Description
The room temperature tensile test of 5052 aluminum alloy base metal and welded structure and the fatigue crack growth rate test under different stress ratios were carried out, and the corresponding test data were obtained.
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Metrics Over Time
Publication Details
DOI
Publisher
Science Data Bank
Subfield
Aerospace Engineering
Field
Engineering
Domain
Physical Sciences
Confidence Score
58%
Source
Scholar Data Model
Keywords
Transportation engineeringMechanicsaluminium alloyResidual stressprediction modelCrack growth behavior