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6110 Aluminum vs. 1100A Aluminum

Both 6110 aluminum and 1100A aluminum are aluminum alloys. They have a very high 98% of their average alloy composition in common.

For each property being compared, the top bar is 6110 aluminum and the bottom bar is 1100A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
69
Elongation at Break, % 2.2
4.5 to 34
Fatigue Strength, MPa 120
35 to 74
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 290
59 to 99
Tensile Strength: Ultimate (UTS), MPa 500
89 to 170
Tensile Strength: Yield (Proof), MPa 500
29 to 150

Thermal Properties

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

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 42
60
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
6.4 to 23
Resilience: Unit (Modulus of Resilience), kJ/m3 1770
5.9 to 150
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
50
Strength to Weight: Axial, points 51
9.1 to 17
Strength to Weight: Bending, points 51
16 to 25
Thermal Diffusivity, mm2/s 67
93
Thermal Shock Resistance, points 22
4.0 to 7.6

Alloy Composition


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Aluminum (Al), % 94.4 to 98.4
99 to 100
Chromium (Cr), % 0.040 to 0.25
0
Copper (Cu), % 0.2 to 0.7
0.050 to 0.2
Iron (Fe), % 0 to 0.8
0 to 1.0
Magnesium (Mg), % 0.5 to 1.1
0 to 0.1
Manganese (Mn), % 0.2 to 0.7
0 to 0.050
Silicon (Si), % 0.7 to 1.5
0 to 1.0
Titanium (Ti), % 0 to 0.15
0 to 0.1
Zinc (Zn), % 0 to 0.3
0 to 0.1
Residuals, % 0 to 0.15
0 to 0.15