𝔖 Bobbio Scriptorium
✦   LIBER   ✦

The effect of residual stresses arising from laser shock peening on fatigue crack growth

✍ Scribed by A. Chahardehi; F.P. Brennan; A. Steuwer


Publisher
Elsevier Science
Year
2010
Tongue
English
Weight
380 KB
Volume
77
Category
Article
ISSN
0013-7944

No coin nor oath required. For personal study only.

✦ Synopsis


Residual stresses have in the past been introduced to manipulate growth rates and shapes of cracks under cyclic loads. Previously, the effectiveness of shot peening in retarding the rate of fatigue crack growth was experimentally studied. It was shown that the compressive residual stresses arising from the shot peening process can affect the rate of crack growth. Laser shock peening can produce a deeper compressive stress field near the surface than shot peening. This advantage makes this technique desirable for the manipulation of crack growth rates. This paper describes an experimental program that was carried out to establish this effect in which steel specimens were partially laser peened and subsequently subjected to cyclic loading to grow fatigue cracks. The residual stress fields generated by the laser shock peening process were measured using the neutron diffraction technique. A state of compressive stress was found near the surface and tensile stresses were measured in the mid-thickness of the specimens. Growth rates of the cracks were observed to be more affected by the tensile core than by the compressive surface stresses.


πŸ“œ SIMILAR VOLUMES


Weld residual stress effects on fatigue
✍ C.D.M. Liljedahl; J. Brouard; O. Zanellato; J. Lin; M.L. Tan; S. Ganguly; P.E. I πŸ“‚ Article πŸ“… 2009 πŸ› Elsevier Science 🌐 English βš– 343 KB

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

The effect of pre-stress cycles on fatig
✍ Tai Shan Kang; H.W. Liu πŸ“‚ Article πŸ“… 1974 πŸ› Elsevier Science 🌐 English βš– 561 KB

Cychc pre-stress increases subsequent fatigue crack growth rate in 2024-T3Sl ahrminum ahoy. This increase in growth rate, caused by the pre-stress, and the increased rate, caused by temper embrittlement as observed by Ritchie and Knott, cannot be explained by the crack tip blunting model alone. Each