An estimate of the residual stress distr
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J.F. Williams; D.C. Stouffer
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Article
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1979
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Elsevier Science
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English
⚖ 784 KB
Experiments have been performed on a series of 2024-T351 Aluminum alloy uniaxiaf, tension specimens loaded under R = 0 conditions to grow a low cycle fatigue crack to a predetermined length. One half of the specimens were given a 33% single pulse overload at the conclusion of the test. All specimens