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2007-T3510 Aluminum

2007-T3510 aluminum is 2007 aluminum in the T3510 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 T3511, which permits such straightening.

It has the highest strength compared to the other variants of 2007 aluminum.

The graph bars on the material properties cards below compare 2007-T3510 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

71 GPa 10 x 106 psi

Elongation at Break

5.7 %

Fatigue Strength

96 MPa 14 x 103 psi

Poisson's Ratio

0.33

Shear Modulus

27 GPa 3.9 x 106 psi

Shear Strength

250 MPa 36 x 103 psi

Tensile Strength: Ultimate (UTS)

420 MPa 61 x 103 psi

Tensile Strength: Yield (Proof)

270 MPa 39 x 103 psi

Thermal Properties

Latent Heat of Fusion

390 J/g

Maximum Temperature: Mechanical

190 °C 380 °F

Melting Completion (Liquidus)

640 °C 1180 °F

Melting Onset (Solidus)

510 °C 950 °F

Specific Heat Capacity

870 J/kg-K 0.21 BTU/lb-°F

Thermal Conductivity

130 W/m-K 75 BTU/h-ft-°F

Thermal Expansion

23 µm/m-K

Electrical Properties

Electrical Conductivity: Equal Volume

47 % IACS

Electrical Conductivity: Equal Weight (Specific)

140 % IACS

Otherwise Unclassified Properties

Base Metal Price

11 % relative

Density

3.1 g/cm3 190 lb/ft3

Embodied Carbon

8.0 kg CO2/kg material

Embodied Energy

150 MJ/kg 63 x 103 BTU/lb

Embodied Water

1130 L/kg 130 gal/lb

Common Calculations

Resilience: Ultimate (Unit Rupture Work)

21 MJ/m3

Resilience: Unit (Modulus of Resilience)

510 kJ/m3

Stiffness to Weight: Axial

13 points

Stiffness to Weight: Bending

44 points

Strength to Weight: Axial

38 points

Strength to Weight: Bending

40 points

Thermal Diffusivity

48 mm2/s

Thermal Shock Resistance

19 points

Alloy Composition

Aluminum (Al)Al 87.5 to 95
Copper (Cu)Cu 3.3 to 4.6
Lead (Pb)Pb 0.8 to 1.5
Magnesium (Mg)Mg 0.4 to 1.8
Manganese (Mn)Mn 0.5 to 1.0
Silicon (Si)Si 0 to 0.8
Iron (Fe)Fe 0 to 0.8
Zinc (Zn)Zn 0 to 0.8
Nickel (Ni)Ni 0 to 0.2
Titanium (Ti)Ti 0 to 0.2
Tin (Sn)Sn 0 to 0.2
Bismuth (Bi)Bi 0 to 0.2
Chromium (Cr)Cr 0 to 0.1
Residualsres. 0 to 0.3

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

Followup Questions

Further Reading

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

Aluminum: Properties and Physical Metallurgy, John E. Hatch (editor), 1984

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

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

Properties and Selection: Nonferrous Alloys and Special-Purpose Materials, ASM Handbook vol. 2, ASM International, 1993