𝔖 Bobbio Scriptorium
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FATIGUE CRACK CLOSURE MEASUREMENTS ON 2024-T3 SHEET SPECIMENS

✍ Scribed by W. Yisheng; J. Schijve


Book ID
118712483
Publisher
John Wiley and Sons
Year
2007
Tongue
English
Weight
315 KB
Volume
18
Category
Article
ISSN
8756-758X

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πŸ“œ SIMILAR VOLUMES


The effect of sheet thickness on fatigue
✍ W.J. Mills; R.W. Hertzberg πŸ“‚ Article πŸ“… 1975 πŸ› Elsevier Science 🌐 English βš– 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
✍ P.J Golden; A.F Grandt Jr.; G.H Bray πŸ“‚ Article πŸ“… 1999 πŸ› Elsevier Science 🌐 English βš– 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 specimen configuration and
✍ Vikas Kumar Saxena; G. Malakondaiah; V.M. Radhakrishnan πŸ“‚ Article πŸ“… 1994 πŸ› Elsevier Science 🌐 English βš– 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