Strains were mapped in a commercial jet engine titanium alloy fan blade hub

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  • Ti-6Al-4V alpha-beta alloy
  • Large sample (150 lbs)
Long data acquisition times were required

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Diffraction UC | Residual Stress UC | Thermophysical Properties UC
Diffraction & Thermophysical Prop. Group | High Temperature Materials Laboratory
Materials Science & Technology Division | Oak Ridge National Laboratory

Acknowledgments

URL: http://www.html.ornl.gov/diffgroup/hub.html