๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

The effects of warm working on aluminum alloy 7075-T651

โœ Scribed by John M. Papazian


Publisher
Elsevier Science
Year
1981
Weight
687 KB
Volume
51
Category
Article
ISSN
0025-5416

No coin nor oath required. For personal study only.


๐Ÿ“œ SIMILAR VOLUMES


Fatigue of 7075-T651 aluminum alloy
โœ Tianwen Zhao; Yanyao Jiang ๐Ÿ“‚ Article ๐Ÿ“… 2008 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 668 KB

Extensive fatigue experiments were conducted using 7075-T651 aluminum alloy under uniaxial, torsion, and axial-torsion loading. Detailed fatigue results were reported. Different mean stresses were applied in the experiments and the mean stress was found to have a significant influence on the fatigue

Environmental effects on low cycle fatig
โœ E.U. Lee; A.K. Vasudevan; G. Glinka ๐Ÿ“‚ Article ๐Ÿ“… 2009 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 338 KB

The environmental effects on the low cycle fatigue (LCF) behavior of 2024-T351 and 7075-T651 aluminum alloys were studied at room temperature. The specimens were subjected to identical LCF tests at strain ratio R of ร€1 and frequency of 5 Hz in three environments: vacuum, air and 1% NaCl solution of

A study of fatigue crack growth of 7075-
โœ Tianwen Zhao; Jixi Zhang; Yanyao Jiang ๐Ÿ“‚ Article ๐Ÿ“… 2008 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 370 KB

Both standard and non-standard compact specimens were employed to experimentally study the crack growth behavior of 7075-T651 aluminum alloy in ambient air. The effects of the stress ratio (R), overloading, underloading, and high-low sequence loading on fatigue crack growth rate were investigated. S

Fatigue of 7075-T651 aluminum alloy unde
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

Effects of crack length and crack front
โœ Henk F. De Jong ๐Ÿ“‚ Article ๐Ÿ“… 1981 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 554 KB

Fracture toughness tests on compact tension specimens of aluminum 7075-T6.51 were carried out to investigate the influence of the crack length ratio on the critical stress intensity factor. The results showed that there is probably no, or only a minor influence of the crack length ratio in the inves