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6106 Aluminum vs. 5082 Aluminum

Both 6106 aluminum and 5082 aluminum are aluminum alloys. They have a very high 96% of their average alloy composition in common.

For each property being compared, the top bar is 6106 aluminum and the bottom bar is 5082 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
67
Elongation at Break, % 9.1
1.1
Fatigue Strength, MPa 88
110 to 130
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
25
Shear Strength, MPa 170
210 to 230
Tensile Strength: Ultimate (UTS), MPa 290
380 to 400
Tensile Strength: Yield (Proof), MPa 220
300 to 340

Thermal Properties

Latent Heat of Fusion, J/g 400
400
Maximum Temperature: Mechanical, °C 160
180
Melting Completion (Liquidus), °C 660
640
Melting Onset (Solidus), °C 610
560
Specific Heat Capacity, J/kg-K 900
910
Thermal Conductivity, W/m-K 190
130
Thermal Expansion, µm/m-K 23
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 49
32
Electrical Conductivity: Equal Weight (Specific), % IACS 160
110

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
8.9
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1190
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 24
4.0 to 4.3
Resilience: Unit (Modulus of Resilience), kJ/m3 370
670 to 870
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
51
Strength to Weight: Axial, points 29
39 to 41
Strength to Weight: Bending, points 35
43 to 45
Thermal Diffusivity, mm2/s 78
54
Thermal Shock Resistance, points 13
17 to 18

Alloy Composition

Aluminum (Al), % 97.2 to 99.3
93.5 to 96
Chromium (Cr), % 0 to 0.2
0 to 0.15
Copper (Cu), % 0 to 0.25
0 to 0.15
Iron (Fe), % 0 to 0.35
0 to 0.35
Magnesium (Mg), % 0.4 to 0.8
4.0 to 5.0
Manganese (Mn), % 0.050 to 0.2
0 to 0.15
Silicon (Si), % 0.3 to 0.6
0 to 0.2
Titanium (Ti), % 0 to 0.1
0 to 0.1
Zinc (Zn), % 0 to 0.15
0 to 0.25
Residuals, % 0
0 to 0.15