2023 Boeing IRAD Testing
From Engineered Residual Stress Implementation (ERSI)
Revision as of 14:56, 7 August 2024 by Dallen-Andrew (talk | contribs)
| 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:
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