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EFFECT OF STRESS RATIO ON FATIGUE-CRACK GROWTH IN 7075-T-6 AND 2024-T-3 ALUMINUM-ALLOY SPECIMENS [NASA TN D-5390]

By: Hudson, C. Michael.
Material type: materialTypeLabelBookSeries: National Aeronautics and Space Administration ; Nasa Technical Note. Publisher: Washington, D.C. National Aeronautics and Space Administration 1969Description: 29p.Subject(s): Stress ratio
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