Alclad Aluminum 2014-T6, T651

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Alclad Aluminum 2014-T6, T651
Categories:	Metal; Nonferrous Metal; Aluminum Alloy; 2000 Series Aluminum Alloy
Material Notes:	Used in applications requiring high strength/hardness, including elevated temperature uses. Specific applications include heavy duty forgings, plate, and extrusions for aerospace fittings, wheels, tanks, and major structural components, heavy duty automotive frame and suspension componentry. 2014 exhibits poor corrosion resistance for an aluminum alloy so the clad version is used when necessary. Data points with the AA note have been provided by the Aluminum Association, Inc. and are NOT FOR DESIGN. Composition Notes: Composition for AA 2014 (not Alclad 2014 specifically). Composition information provided by the Aluminum Association and is not for design.
Key Words:	UNS A82014; Alclad 2014-T6, T651; Alclad 2014-T6, T651; Al2014-T6
Vendors:

Available Properties

Density, For AA2014 (Not Alclad)
Tensile Strength, Ultimate, AA; Typical
Tensile Strength, Ultimate, Plate; T62, T651
Tensile Strength, Ultimate, Sheet
Tensile Strength, Ultimate, Sheet
Tensile Strength, Ultimate, Plate; T62, T651
Tensile Strength, Ultimate, Sheet
Tensile Strength, Ultimate, Plate; T62, T651
Tensile Strength, Ultimate, Plate; T62, T651
Tensile Strength, Ultimate, Plate; T62, T651
Tensile Strength, Yield, AA; Typical
Tensile Strength, Yield, Sheet
Tensile Strength, Yield, Sheet
Tensile Strength, Yield, Plate; T62, T651
Tensile Strength, Yield, Sheet
Tensile Strength, Yield, Plate; T62, T651
Tensile Strength, Yield, Plate; T62, T651
Tensile Strength, Yield, Plate; T62, T651
Tensile Strength, Yield, Plate; T62, T651
Elongation at Break, Plate; T62, T651
Elongation at Break, Plate; T62, T651
Elongation at Break, Plate; T62, T651
Elongation at Break, Plate; T62, T651
Elongation at Break, Sheet
Elongation at Break, Sheet
Elongation at Break, Sheet
Elongation at Break, Plate; T62, T651
Elongation at Break, AA; Typical
Modulus of Elasticity, AA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus.
Shear Strength, AA; Typical
Annealing Temperature
Solution Temperature
Aging Temperature, Sheet, plate, wire, rod, bar, shapes, tube; 18 hr at temperature
Aging Temperature, Forgings; 10 hr at temperature
Aluminum, Al, As remainder
Chromium, Cr
Copper, Cu
Iron, Fe
Magnesium, Mg
Manganese, Mn
Other, each
Other, total
Silicon, Si
Titanium, Ti
Zinc, Zn

Property Data

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