An Investigation of Residual Stress Characterization of 7075-T6 Aluminum for Application in Fatigue Analysis

Abstract

Residual stresses induced by a stress concentration have been shown to increase the fatigue life of materials. An experimental investigation was undertaken to establish a relationship which would allow for the prediction of local residual stresses at a notch from known geometrical stress concentration factors and applied loads. Notched flat plate specimens were tested utilizing photoelastic coatings for measurement of stress concentration factors and residual stresses. Handbook values for stress concentration factors were found to be accurate within seven percent for the geometrics tested. The residual stress characterization consisted of a plot of nominal stress versus residual stress. These plots predicted residual stresses to within ten percent of the measured values for typical flight load histories.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1978
Accession Number
ADA067580

Entities

People

  • Gary L. Stuart

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Aluminum
  • Cyclic Tests
  • Fatigue Life
  • Fatigue Tests (Mechanics)
  • Flight Loads
  • Gages
  • Geometry
  • Materials
  • Measurement
  • Mechanics
  • Modulus Of Elasticity
  • Residual Stress
  • Strain Gages
  • Stress Concentration
  • Stress Strain Relations
  • Stresses

Readers

  • Materials Science and Engineering.
  • Structural Dynamics.