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6106 Aluminum vs. 8176 Aluminum

Both 6106 aluminum and 8176 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 6106 aluminum and the bottom bar is 8176 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 49
61
Electrical Conductivity: Equal Weight (Specific), % IACS 160
200

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
8.2
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1190
1190

Common Calculations

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

Alloy Composition

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