The residual strength of cracked sheet - Testsinterrupted after intermediate slow crack growth

Title

The residual strength of cracked sheet - Testsinterrupted 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 " T 6 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 t o have no effect on the residual strength

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 Publisher

Nationaal Lucht- en Ruimtevaartlaboratorium

 Access restriction

Campus only

 Source

NLR-M.2145

 Part of collection

Aerospace Engineering Reports

 Document type

report

 Rights

(c)1965 National Aerospace Laboratory NLR
Files
PDF NLR-M.2145.pdf 25.76 MB
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