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6018 (AlMg1SiPbMn) Aluminum

6018 aluminum is a 6000-series aluminum alloy: there is significant alloying with both magnesium and silicon, and the alloy is formulated for primary forming into wrought products. 6018 is the Aluminum Association (AA) designation for this material. In European standards, it will be given as EN AW-6018. AlMg1SiPbMn is the EN chemical designation. Additionally, the UNS number is A96018.

It received its standard designation in 1991, making it a fairly young material.

The properties of 6018 aluminum include three common variations. This page shows summary ranges across all of them. For more specific values, follow the links immediately below. The graph bars on the material properties cards further below compare 6018 aluminum to: 6000-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

69 GPa 10 x 106 psi

Elongation at Break

9.0 to 9.1 %

Fatigue Strength

85 to 89 MPa 12 to 13 x 103 psi

Poisson's Ratio

0.33

Shear Modulus

26 GPa 3.7 x 106 psi

Shear Strength

170 to 180 MPa 25 x 103 psi

Tensile Strength: Ultimate (UTS)

290 to 300 MPa 42 to 43 x 103 psi

Tensile Strength: Yield (Proof)

220 to 230 MPa 32 to 33 x 103 psi

Thermal Properties

Latent Heat of Fusion

400 J/g

Maximum Temperature: Mechanical

160 °C 320 °F

Melting Completion (Liquidus)

640 °C 1180 °F

Melting Onset (Solidus)

570 °C 1060 °F

Specific Heat Capacity

890 J/kg-K 0.21 BTU/lb-°F

Thermal Conductivity

170 W/m-K 96 BTU/h-ft-°F

Thermal Expansion

23 µm/m-K

Electrical Properties

Electrical Conductivity: Equal Volume

44 % IACS

Electrical Conductivity: Equal Weight (Specific)

140 % IACS

Otherwise Unclassified Properties

Base Metal Price

10 % relative

Density

2.9 g/cm3 180 lb/ft3

Embodied Carbon

8.2 kg CO2/kg material

Embodied Energy

150 MJ/kg 65 x 103 BTU/lb

Embodied Water

1180 L/kg 140 gal/lb

Common Calculations

Resilience: Ultimate (Unit Rupture Work)

24 to 25 MJ/m3

Resilience: Unit (Modulus of Resilience)

360 to 380 kJ/m3

Stiffness to Weight: Axial

13 points

Stiffness to Weight: Bending

48 points

Strength to Weight: Axial

28 to 29 points

Strength to Weight: Bending

34 to 35 points

Thermal Diffusivity

65 mm2/s

Thermal Shock Resistance

13 points

Alloy Composition

Among wrought aluminum alloys, the composition of 6018 aluminum is notable for including lead (Pb) and bismuth (Bi). Lead is used to improve machinability at the cost of toxicity and a decrease in weldability. Bismuth is used to improve machinability at the cost of a decrease in weldability.

Aluminum (Al)Al 93.1 to 97.8
Magnesium (Mg)Mg 0.6 to 1.2
Silicon (Si)Si 0.5 to 1.2
Lead (Pb)Pb 0.4 to 1.2
Manganese (Mn)Mn 0.3 to 0.8
Bismuth (Bi)Bi 0.4 to 0.7
Iron (Fe)Fe 0 to 0.7
Copper (Cu)Cu 0.15 to 0.4
Zinc (Zn)Zn 0 to 0.3
Titanium (Ti)Ti 0 to 0.2
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

Similar Alloys

Further Reading

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

ASM Specialty Handbook: Aluminum and Aluminum Alloys, J. R. Davis (editor), 1993

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

CRC Materials Science and Engineering Handbook, 4th ed., James F. Shackelford et al. (editors), 2015