The fatigue crack growth rate (FCGR) characteristics of Laser Shock Peened (LSP) titanium 6Al-4V were examined and compared to those of unprocessed material. The FCGR resistance of LSP processed material tested at low stress ratios (R) is shown to be significantly greater than for unprocessed, baseline material. The increased damage tolerance can be attributed to the large residual compressive stresses generated by the LSP process. Differences in the growth rate behavior due to LSP can be accounted for by using the closure corrected effective stress intensity range, ΔKeff, which takes into account only the portion of loading above the crack opening load. The rationale of using ΔKeff is also demonstrated through fractographic investigations.
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July 1999
Technical Papers
Fatigue Crack Growth Rate Characteristics of Laser Shock Peened Ti-6Al-4V
John J. Ruschau,
John J. Ruschau
University of Dayton Research Institute, 300 College Park, Dayton, OH 45469
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Steven R. Thompson,
Steven R. Thompson
AFRL/MLSC, WPAFB, OH
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Theodore Nicholas
Theodore Nicholas
AFRL/MLLN, WPAFB, OH
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John J. Ruschau
University of Dayton Research Institute, 300 College Park, Dayton, OH 45469
Reji John
AFRL/MLLN, WPAFB, OH
Steven R. Thompson
AFRL/MLSC, WPAFB, OH
Theodore Nicholas
AFRL/MLLN, WPAFB, OH
J. Eng. Mater. Technol. Jul 1999, 121(3): 321-329 (9 pages)
Published Online: July 1, 1999
Article history
Received:
June 8, 1998
Revised:
October 21, 1998
Online:
November 27, 2007
Citation
Ruschau, J. J., John, R., Thompson, S. R., and Nicholas, T. (July 1, 1999). "Fatigue Crack Growth Rate Characteristics of Laser Shock Peened Ti-6Al-4V." ASME. J. Eng. Mater. Technol. July 1999; 121(3): 321–329. https://doi.org/10.1115/1.2812381
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