Analysis of Interface Cracks in Adhesively Bonded Lap Shear Joints. Part 4.

Abstract

The conservation laws of elasticity for nonhomogeneous materials developed under this grant are used to study the crack behavior in adhesively bonded lap shear joints. These laws and the fundamental relationships in fracture mechanics of interface cracks, the problem is reduced to a pair of linear algebraic equations, and stress intensity solutions can be determined directly by information extracted from the far field. The numerical results obtained show that: (1) in the lap-shear joint with a given adherend, the opening-mode stress intensity factor (K sub I) is always larger than that of the shearing-mode (K sub II); (2) K sub I is not sensitive to adherent thickness but K sub II increases rapidly with increasing thickness; and (3) K sub I and K sub II increase simultaneously as the interfacial crack length increases. (MM)

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1981
Accession Number
ADA302678

Entities

People

  • J. F. Yau
  • S. S. Wang

Organizations

  • University of Illinois Urbana–Champaign

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  • Air Platforms
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  • Weapons Technologies

DTIC Thesaurus Topics

  • Aeronautics
  • Air Force
  • Aircrafts
  • Composite Materials
  • Crack Tips
  • Elastic Properties
  • Engineering
  • Failure Mode And Effect Analysis
  • Far Field
  • Finite Element Analysis
  • Fracture (Mechanics)
  • J Integrals
  • Jet Propulsion
  • Materials
  • Materials Laboratories
  • Mechanics
  • Navy

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  • Atmospheric Science / Meteorology, specifically Wind Wave Turbulence.
  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)
  • Surface Coatings Technology.

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