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7075-T6 and 2024-T351 Aluminum Alloy Fatigue Crack Growth

Description: 2024-T351 Aluminum Data The 2024-T351 material was provided by the Southwest Research Institute machined into specimens. No additional fabrication was performed by NASA Langley. Thirty-two middle tension and sixty compact tension specimens were machined from a single 1.2 meter wide by 2.4 meter long by 9.525 millimeter thick sheet. The

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