Metallurgical Control of Fatigue Crack Growth in High-Strength Aluminum Alloys

Abstract

The results of 22 different investigations of cyclic crack growth, principally on the 2024-T3 and 7075-T6 alloys, but including results for unalloyed and other 2-, 5-, 6-, and 7-thousand series alloys, were examined and compiled with a view to separating metallurgical effects from other factors. The various crack growth measurements show good agreement when the comparisons involve the same R-value, environment and cyclic frequency. Both the 2024-T3 and 7075-T6 alloy can display widely different rates of Both the 2024-T3 and 7075-T6 alloy can display widely different rates of growth for the same delta K-value. Crack growth rate-delta K measurements have also been converted into S-N curves for cracked members. These curves illustrate the influence of flaw size, stress range, R and K sub c on the cyclic life of the 7075-T6 and 2024-T3 grades.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1972
Accession Number
AD0745989

Entities

People

  • G. T. Hahn
  • R. Simon

Organizations

  • Battelle Memorial Institute

Tags

Communities of Interest

  • Air Platforms
  • Counter IED
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Agreements
  • Air Force
  • Alloys
  • Aluminum Alloys
  • Chemistry
  • Corrosion
  • Crystal Structure
  • Fracture (Mechanics)
  • Frequency
  • Grain Size
  • Materials
  • Materials Laboratories
  • Measurement
  • Mechanics
  • Metals
  • Sensitivity
  • Yield Strength

Readers

  • Materials Science (Mechanical Engineering).
  • Metallurgy
  • Systems Analysis and Design