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Nickel-based alloys are composed of over half of the materials used in the aerospace
industry. These alloys are under constant improvement for better strength and surface
integrity. Surface integrity is defined as the inherent condition of a machined surface
and its major components can be grouped into surface texture (of which surface
roughness is the most important), metallurgy, and the residual stress generated on
the surface and subsurface of the machined workpiece (Jawahir et al., 2011; and
Ulutan and Ozel, 2011). Inconel is a family of austenitic nickel-chromium-based
superalloys. Inconel-718 (UNS N07718) is a precipitation hardening Ni superalloy,
which contains significant levels of molybdenum, iron, columbium and niobium,
along with traces of aluminum and titanium. Due to the high amount of chromium
and other alloying elements, it is a highly corrosion and oxidation resistant material
well suited for service in hot and corrosive environments. When heated, Inconel- 718 forms a stable and adherent oxide layer that protects the surface from further
attack. It is very heat treatable and a wide variety of mechanical properties, including
hardness and strength, can be obtained (Arunachalam and Mannan, 2000).
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