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2618A Aluminum vs. 6110 Aluminum

Both 2618A aluminum and 6110 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 2618A aluminum and the bottom bar is 6110 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 72
70
Elongation at Break, % 4.5
2.2
Fatigue Strength, MPa 120
120
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 27
26
Shear Strength, MPa 260
290
Tensile Strength: Ultimate (UTS), MPa 440
500
Tensile Strength: Yield (Proof), MPa 410
500

Thermal Properties

Latent Heat of Fusion, J/g 390
410
Maximum Temperature: Mechanical, °C 230
170
Melting Completion (Liquidus), °C 670
640
Melting Onset (Solidus), °C 560
600
Specific Heat Capacity, J/kg-K 880
900
Thermal Conductivity, W/m-K 150
170
Thermal Expansion, µm/m-K 23
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 37
42
Electrical Conductivity: Equal Weight (Specific), % IACS 110
140

Otherwise Unclassified Properties

Base Metal Price, % relative 11
9.5
Density, g/cm3 3.0
2.8
Embodied Carbon, kg CO2/kg material 8.4
8.2
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1150
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 19
11
Resilience: Unit (Modulus of Resilience), kJ/m3 1180
1770
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 47
50
Strength to Weight: Axial, points 41
51
Strength to Weight: Bending, points 44
51
Thermal Diffusivity, mm2/s 59
67
Thermal Shock Resistance, points 19
22

Alloy Composition


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Aluminum (Al), % 91.5 to 95.2
94.4 to 98.4
Chromium (Cr), % 0
0.040 to 0.25
Copper (Cu), % 1.8 to 2.7
0.2 to 0.7
Iron (Fe), % 0.9 to 1.4
0 to 0.8
Magnesium (Mg), % 1.2 to 1.8
0.5 to 1.1
Manganese (Mn), % 0 to 0.25
0.2 to 0.7
Nickel (Ni), % 0.8 to 1.4
0
Silicon (Si), % 0.15 to 0.25
0.7 to 1.5
Titanium (Ti), % 0 to 0.2
0 to 0.15
Zinc (Zn), % 0 to 0.15
0 to 0.3
Zirconium (Zr), % 0 to 0.25
0
Residuals, % 0 to 0.15
0 to 0.15