Programmed Load Fatigue Tests on Notched and Welded Specimens of Al-Zn-Mg Alloys

Abstract

The report describes constant amplitude and programmed load fatigue tests on notched and welded specimens in two high strength aluminium-zinc- magnesium alloys. It is shown that, with very few exceptions, the hypothesis that sigma(n/N) = 1 consistently underestimates life. For the notched specimens using the basic quadratic programme sigma(n/N) varied from 0.8 to 14.8. For welded specimens using the same programme the value of sigma(n/N) varied much less and was approximately 2.6 to 7.0 for pulsating tension loading. Changes in the order of application of programme blocks had a negligible effect on the values of sigma(n/N) obtained. However, both for half tensile and for alternating loading, lower values of sigma(n/N) were obtained. When a spectrum parallel to the constant amplitude S-N curve was used high values of sigma(n/N) were obtained, except when the lowest stresses in the programme were omitted. This fact led to the belief that a possible reason for the high values of SIGMA(n/N) is coaxing at the lowest stress levels in the programme.

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Document Details

Document Type
Technical Report
Publication Date
Mar 31, 1970
Accession Number
AD0870058

Entities

People

  • J. D. Harrison
  • T. R. Gurney

Tags

Communities of Interest

  • C4I

DTIC Thesaurus Topics

  • Alloys
  • Aluminum Alloys
  • Crack Propagation
  • Cracks
  • Cycles
  • Electron Microscopes
  • Fatigue Life
  • Fatigue Tests (Mechanics)
  • Magnesium Alloys
  • Materials
  • Mechanical Properties
  • Mechanics
  • Residual Stress
  • Stresses
  • Structural Components
  • Tensile Strength
  • Welded Joints

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  • Materials Science and Engineering.