UDIMET WASPALOY is a nickel-base, austenitic, precipitation-hardenable alloy. It features outstanding tensile and stress-rupture strength up to 1400 F and high oxidation resistance up to 1600 F. It is used widely in gas turbine engines, airframe assemblies and missile systems. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-257. Producer or source: Special Metals Corporation.

aerospace applications, chemical composition, corrosion-resistant alloys, creep fracture, creep properties, elasticity, fatigue properties, fracture toughness, gas turbines, hardness, heat treatability, joinability, machinability, oxidation resistance, physical properties, tensile properties, UDIMET WASPALOY, workability
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1996
ASM International
Topics
Creep fracture Air and spacecraft Gas turbines Corrosion-resistant alloys Nickel alloys Chemical composition Oxidation resistance Heat treatability Joinability Machinability Workability Creep properties Elastic modulus Fatigue properties Fracture toughness Hardness Tensile properties Physical properties Thermal properties
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