๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Corrosion fatigue of a 2024-T3 aluminum alloy in the short crack domain

โœ Scribed by K. -C. Wan; G. S. Chen; M. Gao; R. P. Wei


Publisher
Springer Netherlands
Year
1995
Tongue
English
Weight
271 KB
Volume
69
Category
Article
ISSN
1573-2673

No coin nor oath required. For personal study only.

โœฆ Synopsis


It is well accepted that the steady-state fatigue crack growth rates of long cracks depend uniquely on AK for a fixed load ratio R and test environment. Anomalous growth behavior of short cracks in either inert or deleterious environments that has been reported [1-7], however, calls into question the validity of using only long-crack results in evaluating the service life of a structural component and argues for the need for considering the effects of crack size. Crack-size effects have been extensively studied from the perspectives of mechanical, metallurgical and chemical principles. Microstructurally and mechanically short cracks [1-3] are associated with the influences of fine-scale microstructure, the limitation of continuum mechanics (or LEFM-linear elastic fracture mechanics), or crack closure. Chemically short cracks [4][5][6][7], on the other hand, normally extend to longer lengths and are attributed to the differences in local crack-tip chemistry (e.g., pH, [Oz], potential) between the long and short cracks and also, perhaps, from the bulk solution. The objective of this study is to explore the effect of crack size in various environments and to identify the key variables that affect crack growth behavior. The crack size investigated herein was chemically short but microstructurally and mechanically long.


๐Ÿ“œ SIMILAR VOLUMES


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

A comparison of fatigue crack formation
โœ P.J Golden; A.F Grandt Jr.; G.H Bray ๐Ÿ“‚ Article ๐Ÿ“… 1999 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 919 KB

The purpose of this research was to compare the resistance to the onset of multi-site damage in thin 2024-T3 and 2524-T3 sheet. Aluminum alloy 2524-T3 is a relatively new fuselage skin sheet material that may offer improved performance with respect to the onset of multi-site damage. The alloys were

Influence of fatigue damage on the mecha
โœ A. May; M.A. Belouchrani; A. Manaa; Y. Bouteghrine ๐Ÿ“‚ Article ๐Ÿ“… 2011 ๐Ÿ› Elsevier ๐ŸŒ English โš– 675 KB

The present work is devoted to study the influence of high cycle fatigue damage rate at R = 0.1, on the mechanical properties of aluminum alloy 2024-T3 which is largely used in aircraft industry. The study consists of an experimental investigation in the evolution of the static properties such as th

Fatigue crack propagation rate at low ฮ”K
โœ T.L. Mackay ๐Ÿ“‚ Article ๐Ÿ“… 1979 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 434 KB

For transport aircraft with long lifetimes, crack growth data to implement the durability life requirements in the low AK range are needed. This is the region comprising most of the lifetime for the cracks of interest, and it is also the region where there is little data available. Crack growth data

Effect of root flaws on the fatigue prop
โœ Caizhi Zhou; Xinqi Yang; Guohong Luan ๐Ÿ“‚ Article ๐Ÿ“… 2006 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 626 KB

The fatigue experiment of friction stir (FS) welds in 2024-T3 aluminum alloys were performed to investigate the influence of root flaws on the fatigue strength and life of FS welds. The test results of welds with flaws (flawed welds) were compared with the results suggested by the International Inst