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NASA-LLIS-2256

Lessons Learned – Penetrant Evaluation of Metallic Tanks and Composite Overwrapped Pressure Vessel Liners

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 2009

Abstract: Abstract:
As the desired crack detection size is decreased and approaches the physical limitations of liquid penetrant inspection techniques, the approach of performing a probability of detection (POD) validation test at a single aspect ratio, and then extending the results to other aspect ratios based on equivalent area predictions may not be valid. POD testing for penetrant inspection of metallic pressure vessels and COPV liners should be performed at the bounds of the required range of crack aspect ratios.
URI: https://yse.yabesh.ir/std/handle/yse/133688
Subject: Additional Categories.Pressure Vessels
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    NASA-LLIS-2256

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:10:11Z
date available2017-09-04T17:10:11Z
date copyright40162
date issued2009
identifier otherYOYCQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/133688
description abstractAbstract:
As the desired crack detection size is decreased and approaches the physical limitations of liquid penetrant inspection techniques, the approach of performing a probability of detection (POD) validation test at a single aspect ratio, and then extending the results to other aspect ratios based on equivalent area predictions may not be valid. POD testing for penetrant inspection of metallic pressure vessels and COPV liners should be performed at the bounds of the required range of crack aspect ratios.
languageEnglish
titleNASA-LLIS-2256num
titleLessons Learned – Penetrant Evaluation of Metallic Tanks and Composite Overwrapped Pressure Vessel Linersen
typestandard
page3
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2009
contenttypefulltext
subject keywordsAdditional Categories.Pressure Vessels
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