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5110A Aluminum vs. 6081 Aluminum

Both 5110A aluminum and 6081 aluminum are aluminum alloys. They have a very high 98% of their average alloy composition in common.

For each property being compared, the top bar is 5110A aluminum and the bottom bar is 6081 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
69
Elongation at Break, % 4.5 to 28
9.0
Fatigue Strength, MPa 37 to 77
110
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 66 to 110
180
Tensile Strength: Ultimate (UTS), MPa 100 to 190
310
Tensile Strength: Yield (Proof), MPa 32 to 170
270

Thermal Properties

Latent Heat of Fusion, J/g 400
410
Maximum Temperature: Mechanical, °C 180
160
Melting Completion (Liquidus), °C 640
640
Melting Onset (Solidus), °C 640
610
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 220
180
Thermal Expansion, µm/m-K 23
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 57
47
Electrical Conductivity: Equal Weight (Specific), % IACS 190
160

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.5
Density, g/cm3 2.7
2.7
Embodied Carbon, kg CO2/kg material 8.3
8.3
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1190
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 6.8 to 22
27
Resilience: Unit (Modulus of Resilience), kJ/m3 7.6 to 200
540
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
50
Strength to Weight: Axial, points 10 to 19
32
Strength to Weight: Bending, points 18 to 27
37
Thermal Diffusivity, mm2/s 91
74
Thermal Shock Resistance, points 4.5 to 8.4
14

Alloy Composition

Aluminum (Al), % 98.5 to 99.8
96.3 to 98.6
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 0 to 0.2
0 to 0.1
Iron (Fe), % 0 to 0.25
0 to 0.5
Magnesium (Mg), % 0.2 to 0.6
0.6 to 1.0
Manganese (Mn), % 0 to 0.2
0.1 to 0.45
Silicon (Si), % 0 to 0.15
0.7 to 1.1
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0 to 0.030
0 to 0.2
Residuals, % 0
0 to 0.15