The Effect of Inclusion Size and Distribution on Fatigue of 2024-T4 Aluminum.

Abstract

Two experiments were performed to determine the effect of inclusion size and distribution on the fatigue strength of 2024 aluminum. Rolled, 2024 Al sheet was shown to contain about twice as many inclusions larger than 10 microns in diameter in the center plane as at the surface. Bending fatigue tests, in which a zero to maximum tensile stress was applied to one surface of a flat specimen cut from the sheet, showed that when the center plane was made the tensile surface, the fatigue life was reduced to half that obtained with the original surface under tension. An experimental 2024 alloy was made from high purity constituents so that the number of inclusions larger than 10 microns was reduced by a factor of 10 over the commercial alloy. Comparative S/N curves were generated which showed that the fatigue strength of the experimental alloy was increased by 20% in the high amplitude load range and 10% in the low amplitude range. Fatigue lives were increased by a factor of 5. One sample was observed periodically during a test and it was established that crack initiation did not occur at the inclusions as it does in the commercial alloy. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1969
Accession Number
AD0856763

Entities

People

  • D. K. Benson
  • G. G. Shaw
  • J. C. Grosskreutz

Organizations

  • MRIGlobal

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aluminum
  • Amplitude
  • Diameters
  • Fatigue (Mechanics)
  • Fatigue Life
  • Fatigue Tests (Mechanics)
  • Inclusions
  • Mechanical Properties
  • Physical Properties
  • Stresses
  • Tensile Stress

Fields of Study

  • Materials science

Readers

  • Metallurgy
  • Structural Health Monitoring of Composite Structures.