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2618A Aluminum vs. 6106 Aluminum

Both 2618A aluminum and 6106 aluminum are aluminum alloys. They have a moderately high 95% of their average alloy composition in common.

For each property being compared, the top bar is 2618A aluminum and the bottom bar is 6106 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 72
69
Elongation at Break, % 4.5
9.1
Fatigue Strength, MPa 120
88
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 27
26
Shear Strength, MPa 260
170
Tensile Strength: Ultimate (UTS), MPa 440
290
Tensile Strength: Yield (Proof), MPa 410
220

Thermal Properties

Latent Heat of Fusion, J/g 390
400
Maximum Temperature: Mechanical, °C 230
160
Melting Completion (Liquidus), °C 670
660
Melting Onset (Solidus), °C 560
610
Specific Heat Capacity, J/kg-K 880
900
Thermal Conductivity, W/m-K 150
190
Thermal Expansion, µm/m-K 23
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 37
49
Electrical Conductivity: Equal Weight (Specific), % IACS 110
160

Otherwise Unclassified Properties

Base Metal Price, % relative 11
9.5
Density, g/cm3 3.0
2.7
Embodied Carbon, kg CO2/kg material 8.4
8.3
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1150
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 19
24
Resilience: Unit (Modulus of Resilience), kJ/m3 1180
370
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 47
50
Strength to Weight: Axial, points 41
29
Strength to Weight: Bending, points 44
35
Thermal Diffusivity, mm2/s 59
78
Thermal Shock Resistance, points 19
13

Alloy Composition


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Aluminum (Al), % 91.5 to 95.2
97.2 to 99.3
Chromium (Cr), % 0
0 to 0.2
Copper (Cu), % 1.8 to 2.7
0 to 0.25
Iron (Fe), % 0.9 to 1.4
0 to 0.35
Magnesium (Mg), % 1.2 to 1.8
0.4 to 0.8
Manganese (Mn), % 0 to 0.25
0.050 to 0.2
Nickel (Ni), % 0.8 to 1.4
0
Silicon (Si), % 0.15 to 0.25
0.3 to 0.6
Titanium (Ti), % 0 to 0.2
0 to 0.1
Zinc (Zn), % 0 to 0.15
0 to 0.15
Zirconium (Zr), % 0 to 0.25
0
Residuals, % 0 to 0.15
0 to 0.15