2023 Boeing IRAD Testing: Difference between revisions

Revision as of 14:56, 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: 7075-T6 Spike Overload Test

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 |'''Data that is made available:'''
-*“[https://residualstress.org/images/8/86/IndividualP11_-_forERSI.xlsx individualP11 - forERSI.xlsx]” = digitized markers along with the numerical solutions for specimen marked PE-1-1
+*7075-T6 Spike Overload Test
-*“[https://residualstress.org/images/5/5d/IndividualP12_-_forERSI.xlsx individualP12 - forERSI.xlsx]” = digitized markers along with the numerical solutions for specimen marked PE-1-2
-*“[https://residualstress.org/images/1/13/IndividualP31_-_forERSI.xlsx individualP31 - forERSI.xlsx]” = digitized markers along with the numerical solutions for specimen marked PE-3-1
-*“[https://residualstress.org/images/6/62/IndividualP22_-_forERSI.xlsx individualP22 - forERSI.xlsx]” = digitized markers along with the numerical solutions for specimen marked PE-2-2
-|-
-|'''Reference'''
-* [https://residualstress.org/images/1/15/LoghinHarter_PVP2023-101256_v4.pdf Adrian Loghin, James Harter, Validation of Fatigue Crack Growth Modeling Solutions using Measurements Collected on API X65 Piping Specimens, PVP2023-101256, ASME PVP Proceedings, 2023.]
-* Reference for the experimental measurements used in the validation: Li, Z, Jiang, X., Hopman, H, Liu, Z., An investigation on the circumferential surface crack growth in steel pipes subjected to fatigue bending, Theoretical and Applied Fracture Mechanics, pp. 205, 2020.
 |}