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NASA-LLIS-0764

Lessons Learned - Controlling Stress Corrosion Cracking in Aerospace Applications

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 2000

Abstract: Practice:
This practice presents considerations that should be evaluated and applied concerning stress corrosion and subsequent crack propagation in mechanical devices, structural devices, and related components used in aerospace applications. Material selection, heat treat methods, fabrication methodology, testing regimes, and loading path assessments are presented as methods to reduce the potential for stress corrosion cracking in a material's operational environment.
URI: https://yse.yabesh.ir/std/handle/yse/27795
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    NASA-LLIS-0764

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:26:54Z
date available2017-09-04T15:26:54Z
date copyright04/06/2000
date issued2000
identifier otherNPVFQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/27795
description abstractPractice:
This practice presents considerations that should be evaluated and applied concerning stress corrosion and subsequent crack propagation in mechanical devices, structural devices, and related components used in aerospace applications. Material selection, heat treat methods, fabrication methodology, testing regimes, and loading path assessments are presented as methods to reduce the potential for stress corrosion cracking in a material's operational environment.
languageEnglish
titleNASA-LLIS-0764num
titleLessons Learned - Controlling Stress Corrosion Cracking in Aerospace Applicationsen
typestandard
page5
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2000
contenttypefulltext
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