The Effect of Stress Ratio During Crack Propagation and Fatigue for 2024-T3 and 7075-T6 Aluminum

  • K Walker
    Physical Sciences Laboratory, Lockheed-California Company 1 Senior Research Scientist , , P.O. Box 551, Burbank, Calif.91503 .

書誌事項

公開日
1970-01-01
DOI
  • 10.1520/stp32032s
公開者
ASTM International100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959

説明

<jats:p>An effective stress, σ¯ = σmax1-mΔσm where m is assumed to be a material constant, is shown to predict the effect of stress ratio on crack propagation and fatigue life for two aluminum alloys. Simple approximations of notch stress and strain using Neuber's notch rule are introduced to extend the predictions of stress-ratio effects to inelastic notch behavior.</jats:p>

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