Salt stress corrosion cracking of residually stressed Ti-8AI-1Mo-1V break formed sheet at 550 degree F 9561 degree K)[NASA TM X-1082]
By: Pride, Richard A.
Contributor(s): Woodard, John M.
Material type: BookSeries: National Aeronautics and Space Administration (NASA). Publisher: Washington, D. C. NASA April 1965Description: 25p.Subject(s): Residual stresses
Contents:
NASA technical memorandum
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NASA technical memorandum
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