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- W16829505 abstract "ABSTRACT Fatigue crack propagation rates in a welded Al-4.5% Mg naval alloy plate have been studied. Compact tension specimens have been taken to allow tests to be carried out on the rolled plate, the weld metal region and on specimens with welds at right angles to the growing crack. Two mean load values have been investigated. It was found that the weld metal regions had greater fatigue resistance than the rolled plate and this effect increased with increasing mean stress. Similar effects could be obtained by incorporating a weld ahead 01 and at right angles to the advancing crack. The effect of the distance between these welds and the fatigue crack were studied and maximum benefit occurred when the weld region coincided with the onset or plane stress mode growth. These effects were associated with the presence of relatively coarse inclusions in the weld metal which were associated with shear ridges on the fracture surfaces." @default.
- W16829505 created "2016-06-24" @default.
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- W16829505 date "1986-01-01" @default.
- W16829505 modified "2023-10-15" @default.
- W16829505 title "A STUDY OF FATIGUE CRACK GROWTH RATES IN WELDED Al-Mg ALLOY PLATE" @default.
- W16829505 cites W2067017284 @default.
- W16829505 doi "https://doi.org/10.1016/b978-0-08-033440-0.50036-1" @default.
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