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Stanley, David Joseph
This work was undertaken as a comparative study on fatigue properties of a typical third generation Aluminum-Lithium alloy, AA2198-T8, to that of a traditional aerospace aluminum-copper alloy, AA2024-T3, with a focus on developing a methodology for r
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https://explore.openaire.eu/search/publication?articleId=doi_________::ff0c2ecc803578098c10e7af7a5a4288