Titanium alloys are known for their high-temperature strength, good fracture resistance, low specific gravity, and excellent resistance to corrosion. Ti-6Al-4V is the most commonly used titanium alloy in the aerospace, aircraft, automotive, and biomedical industries. This article discusses various additive manufacturing (AM) technologies for processing titanium and its alloys. These include directed-energy deposition (DED), powder-bed fusion (PBF), and sheet lamination. The discussion covers the effect of AM on the microstructures of the materials deposited, static and mechanical properties, and fatigue strength and fracture toughness of Ti-6Al-4V.

This article covers the current state of materials development of nickel-base superalloys for additive manufacturing (AM) processes and the associated challenges. The discussion focuses on nickel-base superalloy fusion AM processes, providing information on typically encountered cracking mechanisms in AM nickel-base superalloys, such as solid-solution-strengthened nickel-base superalloys and precipitate-strengthened nickel-base superalloys. The mechanisms include solidification cracking, strain-age cracking, liquation cracking, and ductility-dip cracking. The article also provides a short discussion on binder jet AM and powder recyclability.