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Aluminum 2024-T4; 2024-T351
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 Has largely superseded 2017 for structural applications.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-T351; AA2024-T351, Aluminium 2024-T4; UNS A92024; ISO AlCu4Mg1; NF A-U4G1 (France); DIN AlCuMg2; AA2024-T4, ASME SB211; CSA CG42 (Canada); Al2024-T4
Vendors: Click here to view all available suppliers for this material.

Please click here if you are a supplier and would like information on how to add your listing to this material.

 
Physical PropertiesOriginal ValueComments
Density 2.78 g/ccAA; Typical
 
Mechanical PropertiesOriginal ValueComments
Hardness, Brinell 120AA; Typical; 500 g load; 10 mm ball
Hardness, Knoop 150Converted from Brinell Hardness Value
Hardness, Rockwell A 46.8Converted from Brinell Hardness Value
Hardness, Rockwell B 75Converted from Brinell Hardness Value
Hardness, Vickers 137Converted from Brinell Hardness Value
Tensile Strength, Ultimate 68.0 ksiAA; Typical
 >= 395 MPaWire, rod, bar and shapes (extruded); T42
 >= 425 MPaCoiled sheet
 >= 425 MPaWire, rod, and bar (rolled or cold finished); T42
 >= 425 MPaWire, rod, and bar (rolled or cold finished); T351
 >= 425 MPaRivet and cold-heading wire and rod
 >= 440 MPaDrawn tube; T42
 >= 495 MPaExtruded tube; T42
 34.0 MPa
@Temperature 371 °C
 52.0 MPa
@Temperature 316 °C
 76.0 MPa
@Temperature 260 °C
 179 MPa
@Temperature 204 °C
 310 MPa
@Temperature 149 °C
 434 MPa
@Temperature 100 °C
 469 MPa
@Temperature 24.0 °C
 476 MPa
@Temperature -28.0 °C
 490 MPa
@Temperature -80.0 °C
 579 MPa
@Temperature -196 °C
Tensile Strength, Yield 47.0 ksiAA; Typical
 >= 260 MPaWire, rod, bar and shapes (extruded); T42
 >= 260 MPaExtruded tube; T42
 >= 275 MPaCoiled sheet
 >= 275 MPaWire, rod, and bar (rolled or cold finished); T42
 >= 275 MPaDrawn tube; T42
 >= 275 MPaRivet and cold-heading wire and rod
 >= 310 MPaWire, rod, and bar (rolled or cold finished); T351
 28.0 MPa
@Strain 0.2 %,
Temperature 371 °C
 41.0 MPa
@Strain 0.2 %,
Temperature 316 °C
 62.0 MPa
@Strain 0.2 %,
Temperature 260 °C
 131 MPa
@Strain 0.2 %,
Temperature 204 °C
 248 MPa
@Strain 0.2 %,
Temperature 149 °C
 310 MPa
@Strain 0.2 %,
Temperature 100 °C
 324 MPa
@Strain 0.2 %,
Temperature -28.0 °C
 324 MPa
@Strain 0.2 %,
Temperature 24.0 °C
 338 MPa
@Strain 0.2 %,
Temperature -80.0 °C
 421 MPa
@Strain 0.2 %,
Temperature -196 °C
Elongation at Break >= 10 %Wire, rod, and bar (rolled or cold finished); T42
 >= 10 %Wire, rod, and bar (rolled or cold finished); T351
 >= 10 %Rivet and cold-heading wire and rod
 8.0 - 12 %Wire, rod, bar and shapes (extruded); T42
 8.0 - 12 %Extruded tube; T42
 10 - 16 %Drawn tube; T42
 12 - 15 %Coiled sheet
 17 %
@Temperature 149 °C
 19 %
@Temperature -196 °C
 19 %
@Temperature -80.0 °C
 19 %
@Temperature -28.0 °C
 19 %
@Temperature 24.0 °C
 19 %
@Temperature 100 °C
 27 %
@Temperature 204 °C
 55 %
@Temperature 260 °C
 75 %
@Temperature 316 °C
 100 %
@Temperature 371 °C
Modulus of Elasticity 10600 ksiAA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus.
Ultimate Bearing Strength 814 MPaEdge distance/pin diameter = 2.0
Bearing Yield Strength 441 MPaEdge distance/pin diameter = 2.0
Poissons Ratio 0.33
Fatigue Strength 20000 psi
@# of Cycles 5.00e+8
completely reversed stress; RR Moore machine/specimen
Fracture Toughness 26.0 MPa-m½K(IC) in S-L Direction
 32.0 MPa-m½K(IC) in T-L Direction
 37.0 MPa-m½K(IC) in L-T Direction
Machinability 70 %0-100 Scale of Aluminum Alloys
Shear Modulus 28.0 GPa
Shear Strength 41.0 ksiAA; Typical
 
Electrical PropertiesOriginal ValueComments
Electrical Resistivity 35.0 ohm-cir-mil/ft
@Temperature 20.0 °C
AA; Typical
 
Thermal PropertiesOriginal ValueComments
CTE, linear 12.9 µin/in-°F
@Temperature 20.0 - 100 °C
AA; Typical; average over range
 21.1 µm/m-°C
@Temperature -50.0 - 20.0 °C
 22.9 µm/m-°C
@Temperature 20.0 - 100 °C
 23.8 µm/m-°C
@Temperature 20.0 - 200 °C
 24.7 µm/m-°C
@Temperature 20.0 - 300 °C
Specific Heat Capacity 0.875 J/g-°C
Thermal Conductivity 840 BTU-in/hr-ft²-°FAA; Typical at 77°F
Melting Point 935 - 1180 °FAA; Typical range based on typical composition for wrought products >= 1/4 in. thickness. Eutectic melting is not eliminated by homogenization.
Solidus 935 °FAA; Typical
Liquidus 1180 °FAA; Typical
 
Processing PropertiesOriginal ValueComments
Annealing Temperature 775 °F
Solution Temperature 493 °C
 
Component Elements PropertiesOriginal ValueComments
Aluminum, Al 90.7 - 94.7 %As remainder
Chromium, Cr <= 0.10 %
Copper, Cu 3.8 - 4.9 %
Iron, Fe <= 0.50 %
Magnesium, Mg 1.2 - 1.8 %
Manganese, Mn 0.30 - 0.90 %
Other, each <= 0.05 %
Other, total <= 0.15 %
Silicon, Si <= 0.50 %
Titanium, Ti <= 0.15 %
Zinc, Zn <= 0.25 %

References for this datasheet.

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