2023 Boeing IRAD Testing: Difference between revisions
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*7075-T6 Spike Overload Test | *[https://residualstress.org/images/0/0e/7075T6_SpikeOverload_Boeing_IRAD_Test.xlsx 7075-T6 Spike Overload Test] | ||
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|'''Data that is made available:''' | |'''Data that is made available:''' | ||
*Ti-6Al-4V Hole Shakedown Test | *[https://residualstress.org/images/d/de/Ti64_Boeing_IRAD_Shakedown_Test.xlsx Ti-6Al-4V Hole Shakedown Test] | ||
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|'''Data that is made available:''' | |'''Data that is made available:''' | ||
*Ph13-8Mo Hole Shakedown Test | *[https://residualstress.org/images/d/de/Ph13-8Mo_Boeing_IRAD_Shakedown_Test.xlsx Ph13-8Mo Hole Shakedown Test] | ||
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Latest revision as of 15:00, 7 August 2024
| Point of Contact: Moises Ocasio |
| 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. |
| Data that is made available: |
| Point of Contact: Moises Ocasio |
| 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. |
| Data that is made available: |
| Point of Contact: Moises Ocasio |
| 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. |
| Data that is made available: |
