Special Hybrid Stress Finite Elements for the Analysis of Interface Stress Distribution in Adhesive Joints

Abstract

The widespread application of adhesively bonded joints has necessitated the development of methodology to predict ultimate static joint strength and service life under cyclic loading. Due to the complexity of mathematically modelling adhesive joint response, analytical treatments are limited to highly idealized joint configurations, simplified assumed stress states, applied loading and material behavior. To overcome these limitations, a specialized finite element-based numerical approach is investigated wherein special 2-D and 3-D layered finite elements are formulated to improve the computational efficiency and accuracy of determining stresses in adhesive joints. The hybrid stress technique is used to explicitly enforce stress equilibrium throughout the element domain and stress continuity conditions at layer interfaces. The emphasis of this research is to explore a variety of possible element configurations to assess element performance. The optimum 2-D and 3-D element formulations demonstrate improved performance compared to standard displacement-based finite elements in predicting joint stresses.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1994
Accession Number
ADA281612

Entities

People

  • Erik Saether
  • Kristen Weight

Organizations

  • United States Army Research Laboratory

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Adhesives
  • Air Force
  • Aspect Ratio
  • Bonded Joints
  • Continuity
  • Displacement
  • Finite Element Analysis
  • Geometry
  • Joints
  • Materials
  • Materials Science
  • Military Research
  • Shear Stresses
  • Standards
  • Three Dimensional
  • Two Dimensional

Fields of Study

  • Engineering

Readers

  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)
  • Structural Health Monitoring of Composite Structures.