failure Mode And Effect Analysis
  • Fasteners
  • Finite Element Analysis
  • Graphitic Materials
  • Laminates
  • Materials
  • Materials Testing
  • Peak Values
  • Stress Analysis
  • Stresses
  • Test Methods

Fields of Study

  • Engineering

Readers

  • Combustion and Flow Dynamics.
  • Structural Health Monitoring of Composite Structures.