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2014-T4510 Aluminum

2014-T4510 aluminum is 2014 aluminum in the T4510 temper. To achieve this temper, the metal is solution heat-treated, stress relieved, then naturally aged. The stress relief is accomplished by stretching the metal by an amount that depends on the type of standard wrought product being made (extrusion or tube). The metal is not straightened after the stretching operation. This temper is closely related to T4511, which permits such straightening.

The graph bars on the material properties cards below compare 2014-T4510 aluminum to: 2000-series alloys (top), all aluminum alloys (middle), and the entire database (bottom). A full bar means this is the highest value in the relevant set. A half-full bar means it's 50% of the highest, and so on.

Mechanical Properties

Elastic (Young's, Tensile) Modulus

72 GPa 10 x 106 psi

Elongation at Break

11 %

Fatigue Strength

130 MPa 18 x 103 psi

Poisson's Ratio

0.33

Shear Modulus

27 GPa 3.9 x 106 psi

Shear Strength

240 MPa 35 x 103 psi

Tensile Strength: Ultimate (UTS)

410 MPa 59 x 103 psi

Tensile Strength: Yield (Proof)

270 MPa 38 x 103 psi

Thermal Properties

Latent Heat of Fusion

400 J/g

Maximum Temperature: Mechanical

210 °C 410 °F

Melting Completion (Liquidus)

630 °C 1160 °F

Melting Onset (Solidus)

510 °C 940 °F

Specific Heat Capacity

870 J/kg-K 0.21 BTU/lb-°F

Thermal Conductivity

150 W/m-K 89 BTU/h-ft-°F

Thermal Expansion

23 µm/m-K

Electrical Properties

Electrical Conductivity: Equal Volume

40 % IACS

Electrical Conductivity: Equal Weight (Specific)

120 % IACS

Otherwise Unclassified Properties

Base Metal Price

11 % relative

Density

3.0 g/cm3 190 lb/ft3

Embodied Carbon

8.1 kg CO2/kg material

Embodied Energy

150 MJ/kg 64 x 103 BTU/lb

Embodied Water

1130 L/kg 140 gal/lb

Common Calculations

Resilience: Ultimate (Unit Rupture Work)

38 MJ/m3

Resilience: Unit (Modulus of Resilience)

490 kJ/m3

Stiffness to Weight: Axial

13 points

Stiffness to Weight: Bending

46 points

Strength to Weight: Axial

38 points

Strength to Weight: Bending

40 points

Thermal Diffusivity

58 mm2/s

Thermal Shock Resistance

18 points

Alloy Composition

Aluminum (Al)Al 90.4 to 95
Copper (Cu)Cu 3.9 to 5.0
Silicon (Si)Si 0.5 to 1.2
Manganese (Mn)Mn 0.4 to 1.2
Magnesium (Mg)Mg 0.2 to 0.8
Iron (Fe)Fe 0 to 0.7
Zinc (Zn)Zn 0 to 0.25
Zirconium (Zr)Zr 0 to 0.2
Titanium (Ti)Ti 0 to 0.15
Chromium (Cr)Cr 0 to 0.1
Residualsres. 0 to 0.15

All values are % weight. Ranges represent what is permitted under applicable standards.

Followup Questions

Further Reading

Aerospace Materials, Brian Cantor et al. (editors), 2001

ASTM B221: Standard Specification for Aluminum and Aluminum-Alloy Extruded Bars, Rods, Wire, Profiles, and Tubes

Handbook of Aluminum Bonding Technology and Data, J. D. Minford, 1993

EN 754-2: Aluminium and aluminium alloys. Cold drawn rod/bar and tube. Mechanical properties

ASTM B209: Standard Specification for Aluminum and Aluminum-Alloy Sheet and Plate

EN 755-2: Aluminium and aluminium alloys. Extruded rod/bar, tube and profiles. Mechanical properties

Aluminum Standards and Data, Aluminum Association Inc., 2013

EN 573-3: Aluminium and aluminium alloys. Chemical composition and form of wrought products. Chemical composition and form of products