Anisotropy of Residual Stresses Occurring upon Laser Shock Processing of the 2024-T351 Aluminum Alloy and Ways to Reduce It
Author:
Publisher
Allerton Press
Subject
Industrial and Manufacturing Engineering,Mechanical Engineering,Safety, Risk, Reliability and Quality
Link
https://link.springer.com/content/pdf/10.3103/S1052618821080112.pdf
Reference19 articles.
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2. Liu, L., Wang, J., and Zhou, J., Characterization and analysis on microhardness and microstructure evolution of brass subjected to laser shock peening, Opt. Laser Technol., 2019, vol. 115, pp. 325–330. https://doi.org/10.1016/j.optlastec.2019.02.043
3. Su, C., Zhou, J.Z., Meng, X., and Huang, S., Improvement in fatigue performance of aluminum alloy welded joints by laser shock peening in a dynamic strain aging temperature regime, Materials, 2016, vol. 9, no. 10, p. 799. https://doi.org/10.3390/ma9100799
4. Morales, M., Ocaña, J.L., Molpeceres, C., Porro, J.A., and García-Beltrán, A., Model based optimization criteria for the generation of deep compressive residual stress fields in high elastic limit metallic alloys by ns-laser shock processing, Surf. Coat. Technol., 2008, vol. 202, no. 11, pp. 2257–2262. https://doi.org/10.1016/j.surfcoat.2007.12.007
5. Sano, Y., Masaki, K., Gushi, T., and Sano, T., Improvement in fatigue performance offriction stir welded a6061-t6 aluminum alloy by laser peening withoutcoating, Mater. Des., 2012, vol. 36, pp. 809–814. https://doi.org/10.1016/j.matdes.2011.10.053
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