2023 Boeing IRAD Testing - Revision history

Dallen-Andrew at 19:00, 7 August 2024

2024-08-07T19:00:52Z

← Older revision		Revision as of 15:00, 7 August 2024
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	\|-		\|-
	\|'''Data that is made available:'''		\|'''Data that is made available:'''
	*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]
	\|}		\|}

Dallen-Andrew at 18:58, 7 August 2024

2024-08-07T18:58:02Z

← Older revision		Revision as of 14:58, 7 August 2024
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	\|'''Point of Contact:''' ''Moises Ocasio''		\|'''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~~.		\|'''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:'''		\|'''Data that is made available:'''
	*~~7075~~-~~T6 Spike Overload~~ Test		*Ti-6Al-4V Hole Shakedown Test
	\|}		\|}

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	\|'''Point of Contact:''' ''Moises Ocasio''		\|'''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~~.		\|'''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:'''		\|'''Data that is made available:'''
	*~~7075~~-~~T6 Spike Overload~~ Test		*Ph13-8Mo Hole Shakedown Test
	\|}		\|}

Dallen-Andrew at 18:56, 7 August 2024

2024-08-07T18:56:34Z

← Older revision		Revision as of 14:56, 7 August 2024
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			{\| 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:'''
			*7075-T6 Spike Overload Test
			\|}

			{\| 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:'''
			*7075-T6 Spike Overload Test
			\|}

	{\| class="wikitable" style="width: 50%;"		{\| class="wikitable" style="width: 50%;"
	\|-		\|-

Dallen-Andrew at 18:56, 7 August 2024

2024-08-07T18:56:11Z

← Older revision		Revision as of 14:56, 7 August 2024
Line 6:		Line 6:
	\|-		\|-
	\|'''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~~		*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.
	\|}		\|}

Dallen-Andrew: 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..."

2024-08-07T18:55:00Z

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..."

New page

{| 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 numerical solutions for specimen marked PE-1-1
*“[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.
|}