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  4. The effect of residual thermal stresses on the fatigue crack growth of laser-surface-annealed AISI 304 stainless steel. Part I: Computer simulation
 
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The effect of residual thermal stresses on the fatigue crack growth of laser-surface-annealed AISI 304 stainless steel. Part I: Computer simulation

Journal
Materials Science and Engineering A
Journal Volume
364
Journal Issue
1-2
Pages
101-108
Date Issued
2004
Author(s)
Shiue, R.K.
Chang, C.T.
Young, M.C.
Tsay, L.W.
REN-KAE SHIUE  
DOI
10.1016/j.msea.2003.07.003
URI
https://scholars.lib.ntu.edu.tw/handle/123456789/491899
URL
https://www.scopus.com/inward/record.uri?eid=2-s2.0-0742287953&doi=10.1016%2fj.msea.2003.07.003&partnerID=40&md5=2c10056068427242d9ebd75e779cdeb0
Abstract
The effect of residual thermal stresses on the fatigue crack growth of the laser-surface-annealed AISI 304 stainless steel, especially the effect of stress redistribution ahead of the crack tip was extensively evaluated in the study. Based on the finite element simulation, the longitudinal residual tensile stress field has a width of roughly 20 mm on the laser-irradiated surface and was symmetric with respect to the centerline of the laser-annealed zone (LAZ). Meanwhile, residual compressive stresses distributed over a wide region away from the LAZ. After introducing a notch perpendicular to the LAZ, the distribution of longitudinal residual stresses became unsymmetrical about the centerline of LAZ. High residual compressive stresses exist within a narrow range ahead of notch tip. The improved crack growth resistance of the laser-annealed specimen might be attributed to those induced compressive stresses. As the notch tip passed through the centerline of the LAZ, the residual stress ahead of the notch tip was completely reverted into residual tensile stresses. The existence of unanimous residual tensile stresses ahead of the notch tip was maintained, even if the notch tip extended deeply into the LAZ. Additionally, the presence of the residual tensile stress ahead of the notch tip did not accelerate the fatigue crack growth rate in the compact tension specimen. © 2003 Elsevier B.V. All rights reserved.
Type
journal article

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