Journal
INTERNATIONAL JOURNAL OF MODERN PHYSICS B
Volume 31, Issue 16-19, Pages -Publisher
WORLD SCIENTIFIC PUBL CO PTE LTD
DOI: 10.1142/S021797921744009X
Keywords
Aluminum alloy; corrosion fatigue; crack propagation; high-speed train
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A modified single-edge notch tension (SENT) specimen exposed to saline environment was utilized to investigate the corrosion fatigue crack growth behaviors of 5083, 6005 and 7N01 aluminum alloys. The fatigue crack propagation life, corrosion fatigue crack rate (da/dN) were tested. The microstructures and fracture surfaces of specimens were examined by optical microscopy and scanning electron microscopy (SEM). The results showed that fatigue crack propagation rate of 7N01 in 3.5% NaCl was significantly higher than 6005 and 5083 alloys. The mechanisms of anodic dissolution and hydrogen embrittlement are used to explain the results.
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