๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Fatigue crack growth retardation assessment of 2024-T3 and 6061-T6 aluminium specimens

โœ Scribed by Sp.G. Pantelakis; Th.B. Kermanidis; D.G. Pavlou


Book ID
107919630
Publisher
Elsevier Science
Year
1995
Tongue
English
Weight
413 KB
Volume
22
Category
Article
ISSN
0167-8442

No coin nor oath required. For personal study only.


๐Ÿ“œ SIMILAR VOLUMES


Influence of specimen configuration and
โœ Vikas Kumar Saxena; G. Malakondaiah; V.M. Radhakrishnan ๐Ÿ“‚ Article ๐Ÿ“… 1994 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 425 KB

## Experimental investigations have been carried out to study the effect of specimen configuration and loading history on the crack growth behaviour of 2024-T3 aluminium alloy at room temperature. It has been observed that fatigue crack growth rate in specimens loaded symmetrically is higher than

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