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FATIGUE STRENGTH OF 7075-T6 ALUMINIUM ALLOY UNDER COMBINED AXIAL LOADING AND TORSION

โœ Scribed by K. Tanaka1,; S. Matsuoka; M. Kimura2

Book ID
109012008
Publisher
John Wiley and Sons
Year
1984
Tongue
English
Weight
1014 KB
Volume
7
Category
Article
ISSN
8756-758X

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Fatigue of 7075-T651 aluminum alloy unde
Fatigue of 7075-T651 aluminum alloy under constant and variable amplitude loadings
โœ E.U. Lee; G. Glinka; A.K. Vasudevan; N. Iyyer; N.D. Phan ๐Ÿ“‚ Article ๐Ÿ“… 2009 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 508 KB

The fatigue crack growth (FCG) behavior of 7075-T651 aluminum alloy was studied under constant and variable amplitude loadings in vacuum, air and 1% NaCl solution. In the study of constant amplitude loading fatigue, the stress ratios were 0.1 and 0.85 and the loading frequency was 10 Hz. In the stud