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- W1566510452 abstract "The fatigue crack growth rate of aluminum-lithium (Al-Li) alloy 2195 plate and weldments was determined at 200 degrees F, ambient temperature and -320 degrees F. The effects of stress ratio (R), welding process, orientation and thickness were studied. Results are compared with plate data from the Space Shuttle Super Lightweight Tank (SLWT) allowables program. Data from the current series of tests, both plate and weldment, falls within the range of data generated during the SLWT allowables program." @default.
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- W1566510452 date "2000-05-01" @default.
- W1566510452 modified "2023-09-26" @default.
- W1566510452 title "Fatigue Crack Growth Rate Test Results for Al-Li 2195 Parent Metal, Variable Polarity Plasma Arc Welds and Friction Stir Welds" @default.
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