From Engineered Residual Stress Implementation (ERSI)
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| |'''Point of Contact:''' ''Moises Ocasio''
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| |'''Description:''' A spike overload test was conducted on 7075-T6 to improve the understanding of crack growth rate constraint-loss behavior as a function of thickness and finite width effects.
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| |'''Data that is made available:'''
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| *[https://residualstress.org/images/0/0e/7075T6_SpikeOverload_Boeing_IRAD_Test.xlsx 7075-T6 Spike Overload Test]
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| |}
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| |'''Point of Contact:''' ''Moises Ocasio''
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| |'''Description:''' A hole shakedown test was conducted on Ti-6l-4V LS to validate methods and best practices used to handle local yielding at holes due to extreme loads.
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| |'''Data that is made available:'''
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| *[https://residualstress.org/images/d/de/Ti64_Boeing_IRAD_Shakedown_Test.xlsx Ti-6Al-4V Hole Shakedown Test]
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| |}
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| |'''Point of Contact:''' ''Moises Ocasio''
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| |'''Description:''' A hole shakedown test was conducted on Ph13-8Mo LS to validate methods and best practices used to handle local yielding at holes due to extreme loads.
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| |'''Data that is made available:'''
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| *[https://residualstress.org/images/d/de/Ph13-8Mo_Boeing_IRAD_Shakedown_Test.xlsx Ph13-8Mo Hole Shakedown Test]
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| |}
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Revision as of 03:28, 14 July 2026
