Aluminum 2024-T361

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Aluminum 2024-T361
Categories:	Metal; Nonferrous Metal; Aluminum Alloy; 2000 Series Aluminum Alloy
Material Notes:	General 2024 characteristics and uses (from Alcoa): Good machinability and surface finish capabilities. A high strength material of adequate workability. Has largely superseded 2017 for structural applications. Uses: Aircraft fittings, gears and shafts, bolts, clock parts, computer parts, couplings, fuse parts, hydraulic valve bodies, missile parts, munitions, nuts, pistons, rectifier parts, worm gears, fastening devices, veterinary and orthopedic equipment, structures. 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 2024-T361; UNS A92024; ISO AlCu4Mg1; NF A-U4G1 (France); DIN AlCuMg2, ASME SB211; CSA CG42 (Canada); AA2024-T361; Al2024-T361
Vendors:

Available Properties

Density, AA; Typical
Hardness, Brinell, AA; Typical; 500 g load; 10 mm ball
Hardness, Knoop, Converted from Brinell Hardness Value
Hardness, Rockwell A, Converted from Brinell Hardness Value
Hardness, Rockwell B, Converted from Brinell Hardness Value
Hardness, Vickers, Converted from Brinell Hardness Value
Tensile Strength, Ultimate, AA; Typical
Tensile Strength, Ultimate, Sheet and plate
Tensile Strength, Ultimate, Sheet and plate
Tensile Strength, Ultimate, Sheet and plate
Tensile Strength, Yield, AA; Typical
Tensile Strength, Yield, Sheet and plate
Tensile Strength, Yield, Sheet and plate
Tensile Strength, Yield, Sheet and plate
Elongation at Break, Sheet and plate
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.
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
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
Aging Temperature, 8 to 16 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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