๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

The Effect of Surface Engineering Treatments on the Fatigue Behavior of 2024-T351 Aluminum Alloy

โœ Scribed by C.A. Rodopoulos; A.Th. Kermanidis; E. Statnikov; V. Vityazev; O. Korolkov


Book ID
107458087
Publisher
Springer US
Year
2007
Tongue
English
Weight
543 KB
Volume
16
Category
Article
ISSN
1059-9495

No coin nor oath required. For personal study only.


๐Ÿ“œ SIMILAR VOLUMES


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

The effect of sheet thickness on fatigue
โœ W.J. Mills; R.W. Hertzberg ๐Ÿ“‚ Article ๐Ÿ“… 1975 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 794 KB

Variable-amplitude fat@ue studies of 2024-13 ab&num alloy were performed to examine the effect of sheet thickness on fatigue crack growth rate retardation. Results indicated tbat the amouot of retardation increased with decreasing specimen thickness. This phenomenon was attrii to enhanced plastic st

Understanding the effect of block overlo
โœ Chris A. Rodopoulos; Alexis Th. Kermanidis ๐Ÿ“‚ Article ๐Ÿ“… 2007 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 577 KB

This work aims to provide extensive experimental evidence that reinforce the fact that block overloading can produce phenomena of either crack growth acceleration or retardation depending on its magnitude, duration and the fatigue damage stage characterising its onset. Compared to the majority of si

Effects of crack closure on fatigue crac
โœ Y. Yamada; T. Lacy; J. Newman Jr.; B.L. Smith; B. Kumar ๐Ÿ“‚ Article ๐Ÿ“… 2007 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 396 KB

Effects of plasticity induced crack closure on the calculated fatigue crack-growth behaviour of middle-crack tension specimens made of 2024-T351 alloy subjected to variable amplitude fatigue loading were examined. The specified loadings were four distinct aircraft spectra: (1) ''modified'' center-wi