Titanium Alloys: An Atlas of Structures and Fracture Features

By V. Joshi. 2006

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An experimental study of residual stress and direction-dependence of fatigue crack growth behaviour in as-built and stress-relieved selective-laser-melted Ti6Al4V (2019, background): “Introduction Titanium alloy Ti6Al4V is widely used in the aerospace industry to produce parts which require high strength, low density, excellent corrosion resistance, and unique combination of fatigue crack growth resistance and ductility [1,2].”