Aluminum 2024-T851
Subcategory: Aluminum Alloy; Nonferrous Metal; 2000 Series Aluminum Alloy
Close Analogs: 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 or producer and the purchaser have mutually so agreed. Agreement may be indicated, for example, by reference to a standard, by letter, by order note, or other means which allow the Zr + Ti limit. Aluminum content reported is calculated as remainder. Composition information provided by the Aluminum Association and is not for design.
Key Words: Aluminium 2024-T851; AA2024-T851; UNS A92024
Material Notes: Weldability = C; Stress Corrosion Cracking Resistance = B; General Corrosion Resistance = D (A = best; E = worst). Good machinability and surface finish capabilities. A high strength material of adequate workability. Has largely superceded 2017 for structural applications.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. Some data provided by Alcoa. Data points with the AA note have been provided by the Aluminum Association, Inc. and are NOT FOR DESIGN.
Available Properties |
- Density
- Hardness, Brinell
- Hardness, Knoop
- Hardness, Rockwell A
- Hardness, Rockwell B
- Hardness, Vickers
- Tensile Strength, Ultimate
- Tensile Strength, Yield
- Elongation at Break
- Modulus of Elasticity
- Poissons Ratio
- Fatigue Strength
- Machinability
- Shear Modulus
- Shear Strength
- Electrical Resistivity
- CTE, linear 68°F
- CTE, linear 250°C
- Specific Heat Capacity
- Thermal Conductivity
- Melting Point
- Solidus
- Liquidus
- Annealing Temperature
- Solution Temperature
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Property Data |
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