2023 Boeing IRAD Testing: Difference between revisions

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(Created page with "{| class="wikitable" style="width: 50%;" |- |'''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:''' *“[https://residualstress.org/images/8/86/IndividualP11_-_forERSI.xlsx individualP11 - forERSI.xlsx]” = digitized markers along with the numeric...")
 
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|'''Data that is made available:'''
|'''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
*[https://residualstress.org/images/0/0e/7075T6_SpikeOverload_Boeing_IRAD_Test.xlsx 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
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*“[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
{| class="wikitable" style="width: 50%;"
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|'''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.
|-
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|'''Reference'''
|'''Data that is made available:'''
*[https://residualstress.org/images/d/de/Ti64_Boeing_IRAD_Shakedown_Test.xlsx Ti-6Al-4V Hole Shakedown Test]
|}


* [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.]
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* 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.
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|'''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:'''
*[https://residualstress.org/images/d/de/Ph13-8Mo_Boeing_IRAD_Shakedown_Test.xlsx Ph13-8Mo Hole Shakedown Test]
|}
|}

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:
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