Open AccessResidual Strength of Five Boron/Aluminum Laminates with Crack-Like Notches After Fatigue Loading
Author(s) -
RA Simonds
Publication year - 1986
Publication title -
nasa sti repository (national aeronautics and space administration)
Language(s) - English
Resource type - Book series
DOI - 10.1520/stp17393s
Subject(s) - materials science , composite material , residual stress , residual strength , aluminium , fatigue limit , structural engineering , fatigue testing , boron , engineering , chemistry , organic chemistry
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