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6081 Aluminum vs. 5110A Aluminum

Both 6081 aluminum and 5110A 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 6081 aluminum and the bottom bar is 5110A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

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 1180
1190

Common Calculations

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

Alloy Composition

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