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6106 Aluminum vs. 5070 Aluminum

Both 6106 aluminum and 5070 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 5070 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
68
Elongation at Break, % 9.1
20
Fatigue Strength, MPa 88
150
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 170
190
Tensile Strength: Ultimate (UTS), MPa 290
300
Tensile Strength: Yield (Proof), MPa 220
140

Thermal Properties

Latent Heat of Fusion, J/g 400
390
Maximum Temperature: Mechanical, °C 160
190
Melting Completion (Liquidus), °C 660
640
Melting Onset (Solidus), °C 610
550
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 190
130
Thermal Expansion, µm/m-K 23
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 49
31
Electrical Conductivity: Equal Weight (Specific), % IACS 160
100

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
8.8
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1190
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 24
51
Resilience: Unit (Modulus of Resilience), kJ/m3 370
150
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
50
Strength to Weight: Axial, points 29
31
Strength to Weight: Bending, points 35
37
Thermal Diffusivity, mm2/s 78
53
Thermal Shock Resistance, points 13
14

Alloy Composition

Aluminum (Al), % 97.2 to 99.3
92.4 to 95.7
Chromium (Cr), % 0 to 0.2
0 to 0.3
Copper (Cu), % 0 to 0.25
0 to 0.25
Iron (Fe), % 0 to 0.35
0 to 0.4
Magnesium (Mg), % 0.4 to 0.8
3.5 to 4.5
Manganese (Mn), % 0.050 to 0.2
0.4 to 0.8
Silicon (Si), % 0.3 to 0.6
0 to 0.25
Titanium (Ti), % 0 to 0.1
0 to 0.15
Zinc (Zn), % 0 to 0.15
0.4 to 0.8
Residuals, % 0
0 to 0.15