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2618A Aluminum vs. 6081 Aluminum

Both 2618A aluminum and 6081 aluminum are aluminum alloys. They have a very high 95% of their average alloy composition in common.

For each property being compared, the top bar is 2618A aluminum and the bottom bar is 6081 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 72
69
Elongation at Break, % 4.5
9.0
Fatigue Strength, MPa 120
110
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 27
26
Shear Strength, MPa 260
180
Tensile Strength: Ultimate (UTS), MPa 440
310
Tensile Strength: Yield (Proof), MPa 410
270

Thermal Properties

Latent Heat of Fusion, J/g 390
410
Maximum Temperature: Mechanical, °C 230
160
Melting Completion (Liquidus), °C 670
640
Melting Onset (Solidus), °C 560
610
Specific Heat Capacity, J/kg-K 880
900
Thermal Conductivity, W/m-K 150
180
Thermal Expansion, µm/m-K 23
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 37
47
Electrical Conductivity: Equal Weight (Specific), % IACS 110
160

Otherwise Unclassified Properties

Base Metal Price, % relative 11
9.5
Density, g/cm3 3.0
2.7
Embodied Carbon, kg CO2/kg material 8.4
8.3
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1150
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 19
27
Resilience: Unit (Modulus of Resilience), kJ/m3 1180
540
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 47
50
Strength to Weight: Axial, points 41
32
Strength to Weight: Bending, points 44
37
Thermal Diffusivity, mm2/s 59
74
Thermal Shock Resistance, points 19
14

Alloy Composition


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Aluminum (Al), % 91.5 to 95.2
96.3 to 98.6
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 1.8 to 2.7
0 to 0.1
Iron (Fe), % 0.9 to 1.4
0 to 0.5
Magnesium (Mg), % 1.2 to 1.8
0.6 to 1.0
Manganese (Mn), % 0 to 0.25
0.1 to 0.45
Nickel (Ni), % 0.8 to 1.4
0
Silicon (Si), % 0.15 to 0.25
0.7 to 1.1
Titanium (Ti), % 0 to 0.2
0 to 0.15
Zinc (Zn), % 0 to 0.15
0 to 0.2
Zirconium (Zr), % 0 to 0.25
0
Residuals, % 0 to 0.15
0 to 0.15