Aluminum 2014-O

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Aluminum 2014-O
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. Data points with the AA note have been provided by the Aluminum Association, Inc. and are NOT FOR DESIGN. Composition Notes: A Zr + Ti limit of 0.20 percent maximum may be used with this alloy designation for extruded and forged products only, but only when the supplier and the purchaser have mutually agreed. Composition information provided by the Aluminum Association and is not for design.
Key Words:	Aluminium 2014-O; UNS A92014; ISO AlCu4SiMg; BS H15 (UK); CSA CS41N (Canada); AA2014-O, DIN AlCuSiMn; NF A-U4SG (France); Al2014-O
Vendors:

Available Properties

Density, AA; Typical
Hardness, Brinell, AA; Typical; 500 g load; 10 mm ball
Tensile Strength, Ultimate, AA; Typical
Tensile Strength, Ultimate, Extruded wire, rod, bar, and shapes
Tensile Strength, Ultimate, Extruded tube
Tensile Strength, Ultimate, Sheet and plate
Tensile Strength, Ultimate, Sheet and plate
Tensile Strength, Ultimate, Drawn tube
Tensile Strength, Yield, AA; Typical
Tensile Strength, Yield, Extruded wire, rod, bar, and shapes
Tensile Strength, Yield, Extruded tube
Tensile Strength, Yield, Sheet and plate
Tensile Strength, Yield, Drawn tube
Elongation at Break, Extruded wire, rod, bar, and shapes
Elongation at Break, Extruded tube
Elongation at Break, Sheet and plate
Elongation at Break, Sheet and plate
Elongation at Break, AA; Typical
Modulus of Elasticity, AA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus.
Tensile Modulus
Compressive Strength
Compressive Modulus
Poissons Ratio
Fatigue Strength, completely reversed stress; RR Moore machine/specimen
Machinability, 0-100 Scale of Aluminum Alloys
Shear Modulus
Shear Strength, AA; Typical
Electrical Resistivity, AA; Typical
CTE, linear
CTE, linear
CTE, linear, AA; Typical; average over range
CTE, linear
CTE, linear
Specific Heat Capacity, Estimated from trends in similar Al alloys.
Thermal Conductivity, AA; Typical at 77°F
Melting Point, AA; Typical range based on typical composition for wrought products >= 1/4 in. thickness. Eutectic melting is not eliminated by homogenization.
Solidus, AA; Typical
Liquidus, AA; Typical
Annealing Temperature
Solution 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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