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6110 Aluminum vs. 8176 Aluminum

Both 6110 aluminum and 8176 aluminum are aluminum alloys. They have a very high 97% of their average alloy composition in common.

For each property being compared, the top bar is 6110 aluminum and the bottom bar is 8176 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
69
Elongation at Break, % 2.2
15
Fatigue Strength, MPa 120
59
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 290
70
Tensile Strength: Ultimate (UTS), MPa 500
160
Tensile Strength: Yield (Proof), MPa 500
95

Thermal Properties

Latent Heat of Fusion, J/g 410
400
Maximum Temperature: Mechanical, °C 170
170
Melting Completion (Liquidus), °C 640
660
Melting Onset (Solidus), °C 600
650
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 170
230
Thermal Expansion, µm/m-K 23
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 42
61
Electrical Conductivity: Equal Weight (Specific), % IACS 140
200

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.5
Density, g/cm3 2.8
2.7
Embodied Carbon, kg CO2/kg material 8.2
8.2
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1170
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 11
21
Resilience: Unit (Modulus of Resilience), kJ/m3 1770
66
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
50
Strength to Weight: Axial, points 51
16
Strength to Weight: Bending, points 51
24
Thermal Diffusivity, mm2/s 67
93
Thermal Shock Resistance, points 22
7.0

Alloy Composition

Aluminum (Al), % 94.4 to 98.4
98.6 to 99.6
Chromium (Cr), % 0.040 to 0.25
0
Copper (Cu), % 0.2 to 0.7
0
Gallium (Ga), % 0
0 to 0.030
Iron (Fe), % 0 to 0.8
0.4 to 1.0
Magnesium (Mg), % 0.5 to 1.1
0
Manganese (Mn), % 0.2 to 0.7
0
Silicon (Si), % 0.7 to 1.5
0.030 to 0.15
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.3
0 to 0.1
Residuals, % 0
0 to 0.15