Evaluation of Size Effect on the Fatigue Properties of Aluminum Alloys 7075, 7079 and X7080

Abstract

The first phase of an evaluation to determine the size effect on the fatigue properties of 7075-T651, 7079-T651 aluminum alloy stretcher leveled plates and an X7080 aluminum alloy hand forging has been completed. Evaluation of the large section specimens (4 square inches test section) showed that the fatigue strength of the X7080 aluminum alloy hand forging, 40,000 p.s.i. at 1, 000,000 cycles, was approximately 48% and 60% higher than the fatigue strengths of 27,000 p.s.i. and 25,000 p.s.i. for the 7075 and 7079 alloy stretcher leveled plates, respectively. The notched fatigue strength of the X7080 alloy, 14,000 p. s.i. at 1,000,000 cycles, was approximately 17% higher than the notched fatigue strength of 12,000 p.s.i. for the 7075 and 7079 alloys.

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Document Details

Document Type
Technical Report
Publication Date
Feb 24, 1970
Accession Number
AD0866333

Entities

People

  • Joseph Viglione
  • M. L. Stellabotte

Organizations

  • Naval Air Warfare Center Warminster

Tags

DTIC Thesaurus Topics

  • Alloys
  • Aluminum
  • Aluminum Alloys
  • Crack Propagation
  • Cracks
  • Department Of Defense
  • Dynamic Loads
  • Fatigue Tests (Mechanics)
  • Grain Boundaries
  • Materials
  • Microstructure
  • Notch Sensitivity
  • Precipitation
  • Stress Concentration
  • Stresses
  • Stretchers
  • Test And Evaluation

Fields of Study

  • Materials science

Readers

  • Mathematics or Statistics
  • Metallurgy