Print Email Facebook Twitter The residual strength of cracked sheet - Tests interrupted after intermediate slow crack growth Title The residual strength of cracked sheet - Tests interrupted after intermediate slow crack growth Author Broek, D. Institution National Aerospace Laboratory NLR Date 1965-07-31 Abstract Residual strength tests were performed on 2024-T3 and 7075-T6 aluminium alloy sheet specimens of 600 mm width. After the cracks had shown some stable slow growth the specimens were unloaded and then reloaded. Unloading appeared to have no effect on the residual strength To reference this document use: http://resolver.tudelft.nl/uuid:af8c8cc1-057d-446d-8345-585cb7db3fc0 Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR-TR M.2145 Part of collection Aerospace Engineering Reports Document type report Rights (c)1965 National Aerospace Laboratory NLR Files PDF NLR-TR.M.2145.pdf 8.36 MB Close viewer /islandora/object/uuid:af8c8cc1-057d-446d-8345-585cb7db3fc0/datastream/OBJ/view