β Scribed by A.E. Morabito; A. Chrysochoos; V. Dattoma; U. Galietti
No coin nor oath required. For personal study only.
π SIMILAR VOLUMES
The interaction between residual stress and fatigue crack growth rate has been investigated in middle tension and compact tension specimens machined from a variable polarity plasma arc welded aluminium alloy 2024-T351 plate. The specimens were tested at three levels of applied constant stress intens
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
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
## 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