2025 A10 CX Dataset and Round Robin: Difference between revisions
From Engineered Residual Stress Implementation (ERSI)
Jump to navigationJump to search
No edit summary |
No edit summary |
||
| Line 6: | Line 6: | ||
|- | |- | ||
|'''Data that is made available:''' | |'''Data that is made available:''' | ||
* | |||
*[https://residualstress.org/images/0/0e/7075T6_SpikeOverload_Boeing_IRAD_Test.xlsx 7075-T6 Spike Overload Test] | *[https://residualstress.org/images/0/0e/7075T6_SpikeOverload_Boeing_IRAD_Test.xlsx 7075-T6 Spike Overload Test] | ||
|} | |} | ||
Revision as of 00:55, 21 July 2026
| Point of Contact: Bob Pilarczyk |
| Description: •The A-10 program is transitioning toward using residual stresses from cold expansion directly in damage tolerance analyses. A test program was developed to target and isolate the load history and residual stress effects for Cx holes. Fatigue tests include baseline non-Cx and Cx holes, constant amplitude and spectrum loading, and are complimented with residual stress measurements for each condition. |
| Data that is made available: |
