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8176 Aluminum vs. 6106 Aluminum

Both 8176 aluminum and 6106 aluminum are aluminum alloys. They have a very high 99% of their average alloy composition in common.

For each property being compared, the top bar is 8176 aluminum and the bottom bar is 6106 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
69
Elongation at Break, % 15
9.1
Fatigue Strength, MPa 59
88
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 70
170
Tensile Strength: Ultimate (UTS), MPa 160
290
Tensile Strength: Yield (Proof), MPa 95
220

Thermal Properties

Latent Heat of Fusion, J/g 400
400
Maximum Temperature: Mechanical, °C 170
160
Melting Completion (Liquidus), °C 660
660
Melting Onset (Solidus), °C 650
610
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 230
190
Thermal Expansion, µm/m-K 24
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 61
49
Electrical Conductivity: Equal Weight (Specific), % IACS 200
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 8.2
8.3
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1190
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 21
24
Resilience: Unit (Modulus of Resilience), kJ/m3 66
370
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
50
Strength to Weight: Axial, points 16
29
Strength to Weight: Bending, points 24
35
Thermal Diffusivity, mm2/s 93
78
Thermal Shock Resistance, points 7.0
13

Alloy Composition


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Aluminum (Al), % 98.6 to 99.6
97.2 to 99.3
Chromium (Cr), % 0
0 to 0.2
Copper (Cu), % 0
0 to 0.25
Gallium (Ga), % 0 to 0.030
0
Iron (Fe), % 0.4 to 1.0
0 to 0.35
Magnesium (Mg), % 0
0.4 to 0.8
Manganese (Mn), % 0
0.050 to 0.2
Silicon (Si), % 0.030 to 0.15
0.3 to 0.6
Titanium (Ti), % 0
0 to 0.1
Zinc (Zn), % 0 to 0.1
0 to 0.15
Residuals, % 0 to 0.15
0 to 0.15