Abstract
Ti-8A1-1Mo-1V is a titanium alloy having excellent creep resistance and stress-rupture life. It is recommended for jet engine components operating up to 900 F. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear strength as well as fracture toughness and creep. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Ti-32. Producer or source: Titanium Metals Corporation of America.
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Copyright © ASM International® 1996
1996
ASM International
Topics
Creep fracture
High-temperature alloys
Alpha and near alpha titanium alloys
Chemical composition
Heat treatability
Joinability
Machinability
Workability
Creep resistance
Elastic modulus
Fracture toughness
Shear strength
Tensile properties
Physical properties
Thermal properties
Aircraft turbine engine components
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